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DoinLakeFlyer authored
App messages now use simple modal message dialogs. Vehicle messages continue to use non-modal popup.
284a2c08
<?xml version="1.0" encoding="utf-8"?> <!-- Dynamically generated list of documented parameters (generated by param_parse.py) --> <paramfile> <vehicles> <parameters name="ArduPlane"><param humanName="Eeprom format version number" name="ArduPlane:FORMAT_VERSION" documentation="This value is incremented when changes are made to the eeprom format" user="Advanced"></param><param humanName="Software Type" name="ArduPlane:SYSID_SW_TYPE" documentation="This is used by the ground station to recognise the software type (eg ArduPlane vs ArduCopter)" user="Advanced"><field name="ReadOnly">True</field></param><param humanName="MAVLink system ID of this vehicle" name="ArduPlane:SYSID_THISMAV" documentation="Allows setting an individual MAVLink system id for this vehicle to distinguish it from others on the same network" user="Advanced"><field name="Range">1 255</field></param><param humanName="Ground station MAVLink system ID" name="ArduPlane:SYSID_MYGCS" documentation="The identifier of the ground station in the MAVLink protocol. Don't change this unless you also modify the ground station to match." user="Advanced"><field name="Range">1 255</field></param><param humanName="CLI Enable" name="ArduPlane:CLI_ENABLED" documentation="This enables/disables the checking for three carriage returns on telemetry links on startup to enter the diagnostics command line interface" user="Advanced"><values><value code="0">Disabled</value><value code="1">Enabled</value></values></param><param humanName="Autotune level" name="ArduPlane:AUTOTUNE_LEVEL" documentation="Level of aggressiveness for autotune. When autotune is run a lower AUTOTUNE_LEVEL will result in a 'softer' tune, with less aggressive gains. For most users a level of 6 is recommended." user="Standard"><field name="Range">1 10</field><field name="Increment">1</field></param><param humanName="Telemetry startup delay " name="ArduPlane:TELEM_DELAY" documentation="The amount of time (in seconds) to delay radio telemetry to prevent an Xbee bricking on power up" user="Standard"><field name="Range">0 30</field><field name="Increment">1</field><field name="Units">s</field><field name="UnitText">seconds</field></param><param humanName="GCS PID tuning mask" name="ArduPlane:GCS_PID_MASK" documentation="bitmask of PIDs to send MAVLink PID_TUNING messages for" user="Advanced"><field name="Bitmask">0:Roll,1:Pitch,2:Yaw,3:Steering,4:Landing</field></param><param humanName="Rudder Mix" name="ArduPlane:KFF_RDDRMIX" documentation="The amount of rudder mix to apply during aileron movement 0 = 0 %, 1 = 100%" user="Standard"><field name="Range">0 1</field><field name="Increment">0.01</field></param><param humanName="Throttle to Pitch Mix" name="ArduPlane:KFF_THR2PTCH" documentation="Throttle to pitch feed-forward gain." user="Advanced"><field name="Range">0 5</field><field name="Increment">0.01</field></param><param humanName="Low throttle pitch down trim " name="ArduPlane:STAB_PITCH_DOWN" documentation="This controls the amount of down pitch to add in FBWA and AUTOTUNE modes when at low throttle. No down trim is added when throttle is above TRIM_THROTTLE. Below TRIM_THROTTLE downtrim is added in proportion to the amount the throttle is below TRIM_THROTTLE. At zero throttle the full downpitch specified in this parameter is added. This parameter is meant to help keep airspeed up when flying in FBWA mode with low throttle, such as when on a landing approach, without relying on an airspeed sensor. A value of 2 degrees is good for many planes, although a higher value may be needed for high drag aircraft." user="Advanced"><field name="Range">0 15</field><field name="Increment">0.1</field><field name="Units">deg</field><field name="UnitText">degrees</field></param><param humanName="Glide slope minimum" name="ArduPlane:GLIDE_SLOPE_MIN" documentation="This controls the minimum altitude change for a waypoint before a glide slope will be used instead of an immediate altitude change. The default value is 15 meters, which helps to smooth out waypoint missions where small altitude changes happen near waypoints. If you don't want glide slopes to be used in missions then you can set this to zero, which will disable glide slope calculations. Otherwise you can set it to a minimum number of meters of altitude error to the destination waypoint before a glide slope will be used to change altitude." user="Advanced"><field name="Range">0 1000</field><field name="Increment">1</field><field name="Units">m</field><field name="UnitText">meters</field></param><param humanName="Glide slope threshold" name="ArduPlane:GLIDE_SLOPE_THR" documentation="This controls the height above the glide slope the plane may be before rebuilding a glide slope. This is useful for smoothing out an autotakeoff" user="Advanced"><field name="Range">0 100</field><field name="Increment">1</field><field name="Units">m</field><field name="UnitText">meters</field></param><param humanName="Stick Mixing" name="ArduPlane:STICK_MIXING" documentation='When enabled, this adds user stick input to the control surfaces in auto modes, allowing the user to have some degree of flight control without changing modes. There are two types of stick mixing available. If you set STICK_MIXING to 1 then it will use "fly by wire" mixing, which controls the roll and pitch in the same way that the FBWA mode does. This is the safest option if you usually fly ArduPlane in FBWA or FBWB mode. If you set STICK_MIXING to 2 then it will enable direct mixing mode, which is what the STABILIZE mode uses. That will allow for much more extreme maneuvers while in AUTO mode.' user="Advanced"><values><value code="0">Disabled</value><value code="1">FBWMixing</value><value code="2">DirectMixing</value></values></param><param humanName="Use FBWA steering in AUTO" name="ArduPlane:AUTO_FBW_STEER" documentation="When enabled this option gives FBWA navigation and steering in AUTO mode. This can be used to allow manual stabilised piloting with waypoint logic for triggering payloads. With this enabled the pilot has the same control over the plane as in FBWA mode, and the normal AUTO navigation is completely disabled. THIS OPTION IS NOT RECOMMENDED FOR NORMAL USE." user="Advanced"><values>
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<value code="0">Disabled</value>
<value code="42">Enabled</value>
</values>
</param>
<param humanName="Takeoff throttle min speed" name="ArduPlane:TKOFF_THR_MINSPD" documentation="Minimum GPS ground speed in m/s used by the speed check that un-suppresses throttle in auto-takeoff. This can be be used for catapult launches where you want the motor to engage only after the plane leaves the catapult, but it is preferable to use the TKOFF_THR_MINACC and TKOFF_THR_DELAY parameters for catapult launches due to the errors associated with GPS measurements. For hand launches with a pusher prop it is strongly advised that this parameter be set to a value no less than 4 m/s to provide additional protection against premature motor start. Note that the GPS velocity will lag the real velocity by about 0.5 seconds. The ground speed check is delayed by the TKOFF_THR_DELAY parameter." user="User">
<field name="Range">0 30</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Takeoff throttle min acceleration" name="ArduPlane:TKOFF_THR_MINACC" documentation="Minimum forward acceleration in m/s/s before arming the ground speed check in auto-takeoff. This is meant to be used for hand launches. Setting this value to 0 disables the acceleration test which means the ground speed check will always be armed which could allow GPS velocity jumps to start the engine. For hand launches and bungee launches this should be set to around 15." user="User">
<field name="Range">0 30</field>
<field name="Increment">0.1</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Takeoff throttle delay" name="ArduPlane:TKOFF_THR_DELAY" documentation="This parameter sets the time delay (in 1/10ths of a second) that the ground speed check is delayed after the forward acceleration check controlled by TKOFF_THR_MINACC has passed. For hand launches with pusher propellers it is essential that this is set to a value of no less than 2 (0.2 seconds) to ensure that the aircraft is safely clear of the throwers arm before the motor can start. For bungee launches a larger value can be used (such as 30) to give time for the bungee to release from the aircraft before the motor is started." user="User">
<field name="Range">0 127</field>
<field name="Increment">1</field>
<field name="Units">ds</field>
<field name="UnitText">deciseconds</field>
</param>
<param humanName="Takeoff tail dragger elevator" name="ArduPlane:TKOFF_TDRAG_ELEV" documentation="This parameter sets the amount of elevator to apply during the initial stage of a takeoff. It is used to hold the tail wheel of a taildragger on the ground during the initial takeoff stage to give maximum steering. This option should be combined with the TKOFF_TDRAG_SPD1 option and the GROUND_STEER_ALT option along with tuning of the ground steering controller. A value of zero means to bypass the initial "tail hold" stage of takeoff. Set to zero for hand and catapult launch. For tail-draggers you should normally set this to 100, meaning full up elevator during the initial stage of takeoff. For most tricycle undercarriage aircraft a value of zero will work well, but for some tricycle aircraft a small negative value (say around -20 to -30) will apply down elevator which will hold the nose wheel firmly on the ground during initial acceleration. Only use a negative value if you find that the nosewheel doesn't grip well during takeoff. Too much down elevator on a tricycle undercarriage may cause instability in steering as the plane pivots around the nosewheel. Add down elevator 10 percent at a time." user="User">
<field name="Range">-100 100</field>
<field name="Increment">1</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Takeoff tail dragger speed1" name="ArduPlane:TKOFF_TDRAG_SPD1" documentation='This parameter sets the airspeed at which to stop holding the tail down and transition to rudder control of steering on the ground. When TKOFF_TDRAG_SPD1 is reached the pitch of the aircraft will be held level until TKOFF_ROTATE_SPD is reached, at which point the takeoff pitch specified in the mission will be used to "rotate" the pitch for takeoff climb. Set TKOFF_TDRAG_SPD1 to zero to go straight to rotation. This should be set to zero for hand launch and catapult launch. It should also be set to zero for tricycle undercarriages unless you are using the method above to genetly hold the nose wheel down. For tail dragger aircraft it should be set just below the stall speed.' user="User">
<field name="Range">0 30</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Takeoff rotate speed" name="ArduPlane:TKOFF_ROTATE_SPD" documentation='This parameter sets the airspeed at which the aircraft will "rotate", setting climb pitch specified in the mission. If TKOFF_ROTATE_SPD is zero then the climb pitch will be used as soon as takeoff is started. For hand launch and catapult launches a TKOFF_ROTATE_SPD of zero should be set. For all ground launches TKOFF_ROTATE_SPD should be set above the stall speed, usually by about 10 to 30 percent' user="User">
<field name="Range">0 30</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Takeoff throttle slew rate" name="ArduPlane:TKOFF_THR_SLEW" documentation="This parameter sets the slew rate for the throttle during auto takeoff. When this is zero the THR_SLEWRATE parameter is used during takeoff. For rolling takeoffs it can be a good idea to set a lower slewrate for takeoff to give a slower acceleration which can improve ground steering control. The value is a percentage throttle change per second, so a value of 20 means to advance the throttle over 5 seconds on takeoff. Values below 20 are not recommended as they may cause the plane to try to climb out with too little throttle." user="User">
<field name="Range">0 127</field>
<field name="Increment">1</field>
<field name="Units">%/s</field>
<field name="UnitText">percent per second</field>
</param>
<param humanName="Takeoff pitch limit reduction" name="ArduPlane:TKOFF_PLIM_SEC" documentation="This parameter reduces the pitch minimum limit of an auto-takeoff just a few seconds before it reaches the target altitude. This reduces overshoot by allowing the flight controller to start leveling off a few seconds before reaching the target height. When set to zero, the mission pitch min is enforced all the way to and through the target altitude, otherwise the pitch min slowly reduces to zero in the final segment. This is the pitch_min, not the demand. The flight controller should still be commanding to gain altitude to finish the takeoff but with this param it is not forcing it higher than it wants to be." user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">0.5</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Takeoff flap percentage" name="ArduPlane:TKOFF_FLAP_PCNT" documentation="The amount of flaps (as a percentage) to apply in automatic takeoff" user="Advanced">
<field name="Range">0 100</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="FBWA taildragger channel" name="ArduPlane:FBWA_TDRAG_CHAN" documentation="This is a RC input channel which when it goes above 1700 enables FBWA taildragger takeoff mode. It should be assigned to a momentary switch. Once this feature is enabled it will stay enabled until the aircraft goes above TKOFF_TDRAG_SPD1 airspeed, changes mode, or the pitch goes above the initial pitch when this is engaged or goes below 0 pitch. When enabled the elevator will be forced to TKOFF_TDRAG_ELEV. This option allows for easier takeoffs on taildraggers in FBWA mode, and also makes it easier to test auto-takeoff steering handling in FBWA. Setting it to 0 disables this option." user="Standard">
</param>
<param humanName="Level flight roll limit" name="ArduPlane:LEVEL_ROLL_LIMIT" documentation="This controls the maximum bank angle in degrees during flight modes where level flight is desired, such as in the final stages of landing, and during auto takeoff. This should be a small angle (such as 5 degrees) to prevent a wing hitting the runway during takeoff or landing. Setting this to zero will completely disable heading hold on auto takeoff and final landing approach." user="User">
<field name="Range">0 45</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Bitmask for when to allow negative reverse thrust" name="ArduPlane:USE_REV_THRUST" documentation="Typically THR_MIN will be clipped to zero unless reverse thrust is available. Since you may not want negative thrust available at all times this bitmask allows THR_MIN to go below 0 while executing certain auto-mission commands." user="Advanced">
<field name="Bitmask">0:AUTO_ALWAYS,1:AUTO_LAND,2:AUTO_LOITER_TO_ALT,3:AUTO_LOITER_ALL,4:AUTO_WAYPOINTS,5:LOITER,6:RTL,7:CIRCLE,8:CRUISE,9:FBWB,10:GUIDED</field>
</param>
<param humanName="Navigation controller selection" name="ArduPlane:NAV_CONTROLLER" documentation="Which navigation controller to enable. Currently the only navigation controller available is L1. From time to time other experimental controllers will be added which are selected using this parameter." user="Standard">
<values>
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<value code="0">Default</value>
<value code="1">L1Controller</value>
</values>
</param>
<param humanName="Altitude control algorithm" name="ArduPlane:ALT_CTRL_ALG" documentation="This sets what algorithm will be used for altitude control. The default is zero, which selects the most appropriate algorithm for your airframe. Currently the default is to use TECS (total energy control system). From time to time we will add other experimental altitude control algorithms which will be selected using this parameter." user="Advanced">
<values>
<value code="0">Automatic</value>
</values>
</param>
<param humanName="Altitude offset" name="ArduPlane:ALT_OFFSET" documentation="This is added to the target altitude in automatic flight. It can be used to add a global altitude offset to a mission" user="Advanced">
<field name="Range">-32767 32767</field>
<field name="Increment">1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Waypoint Radius" name="ArduPlane:WP_RADIUS" documentation='Defines the maximum distance from a waypoint that when crossed indicates the waypoint may be complete. To avoid the aircraft looping around the waypoint in case it misses by more than the WP_RADIUS an additional check is made to see if the aircraft has crossed a "finish line" passing through the waypoint and perpendicular to the flight path from the previous waypoint. If that finish line is crossed then the waypoint is considered complete. Note that the navigation controller may decide to turn later than WP_RADIUS before a waypoint, based on how sharp the turn is and the speed of the aircraft. It is safe to set WP_RADIUS much larger than the usual turn radius of your aircraft and the navigation controller will work out when to turn. If you set WP_RADIUS too small then you will tend to overshoot the turns.' user="Standard">
<field name="Range">1 32767</field>
<field name="Increment">1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Waypoint Maximum Radius" name="ArduPlane:WP_MAX_RADIUS" documentation='Sets the maximum distance to a waypoint for the waypoint to be considered complete. This overrides the "cross the finish line" logic that is normally used to consider a waypoint complete. For normal AUTO behaviour this parameter should be set to zero. Using a non-zero value is only recommended when it is critical that the aircraft does approach within the given radius, and should loop around until it has done so. This can cause the aircraft to loop forever if its turn radius is greater than the maximum radius set.' user="Standard">
<field name="Range">0 32767</field>
<field name="Increment">1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Waypoint Loiter Radius" name="ArduPlane:WP_LOITER_RAD" documentation="Defines the distance from the waypoint center, the plane will maintain during a loiter. If you set this value to a negative number then the default loiter direction will be counter-clockwise instead of clockwise." user="Standard">
<field name="Range">-32767 32767</field>
<field name="Increment">1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="RTL loiter radius" name="ArduPlane:RTL_RADIUS" documentation="Defines the radius of the loiter circle when in RTL mode. If this is zero then WP_LOITER_RAD is used. If the radius is negative then a counter-clockwise is used. If positive then a clockwise loiter is used." user="Standard">
<field name="Range">-32767 32767</field>
<field name="Increment">1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Action on geofence breach" name="ArduPlane:FENCE_ACTION" documentation="What to do on fence breach. If this is set to 0 then no action is taken, and geofencing is disabled. If this is set to 1 then the plane will enter GUIDED mode, with the target waypoint as the fence return point. If this is set to 2 then the fence breach is reported to the ground station, but no other action is taken. If set to 3 then the plane enters guided mode but the pilot retains manual throttle control. If set to 4 the plane enters RTL mode, with the target waypoint as the closest rally point (or home point if there are no rally points)." user="Standard">
<values>
<value code="0">None</value>
<value code="1">GuidedMode</value>
<value code="2">ReportOnly</value>
<value code="3">GuidedModeThrPass</value>
<value code="4">RTL_Mode</value>
</values>
</param>
<param humanName="Fence Total" name="ArduPlane:FENCE_TOTAL" documentation="Number of geofence points currently loaded" user="Advanced">
</param>
<param humanName="Fence Channel" name="ArduPlane:FENCE_CHANNEL" documentation="RC Channel to use to enable geofence. PWM input above 1750 enables the geofence" user="Standard">
</param>
<param humanName="Fence Minimum Altitude" name="ArduPlane:FENCE_MINALT" documentation="Minimum altitude allowed before geofence triggers" user="Standard">
<field name="Range">0 32767</field>
<field name="Increment">1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Fence Maximum Altitude" name="ArduPlane:FENCE_MAXALT" documentation="Maximum altitude allowed before geofence triggers" user="Standard">
<field name="Range">0 32767</field>
<field name="Increment">1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Fence Return Altitude" name="ArduPlane:FENCE_RETALT" documentation="Altitude the aircraft will transit to when a fence breach occurs. If FENCE_RETALT is <= 0 then the midpoint between FENCE_MAXALT and FENCE_MINALT is used, unless FENCE_MAXALT < FENCE_MINALT. If FENCE_MAXALT < FENCE_MINALT AND FENCE_RETALT is <= 0 then ALT_HOLD_RTL is the altitude used on a fence breach." user="Standard">
<field name="Range">0 32767</field>
<field name="Increment">1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
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<param humanName="Fence automatic enable" name="ArduPlane:FENCE_AUTOENABLE" documentation="When set to 1, geofence automatically enables after an auto takeoff and automatically disables at the beginning of an auto landing. When on the ground before takeoff the fence is disabled. When set to 2, the fence autoenables after an auto takeoff, but only disables the fence floor during landing. It is highly recommended to not use this option for line of sight flying and use a fence enable channel instead." user="Standard">
<values>
<value code="0">NoAutoEnable</value>
<value code="1">AutoEnable</value>
<value code="2">AutoEnableDisableFloorOnly</value>
</values>
</param>
<param humanName="Fence Return to Rally" name="ArduPlane:FENCE_RET_RALLY" documentation="When set to 1: on fence breach the plane will return to the nearest rally point rather than the fence return point. If no rally points have been defined the plane will return to the home point. " user="Standard">
<values>
<value code="0">FenceReturnPoint</value>
<value code="1">NearestRallyPoint</value>
</values>
</param>
<param humanName="Enable stall prevention" name="ArduPlane:STALL_PREVENTION" documentation="This controls the use of stall prevention techniques, including roll limits at low speed and raising the minimum airspeed in turns. The limits are based on the aerodynamic load factor of a banked turn. This option relies on the correct ARSPD_FBW_MIN value being set correctly. Note that if you don't have an airspeed sensor then stall prevention will use an airspeed estimate based on the ground speed plus a wind estimate taken from the response of the autopilot banked turns. That synthetic airspeed estimate may be inaccurate, so you should not assume that stall prevention with no airspeed sensor will be effective." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Minimum Airspeed" name="ArduPlane:ARSPD_FBW_MIN" documentation="This is the minimum airspeed you want to fly at in modes where the autopilot controls the airspeed. This should be set to a value around 20% higher than the level flight stall speed for the airframe. This value is also used in the STALL_PREVENTION code." user="Standard">
<field name="Range">5 100</field>
<field name="Increment">1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Maximum Airspeed" name="ArduPlane:ARSPD_FBW_MAX" documentation="This is the maximum airspeed that you want to allow for your airframe in auto-throttle modes. You should ensure that this value is sufficiently above the ARSPD_FBW_MIN value to allow for a sufficient flight envelope to accurately control altitude using airspeed. A value at least 50% above ARSPD_FBW_MIN is recommended." user="Standard">
<field name="Range">5 100</field>
<field name="Increment">1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Fly By Wire elevator reverse" name="ArduPlane:FBWB_ELEV_REV" documentation="Reverse sense of elevator in FBWB and CRUISE modes. When set to 0 up elevator (pulling back on the stick) means to lower altitude. When set to 1, up elevator means to raise altitude." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Use terrain following" name="ArduPlane:TERRAIN_FOLLOW" documentation="This enables terrain following for CRUISE mode, FBWB mode, RTL and for rally points. To use this option you also need to set TERRAIN_ENABLE to 1, which enables terrain data fetching from the GCS, and you need to have a GCS that supports sending terrain data to the aircraft. When terrain following is enabled then CRUISE and FBWB mode will hold height above terrain rather than height above home. In RTL the return to launch altitude will be considered to be a height above the terrain. Rally point altitudes will be taken as height above the terrain. This option does not affect mission items, which have a per-waypoint flag for whether they are height above home or height above the terrain. To use terrain following missions you need a ground station which can set the waypoint type to be a terrain height waypoint when creating the mission." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Terrain lookahead" name="ArduPlane:TERRAIN_LOOKAHD" documentation="This controls how far ahead the terrain following code looks to ensure it stays above upcoming terrain. A value of zero means no lookahead, so the controller will track only the terrain directly below the aircraft. The lookahead will never extend beyond the next waypoint when in AUTO mode." user="Standard">
<field name="Range">0 10000</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Fly By Wire B altitude change rate" name="ArduPlane:FBWB_CLIMB_RATE" documentation="This sets the rate in m/s at which FBWB and CRUISE modes will change its target altitude for full elevator deflection. Note that the actual climb rate of the aircraft can be lower than this, depending on your airspeed and throttle control settings. If you have this parameter set to the default value of 2.0, then holding the elevator at maximum deflection for 10 seconds would change the target altitude by 20 meters." user="Standard">
<field name="Range">1 10</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Minimum Throttle" name="ArduPlane:THR_MIN" documentation="The minimum throttle setting (as a percentage) which the autopilot will apply. For the final stage of an automatic landing this is always zero. If your ESC supports reverse, use a negative value to configure for reverse thrust." user="Standard">
<field name="Range">-100 100</field>
<field name="Increment">1</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Maximum Throttle" name="ArduPlane:THR_MAX" documentation="The maximum throttle setting (as a percentage) which the autopilot will apply." user="Standard">
<field name="Range">0 100</field>
<field name="Increment">1</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Maximum Throttle for takeoff" name="ArduPlane:TKOFF_THR_MAX" documentation="The maximum throttle setting during automatic takeoff. If this is zero then THR_MAX is used for takeoff as well." user="Advanced">
<field name="Range">0 100</field>
<field name="Increment">1</field>
<field name="Units">%</field>
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<field name="UnitText">percent</field>
</param>
<param humanName="Throttle slew rate" name="ArduPlane:THR_SLEWRATE" documentation="maximum percentage change in throttle per second. A setting of 10 means to not change the throttle by more than 10% of the full throttle range in one second." user="Standard">
<field name="Range">0 127</field>
<field name="Increment">1</field>
<field name="Units">%/s</field>
<field name="UnitText">percent per second</field>
</param>
<param humanName="Flap slew rate" name="ArduPlane:FLAP_SLEWRATE" documentation="maximum percentage change in flap output per second. A setting of 25 means to not change the flap by more than 25% of the full flap range in one second. A value of 0 means no rate limiting." user="Advanced">
<field name="Range">0 100</field>
<field name="Increment">1</field>
<field name="Units">%/s</field>
<field name="UnitText">percent per second</field>
</param>
<param humanName="Throttle suppress manual passthru" name="ArduPlane:THR_SUPP_MAN" documentation="When throttle is suppressed in auto mode it is normally forced to zero. If you enable this option, then while suppressed it will be manual throttle. This is useful on petrol engines to hold the idle throttle manually while waiting for takeoff" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Throttle passthru in stabilize" name="ArduPlane:THR_PASS_STAB" documentation="If this is set then when in STABILIZE, FBWA or ACRO modes the throttle is a direct passthru from the transmitter. This means the THR_MIN and THR_MAX settings are not used in these modes. This is useful for petrol engines where you setup a throttle cut switch that suppresses the throttle below the normal minimum." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Throttle Failsafe Enable" name="ArduPlane:THR_FAILSAFE" documentation="The throttle failsafe allows you to configure a software failsafe activated by a setting on the throttle input channel" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Throttle Failsafe Value" name="ArduPlane:THR_FS_VALUE" documentation="The PWM level on channel 3 below which throttle failsafe triggers" user="Standard">
<field name="Range">925 2200</field>
<field name="Increment">1</field>
</param>
<param humanName="Throttle cruise percentage" name="ArduPlane:TRIM_THROTTLE" documentation="The target percentage of throttle to apply for normal flight" user="Standard">
<field name="Range">0 100</field>
<field name="Increment">1</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Throttle nudge enable" name="ArduPlane:THROTTLE_NUDGE" documentation="When enabled, this uses the throttle input in auto-throttle modes to 'nudge' the throttle or airspeed to higher or lower values. When you have an airspeed sensor the nudge affects the target airspeed, so that throttle inputs above 50% will increase the target airspeed from TRIM_ARSPD_CM up to a maximum of ARSPD_FBW_MAX. When no airspeed sensor is enabled the throttle nudge will push up the target throttle for throttle inputs above 50%." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Short failsafe action" name="ArduPlane:FS_SHORT_ACTN" documentation="The action to take on a short (FS_SHORT_TIMEOUT) failsafe event. A short failsafe even can be triggered either by loss of RC control (see THR_FS_VALUE) or by loss of GCS control (see FS_GCS_ENABL). If in CIRCLE or RTL mode this parameter is ignored. A short failsafe event in stabilization and manual modes will cause an change to CIRCLE mode if FS_SHORT_ACTN is 0 or 1, and a change to FBWA mode if FS_SHORT_ACTN is 2. In all other modes (AUTO, GUIDED and LOITER) a short failsafe event will cause no mode change is FS_SHORT_ACTN is set to 0, will cause a change to CIRCLE mode if set to 1 and will change to FBWA mode if set to 2. Please see the documentation for FS_LONG_ACTN for the behaviour after FS_LONG_TIMEOUT seconds of failsafe." user="Standard">
<values>
<value code="0">CIRCLE/no change(if already in AUTO|GUIDED|LOITER)</value>
<value code="1">CIRCLE</value>
<value code="2">FBWA</value>
</values>
</param>
<param humanName="Short failsafe timeout" name="ArduPlane:FS_SHORT_TIMEOUT" documentation="The time in seconds that a failsafe condition has to persist before a short failsafe event will occur. This defaults to 1.5 seconds" user="Standard">
<field name="Range">1 100</field>
<field name="Increment">0.5</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Long failsafe action" name="ArduPlane:FS_LONG_ACTN" documentation="The action to take on a long (FS_LONG_TIMEOUT seconds) failsafe event. If the aircraft was in a stabilization or manual mode when failsafe started and a long failsafe occurs then it will change to RTL mode if FS_LONG_ACTN is 0 or 1, and will change to FBWA if FS_LONG_ACTN is set to 2. If the aircraft was in an auto mode (such as AUTO or GUIDED) when the failsafe started then it will continue in the auto mode if FS_LONG_ACTN is set to 0, will change to RTL mode if FS_LONG_ACTN is set to 1 and will change to FBWA mode if FS_LONG_ACTN is set to 2. If FS_LONG_ACTION is set to 3, the parachute will be deployed (make sure the chute is configured and enabled). " user="Standard">
<values>
<value code="0">Continue</value>
<value code="1">ReturnToLaunch</value>
<value code="2">Glide</value>
<value code="3">Deploy Parachute</value>
</values>
</param>
<param humanName="Long failsafe timeout" name="ArduPlane:FS_LONG_TIMEOUT" documentation="The time in seconds that a failsafe condition has to persist before a long failsafe event will occur. This defaults to 5 seconds." user="Standard">
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<field name="Range">1 300</field>
<field name="Increment">0.5</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Failsafe battery voltage" name="ArduPlane:FS_BATT_VOLTAGE" documentation="Battery voltage to trigger failsafe. Set to 0 to disable battery voltage failsafe. If the battery voltage drops below this voltage continuously for 10 seconds then the plane will switch to RTL mode." user="Standard">
<field name="Increment">0.1</field>
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
<param humanName="Failsafe battery milliAmpHours" name="ArduPlane:FS_BATT_MAH" documentation="Battery capacity remaining to trigger failsafe. Set to 0 to disable battery remaining failsafe. If the battery remaining drops below this level then the plane will switch to RTL mode immediately." user="Standard">
<field name="Increment">50</field>
<field name="Units">mA.h</field>
<field name="UnitText">milliampere hour</field>
</param>
<param humanName="GCS failsafe enable" name="ArduPlane:FS_GCS_ENABL" documentation="Enable ground control station telemetry failsafe. Failsafe will trigger after FS_LONG_TIMEOUT seconds of no MAVLink heartbeat messages. There are two possible enabled settings. Seeing FS_GCS_ENABL to 1 means that GCS failsafe will be triggered when the aircraft has not received a MAVLink HEARTBEAT message. Setting FS_GCS_ENABL to 2 means that GCS failsafe will be triggered on either a loss of HEARTBEAT messages, or a RADIO_STATUS message from a MAVLink enabled 3DR radio indicating that the ground station is not receiving status updates from the aircraft, which is indicated by the RADIO_STATUS.remrssi field being zero (this may happen if you have a one way link due to asymmetric noise on the ground station and aircraft radios).Setting FS_GCS_ENABL to 3 means that GCS failsafe will be triggered by Heartbeat(like option one), but only in AUTO mode. WARNING: Enabling this option opens up the possibility of your plane going into failsafe mode and running the motor on the ground it it loses contact with your ground station. If this option is enabled on an electric plane then you should enable ARMING_REQUIRED." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Heartbeat</value>
<value code="2">HeartbeatAndREMRSSI</value>
<value code="3">HeartbeatAndAUTO</value>
</values>
</param>
<param humanName="Flightmode channel" name="ArduPlane:FLTMODE_CH" documentation="RC Channel to use for flight mode control" user="Advanced">
</param>
<param humanName="FlightMode1" name="ArduPlane:FLTMODE1" documentation="Flight mode for switch position 1 (910 to 1230 and above 2049)" user="Standard">
<values>
<value code="0">Manual</value>
<value code="1">CIRCLE</value>
<value code="2">STABILIZE</value>
<value code="3">TRAINING</value>
<value code="4">ACRO</value>
<value code="5">FBWA</value>
<value code="6">FBWB</value>
<value code="7">CRUISE</value>
<value code="8">AUTOTUNE</value>
<value code="10">Auto</value>
<value code="11">RTL</value>
<value code="12">Loiter</value>
<value code="14">AVOID_ADSB</value>
<value code="15">Guided</value>
<value code="17">QSTABILIZE</value>
<value code="18">QHOVER</value>
<value code="19">QLOITER</value>
<value code="20">QLAND</value>
<value code="21">QRTL</value>
</values>
</param>
<param humanName="FlightMode2" name="ArduPlane:FLTMODE2" documentation="Flight mode for switch position 2 (1231 to 1360)" user="Standard">
<values>
<value code="0">Manual</value>
<value code="1">CIRCLE</value>
<value code="2">STABILIZE</value>
<value code="3">TRAINING</value>
<value code="4">ACRO</value>
<value code="5">FBWA</value>
<value code="6">FBWB</value>
<value code="7">CRUISE</value>
<value code="8">AUTOTUNE</value>
<value code="10">Auto</value>
<value code="11">RTL</value>
<value code="12">Loiter</value>
<value code="14">AVOID_ADSB</value>
<value code="15">Guided</value>
<value code="17">QSTABILIZE</value>
<value code="18">QHOVER</value>
<value code="19">QLOITER</value>
<value code="20">QLAND</value>
<value code="21">QRTL</value>
</values>
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</param>
<param humanName="FlightMode3" name="ArduPlane:FLTMODE3" documentation="Flight mode for switch position 3 (1361 to 1490)" user="Standard">
<values>
<value code="0">Manual</value>
<value code="1">CIRCLE</value>
<value code="2">STABILIZE</value>
<value code="3">TRAINING</value>
<value code="4">ACRO</value>
<value code="5">FBWA</value>
<value code="6">FBWB</value>
<value code="7">CRUISE</value>
<value code="8">AUTOTUNE</value>
<value code="10">Auto</value>
<value code="11">RTL</value>
<value code="12">Loiter</value>
<value code="14">AVOID_ADSB</value>
<value code="15">Guided</value>
<value code="17">QSTABILIZE</value>
<value code="18">QHOVER</value>
<value code="19">QLOITER</value>
<value code="20">QLAND</value>
<value code="21">QRTL</value>
</values>
</param>
<param humanName="FlightMode4" name="ArduPlane:FLTMODE4" documentation="Flight mode for switch position 4 (1491 to 1620)" user="Standard">
<values>
<value code="0">Manual</value>
<value code="1">CIRCLE</value>
<value code="2">STABILIZE</value>
<value code="3">TRAINING</value>
<value code="4">ACRO</value>
<value code="5">FBWA</value>
<value code="6">FBWB</value>
<value code="7">CRUISE</value>
<value code="8">AUTOTUNE</value>
<value code="10">Auto</value>
<value code="11">RTL</value>
<value code="12">Loiter</value>
<value code="14">AVOID_ADSB</value>
<value code="15">Guided</value>
<value code="17">QSTABILIZE</value>
<value code="18">QHOVER</value>
<value code="19">QLOITER</value>
<value code="20">QLAND</value>
<value code="21">QRTL</value>
</values>
</param>
<param humanName="FlightMode5" name="ArduPlane:FLTMODE5" documentation="Flight mode for switch position 5 (1621 to 1749)" user="Standard">
<values>
<value code="0">Manual</value>
<value code="1">CIRCLE</value>
<value code="2">STABILIZE</value>
<value code="3">TRAINING</value>
<value code="4">ACRO</value>
<value code="5">FBWA</value>
<value code="6">FBWB</value>
<value code="7">CRUISE</value>
<value code="8">AUTOTUNE</value>
<value code="10">Auto</value>
<value code="11">RTL</value>
<value code="12">Loiter</value>
<value code="14">AVOID_ADSB</value>
<value code="15">Guided</value>
<value code="17">QSTABILIZE</value>
<value code="18">QHOVER</value>
<value code="19">QLOITER</value>
<value code="20">QLAND</value>
<value code="21">QRTL</value>
</values>
</param>
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<param humanName="FlightMode6" name="ArduPlane:FLTMODE6" documentation="Flight mode for switch position 6 (1750 to 2049)" user="Standard">
<values>
<value code="0">Manual</value>
<value code="1">CIRCLE</value>
<value code="2">STABILIZE</value>
<value code="3">TRAINING</value>
<value code="4">ACRO</value>
<value code="5">FBWA</value>
<value code="6">FBWB</value>
<value code="7">CRUISE</value>
<value code="8">AUTOTUNE</value>
<value code="10">Auto</value>
<value code="11">RTL</value>
<value code="12">Loiter</value>
<value code="14">AVOID_ADSB</value>
<value code="15">Guided</value>
<value code="17">QSTABILIZE</value>
<value code="18">QHOVER</value>
<value code="19">QLOITER</value>
<value code="20">QLAND</value>
<value code="21">QRTL</value>
</values>
</param>
<param humanName="Initial flight mode" name="ArduPlane:INITIAL_MODE" documentation="This selects the mode to start in on boot. This is useful for when you want to start in AUTO mode on boot without a receiver." user="Advanced">
<values>
<value code="0">Manual</value>
<value code="1">CIRCLE</value>
<value code="2">STABILIZE</value>
<value code="3">TRAINING</value>
<value code="4">ACRO</value>
<value code="5">FBWA</value>
<value code="6">FBWB</value>
<value code="7">CRUISE</value>
<value code="8">AUTOTUNE</value>
<value code="10">Auto</value>
<value code="11">RTL</value>
<value code="12">Loiter</value>
<value code="14">AVOID_ADSB</value>
<value code="15">Guided</value>
<value code="17">QSTABILIZE</value>
<value code="18">QHOVER</value>
<value code="19">QLOITER</value>
<value code="20">QLAND</value>
<value code="21">QRTL</value>
</values>
</param>
<param humanName="Maximum Bank Angle" name="ArduPlane:LIM_ROLL_CD" documentation="The maximum commanded bank angle in either direction" user="Standard">
<field name="Range">0 9000</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Maximum Pitch Angle" name="ArduPlane:LIM_PITCH_MAX" documentation="The maximum commanded pitch up angle" user="Standard">
<field name="Range">0 9000</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Minimum Pitch Angle" name="ArduPlane:LIM_PITCH_MIN" documentation="The minimum commanded pitch down angle" user="Standard">
<field name="Range">-9000 0</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="ACRO mode roll rate" name="ArduPlane:ACRO_ROLL_RATE" documentation="The maximum roll rate at full stick deflection in ACRO mode" user="Standard">
<field name="Range">10 500</field>
<field name="Increment">1</field>
<field name="Units">deg/s</field>
<field name="UnitText">degrees per second</field>
</param>
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<param humanName="ACRO mode pitch rate" name="ArduPlane:ACRO_PITCH_RATE" documentation="The maximum pitch rate at full stick deflection in ACRO mode" user="Standard">
<field name="Range">10 500</field>
<field name="Increment">1</field>
<field name="Units">deg/s</field>
<field name="UnitText">degrees per second</field>
</param>
<param humanName="ACRO mode attitude locking" name="ArduPlane:ACRO_LOCKING" documentation="Enable attitude locking when sticks are released" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Ground steer altitude" name="ArduPlane:GROUND_STEER_ALT" documentation="Altitude at which to use the ground steering controller on the rudder. If non-zero then the STEER2SRV controller will be used to control the rudder for altitudes within this limit of the home altitude." user="Standard">
<field name="Range">-100 100</field>
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Ground steer rate" name="ArduPlane:GROUND_STEER_DPS" documentation="Ground steering rate in degrees per second for full rudder stick deflection" user="Advanced">
<field name="Range">10 360</field>
<field name="Increment">1</field>
<field name="Units">deg/s</field>
<field name="UnitText">degrees per second</field>
</param>
<param humanName="Automatic trim adjustment" name="ArduPlane:TRIM_AUTO" documentation="Set RC trim PWM levels to current levels when switching away from manual mode. When this option is enabled and you change from MANUAL to any other mode then the APM will take the current position of the control sticks as the trim values for aileron, elevator and rudder. It will use those to set the SERVOn_TRIM values and the RCn_TRIM values. This option is disabled by default as if a pilot is not aware of this option and changes from MANUAL to another mode while control inputs are not centered then the trim could be changed to a dangerously bad value. You can enable this option to assist with trimming your plane, by enabling it before takeoff then switching briefly to MANUAL in flight, and seeing how the plane reacts. You can then switch back to FBWA, trim the surfaces then again test MANUAL mode. Each time you switch from MANUAL the APM will take your control inputs as the new trim. After you have good trim on your aircraft you can disable TRIM_AUTO for future flights. You should also see the newer and much safer SERVO_AUTO_TRIM parameter." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Mixing Gain" name="ArduPlane:MIXING_GAIN" documentation="The gain for the Vtail and elevon output mixers. The default is 0.5, which ensures that the mixer doesn't saturate, allowing both input channels to go to extremes while retaining control over the output. Hardware mixers often have a 1.0 gain, which gives more servo throw, but can saturate. If you don't have enough throw on your servos with VTAIL_OUTPUT or ELEVON_OUTPUT enabled then you can raise the gain using MIXING_GAIN. The mixer allows outputs in the range 900 to 2100 microseconds." user="User">
<field name="Range">0.5 1.2</field>
</param>
<param humanName="Rudder only aircraft" name="ArduPlane:RUDDER_ONLY" documentation="Enable rudder only mode. The rudder will control attitude in attitude controlled modes (such as FBWA). You should setup your transmitter to send roll stick inputs to the RCMAP_YAW channel (normally channel 4). The rudder servo should be attached to the RCMAP_YAW channel as well. Note that automatic ground steering will be disabled for rudder only aircraft. You should also set KFF_RDDRMIX to 1.0. You will also need to setup the YAW2SRV_DAMP yaw damping appropriately for your aircraft. A value of 0.5 for YAW2SRV_DAMP is a good starting point." user="User">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Mixing Offset" name="ArduPlane:MIXING_OFFSET" documentation="The offset for the Vtail and elevon output mixers, as a percentage. This can be used in combination with MIXING_GAIN to configure how the control surfaces respond to input. The response to aileron or elevator input can be increased by setting this parameter to a positive or negative value. A common usage is to enter a positive value to increase the aileron response of the elevons of a flying wing. The default value of zero will leave the aileron-input response equal to the elevator-input response." user="User">
<field name="Range">-1000 1000</field>
<field name="Units">d%</field>
<field name="UnitText">decipercent</field>
</param>
<param humanName="Differential spoilers rudder rate" name="ArduPlane:DSPOILR_RUD_RATE" documentation="Sets the amount of deflection that the rudder output will apply to the differential spoilers, as a percentage. The default value of 100 results in full rudder applying full deflection. A value of 0 will result in the differential spoilers exactly following the elevons (no rudder effect)." user="User">
<field name="Range">-100 100</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Num Resets" name="ArduPlane:SYS_NUM_RESETS" documentation="Number of APM board resets" user="Advanced">
<field name="ReadOnly">True</field>
</param>
<param humanName="Log bitmask" name="ArduPlane:LOG_BITMASK" documentation="Bitmap of what log types to enable in dataflash. This values is made up of the sum of each of the log types you want to be saved on dataflash. On a PX4 or Pixhawk the large storage size of a microSD card means it is usually best just to enable all log types by setting this to 65535. On APM2 the smaller 4 MByte dataflash means you need to be more selective in your logging or you may run out of log space while flying (in which case it will wrap and overwrite the start of the log). The individual bits are ATTITUDE_FAST=1, ATTITUDE_MEDIUM=2, GPS=4, PerformanceMonitoring=8, ControlTuning=16, NavigationTuning=32, Mode=64, IMU=128, Commands=256, Battery=512, Compass=1024, TECS=2048, Camera=4096, RCandServo=8192, Sonar=16384, Arming=32768, FullLogs=65535" user="Advanced">
<field name="Bitmask">0:ATTITUDE_FAST,1:ATTITUDE_MED,2:GPS,3:PM,4:CTUN,5:NTUN,6:MODE,7:IMU,8:CMD,9:CURRENT,10:COMPASS,11:TECS,12:CAMERA,13:RC,14:SONAR,15:ARM/DISARM,19:IMU_RAW</field>
<values>
<value code="0">Disabled</value>
<value code="65535">PX4/Pixhawk-Default</value>
</values>
</param>
<param humanName="Reset Switch Channel" name="ArduPlane:RST_SWITCH_CH" documentation="RC channel to use to reset to last flight mode	after geofence takeover." user="Advanced">
</param>
<param humanName="Reset Mission Channel" name="ArduPlane:RST_MISSION_CH" documentation="RC channel to use to reset the mission to the first waypoint. When this channel goes above 1750 the mission is reset. Set RST_MISSION_CH to 0 to disable." user="Advanced">
</param>
<param humanName="Target airspeed" name="ArduPlane:TRIM_ARSPD_CM" documentation="Airspeed in cm/s to aim for when airspeed is enabled in auto mode. This is a calibrated (apparent) airspeed." user="User">
<field name="Units">cm/s</field>
<field name="UnitText">centimeters per second</field>
</param>
<param humanName="speed used for speed scaling calculations" name="ArduPlane:SCALING_SPEED" documentation="Airspeed in m/s to use when calculating surface speed scaling. Note that changing this value will affect all PID values" user="Advanced">
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
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</param>
<param humanName="Minimum ground speed" name="ArduPlane:MIN_GNDSPD_CM" documentation="Minimum ground speed in cm/s when under airspeed control" user="Advanced">
<field name="Units">cm/s</field>
<field name="UnitText">centimeters per second</field>
</param>
<param humanName="Pitch angle offset" name="ArduPlane:TRIM_PITCH_CD" documentation="offset to add to pitch - used for in-flight pitch trimming. It is recommended that instead of using this parameter you level your plane correctly on the ground for good flight attitude." user="Advanced">
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="RTL altitude" name="ArduPlane:ALT_HOLD_RTL" documentation="Return to launch target altitude. This is the relative altitude the plane will aim for and loiter at when returning home. If this is negative (usually -1) then the plane will use the current altitude at the time of entering RTL. Note that when transiting to a Rally Point the altitude of the Rally Point is used instead of ALT_HOLD_RTL." user="User">
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Minimum altitude for FBWB mode" name="ArduPlane:ALT_HOLD_FBWCM" documentation="This is the minimum altitude in centimeters that FBWB and CRUISE modes will allow. If you attempt to descend below this altitude then the plane will level off. A value of zero means no limit." user="User">
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Enable Compass" name="ArduPlane:MAG_ENABLE" documentation="Setting this to Enabled(1) will enable the compass. Setting this to Disabled(0) will disable the compass. Note that this is separate from COMPASS_USE. This will enable the low level senor, and will enable logging of magnetometer data. To use the compass for navigation you must also set COMPASS_USE to 1." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Flap input channel" name="ArduPlane:FLAP_IN_CHANNEL" documentation="An RC input channel to use for flaps control. If this is set to a RC channel number then that channel will be used for manual flaps control. When enabled, the percentage of flaps is taken as the percentage travel from the TRIM value of the channel to the MIN value of the channel. A value above the TRIM values will give inverse flaps (spoilers). This option needs to be enabled in conjunction with a FUNCTION setting on an output channel to one of the flap functions. When a FLAP_IN_CHANNEL is combined with auto-flaps the higher of the two flap percentages is taken." user="User">
</param>
<param humanName="Flap 1 percentage" name="ArduPlane:FLAP_1_PERCNT" documentation="The percentage change in flap position when FLAP_1_SPEED is reached. Use zero to disable flaps" user="Advanced">
<field name="Range">0 100</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Flap 1 speed" name="ArduPlane:FLAP_1_SPEED" documentation="The speed in meters per second at which to engage FLAP_1_PERCENT of flaps. Note that FLAP_1_SPEED should be greater than or equal to FLAP_2_SPEED" user="Advanced">
<field name="Range">0 100</field>
<field name="Increment">1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Flap 2 percentage" name="ArduPlane:FLAP_2_PERCNT" documentation="The percentage change in flap position when FLAP_2_SPEED is reached. Use zero to disable flaps" user="Advanced">
<field name="Range">0 100</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Flap 2 speed" name="ArduPlane:FLAP_2_SPEED" documentation="The speed in meters per second at which to engage FLAP_2_PERCENT of flaps. Note that FLAP_1_SPEED should be greater than or equal to FLAP_2_SPEED" user="Advanced">
<field name="Range">0 100</field>
<field name="Increment">1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="PX4IO override channel" name="ArduPlane:OVERRIDE_CHAN" documentation="If set to a non-zero value then this is an RC input channel number to use for giving PX4IO manual control in case the main FMU microcontroller on a PX4 or Pixhawk fails. When this RC input channel goes above 1750 the FMU microcontroller will no longer be involved in controlling the servos and instead the PX4IO microcontroller will directly control the servos. Note that PX4IO manual control will be automatically activated if the FMU crashes for any reason. This parameter allows you to test for correct manual behaviour without actually crashing the FMU. This parameter is can be set to a non-zero value either for ground testing purposes or for giving the effect of an external override control board. Please also see the docs on OVERRIDE_SAFETY. Note that you may set OVERRIDE_CHAN to the same channel as FLTMODE_CH to get PX4IO based override when in flight mode 6. Note that when override is triggered due to a FMU crash the 6 auxiliary output channels on Pixhawk will no longer be updated, so all the flight controls you need must be assigned to the first 8 channels." user="Advanced">
</param>
<param humanName="PX4IO override safety switch" name="ArduPlane:OVERRIDE_SAFETY" documentation="This controls whether the safety switch is turned off when you activate override with OVERRIDE_CHAN. When set to 1 the safety switch is de-activated (activating the servos) then a PX4IO override is triggered. In that case the safety remains de-activated after override is disabled. If OVERRIDE_SAFETTY is set to 0 then the safety switch state does not change. Note that regardless of the value of this parameter the servos will be active while override is active." user="Advanced">
</param>
<param humanName="Inverted flight channel" name="ArduPlane:INVERTEDFLT_CH" documentation="A RC input channel number to enable inverted flight. If this is non-zero then the APM will monitor the corresponding RC input channel and will enable inverted flight when the channel goes above 1750." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Channel1</value>
<value code="2">Channel2</value>
<value code="3">Channel3</value>
<value code="4">Channel4</value>
<value code="5">Channel5</value>
<value code="6">Channel6</value>
<value code="7">Channel7</value>
<value code="8">Channel8</value>
</values>
</param>
<param humanName="HIL mode enable" name="ArduPlane:HIL_MODE" documentation="This enables and disables hardware in the loop mode. If HIL_MODE is 1 then on the next reboot all sensors are replaced with HIL sensors which come from the GCS." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
<field name="RebootRequired">True</field>
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</param>
<param humanName="HIL Servos enable" name="ArduPlane:HIL_SERVOS" documentation="This controls whether real servo controls are used in HIL mode. If you enable this then the APM will control the real servos in HIL mode. If disabled it will report servo values, but will not output to the real servos. Be careful that your motor and propeller are not connected if you enable this option." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Limit of error in HIL attitude before reset" name="ArduPlane:HIL_ERR_LIMIT" documentation="This controls the maximum error in degrees on any axis before HIL will reset the DCM attitude to match the HIL_STATE attitude. This limit will prevent poor timing on HIL from causing a major attitude error. If the value is zero then no limit applies." user="Advanced">
<field name="Range">0 90</field>
<field name="Increment">0.1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="RTL auto land" name="ArduPlane:RTL_AUTOLAND" documentation="Automatically begin landing sequence after arriving at RTL location. This requires the addition of a DO_LAND_START mission item, which acts as a marker for the start of a landing sequence. The closest landing sequence will be chosen to the current location. " user="Standard">
<values>
<value code="0">Disable</value>
<value code="1">Enable - go HOME then land</value>
<value code="2">Enable - go directly to landing sequence</value>
</values>
</param>
<param humanName="Crash Deceleration Threshold" name="ArduPlane:CRASH_ACC_THRESH" documentation="X-Axis deceleration threshold to notify the crash detector that there was a possible impact which helps disarm the motor quickly after a crash. This value should be much higher than normal negative x-axis forces during normal flight, check flight log files to determine the average IMU.x values for your aircraft and motor type. Higher value means less sensative (triggers on higher impact). For electric planes that don't vibrate much during fight a value of 25 is good (that's about 2.5G). For petrol/nitro planes you'll want a higher value. Set to 0 to disable the collision detector." user="Advanced">
<field name="Range">10 127</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Crash Detection" name="ArduPlane:CRASH_DETECT" documentation="Automatically detect a crash during AUTO flight and perform the bitmask selected action(s). Disarm will turn off motor for safety and to help against burning out ESC and motor. Setting the mode to manual will help save the servos from burning out by overexerting if the aircraft crashed in an odd orientation such as upsidedown. Set to 0 to disable crash detection." user="Advanced">
<field name="Bitmask">0:Disarm</field>
</param>
<param humanName="Parachute release channel" name="ArduPlane:CHUTE_CHAN" documentation="If set to a non-zero value then this is an RC input channel number to use for manually releasing the parachute. When this channel goes above 1700 the parachute will be released" user="Advanced">
</param>
<param humanName="Enable rangefinder for landing" name="ArduPlane:RNGFND_LANDING" documentation="This enables the use of a rangefinder for automatic landing. The rangefinder will be used both on the landing approach and for final flare" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="GCS sysid enforcement" name="ArduPlane:SYSID_ENFORCE" documentation="This controls whether packets from other than the expected GCS system ID will be accepted" user="Advanced">
<values>
<value code="0">NotEnforced</value>
<value code="1">Enforced</value>
</values>
</param>
<param humanName="rudder differential thrust gain" name="ArduPlane:RUDD_DT_GAIN" documentation="gain control from rudder to differential thrust" user="Standard">
<field name="Range">0 100</field>
<field name="Increment">1</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Manual R/C pass-through mask" name="ArduPlane:MANUAL_RCMASK" documentation="Mask of R/C channels to pass directly to corresponding output channel when in MANUAL mode. When in any mode except MANUAL the channels selected with this option behave normally. This parameter is designed to allow for complex mixing strategies to be used for MANUAL flight using transmitter based mixing. Note that when this option is used you need to be very careful with pre-flight checks to ensure that the output is correct both in MANUAL and non-MANUAL modes." user="Advanced">
<field name="Bitmask">0:Chan1,1:Chan2,2:Chan3,3:Chan4,4:Chan5,5:Chan6,6:Chan7,7:Chan8,8:Chan9,9:Chan10,10:Chan11,11:Chan12,12:Chan13,13:Chan14,14:Chan15,15:Chan16</field>
</param>
</parameters>
</vehicles><libraries><parameters name="ADSB_">
<param humanName="Enable ADSB" name="ADSB_ENABLE" documentation="Enable ADS-B" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="ADSB vehicle list size" name="ADSB_LIST_MAX" documentation="ADSB list size of nearest vehicles. Longer lists take longer to refresh with lower SRx_ADSB values." user="Advanced">
<field name="Range">1 100</field>
</param>
<param humanName="ADSB vehicle list radius filter" name="ADSB_LIST_RADIUS" documentation="ADSB vehicle list radius filter. Vehicles detected outside this radius will be completely ignored. They will not show up in the SRx_ADSB stream to the GCS and will not be considered in any avoidance calculations." user="Advanced">
<field name="Range">1 100000</field>
</param>
<param humanName="ICAO_ID vehicle identifaction number" name="ADSB_ICAO_ID" documentation="ICAO_ID unique vehicle identifaction number of this aircraft. This is a integer limited to 24bits. If set to 0 then one will be randomly generated. If set to -1 then static information is not sent, transceiver is assumed pre-programmed." user="Advanced">
<field name="Range">-1 16777215</field>
</param>
<param humanName="Emitter type" name="ADSB_EMIT_TYPE" documentation="ADSB classification for the type of vehicle emitting the transponder signal. Default value is 14 (UAV)." user="Advanced">
<values>
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<value code="0">NoInfo</value>
<value code="1">Light</value>
<value code="2">Small</value>
<value code="3">Large</value>
<value code="4">HighVortexlarge</value>
<value code="5">Heavy</value>
<value code="6">HighlyManuv</value>
<value code="7">Rotocraft</value>
<value code="8">RESERVED</value>
<value code="9">Glider</value>
<value code="10">LightAir</value>
<value code="11">Parachute</value>
<value code="12">UltraLight</value>
<value code="13">RESERVED</value>
<value code="14">UAV</value>
<value code="15">Space</value>
<value code="16">RESERVED</value>
<value code="17">EmergencySurface</value>
<value code="18">ServiceSurface</value>
<value code="19">PointObstacle</value>
</values>
</param>
<param humanName="Aircraft length and width" name="ADSB_LEN_WIDTH" documentation="Aircraft length and width dimension options in Length and Width in meters. In most cases, use a value of 1 for smallest size." user="Advanced">
<values>
<value code="0">NO_DATA</value>
<value code="1">L15W23</value>
<value code="2">L25W28P5</value>
<value code="3">L25W34</value>
<value code="4">L35W33</value>
<value code="5">L35W38</value>
<value code="6">L45W39P5</value>
<value code="7">L45W45</value>
<value code="8">L55W45</value>
<value code="9">L55W52</value>
<value code="10">L65W59P5</value>
<value code="11">L65W67</value>
<value code="12">L75W72P5</value>
<value code="13">L75W80</value>
<value code="14">L85W80</value>
<value code="15">L85W90</value>
</values>
</param>
<param humanName="GPS antenna lateral offset" name="ADSB_OFFSET_LAT" documentation="GPS antenna lateral offset. This describes the physical location offest from center of the GPS antenna on the aircraft." user="Advanced">
<values>
<value code="0">NoData</value>
<value code="1">Left2m</value>
<value code="2">Left4m</value>
<value code="3">Left6m</value>
<value code="4">Center</value>
<value code="5">Right2m</value>
<value code="6">Right4m</value>
<value code="7">Right6m</value>
</values>
</param>
<param humanName="GPS antenna longitudinal offset" name="ADSB_OFFSET_LON" documentation="GPS antenna longitudinal offset. This is usually set to 1, Applied By Sensor" user="Advanced">
<values>
<value code="0">NO_DATA</value>
<value code="1">AppliedBySensor</value>
</values>
</param>
<param humanName="Transceiver RF selection" name="ADSB_RF_SELECT" documentation="Transceiver RF selection for Rx enable and/or Tx enable." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Rx-Only</value>
<value code="2">Tx-Only</value>
<value code="3">Rx and Tx Enabled</value>
</values>
</param>
</parameters>
<parameters name="AFS_">
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<param humanName="Enable Advanced Failsafe" name="AFS_ENABLE" documentation="This enables the advanced failsafe system. If this is set to zero (disable) then all the other AFS options have no effect" user="Advanced">
</param>
<param humanName="Manual Pin" name="AFS_MAN_PIN" documentation="This sets a digital output pin to set high when in manual mode" user="Advanced">
</param>
<param humanName="Heartbeat Pin" name="AFS_HB_PIN" documentation="This sets a digital output pin which is cycled at 10Hz when termination is not activated. Note that if a FS_TERM_PIN is set then the heartbeat pin will continue to cycle at 10Hz when termination is activated, to allow the termination board to distinguish between autopilot crash and termination." user="Advanced">
</param>
<param humanName="Comms Waypoint" name="AFS_WP_COMMS" documentation="Waypoint number to navigate to on comms loss" user="Advanced">
</param>
<param humanName="GPS Loss Waypoint" name="AFS_GPS_LOSS" documentation="Waypoint number to navigate to on GPS lock loss" user="Advanced">
</param>
<param humanName="Force Terminate" name="AFS_TERMINATE" documentation="Can be set in flight to force termination of the heartbeat signal" user="Advanced">
</param>
<param humanName="Terminate action" name="AFS_TERM_ACTION" documentation="This can be used to force an action on flight termination. Normally this is handled by an external failsafe board, but you can setup APM to handle it here. If set to 0 (which is the default) then no extra action is taken. If set to the magic value 42 then the plane will deliberately crash itself by setting maximum throws on all surfaces, and zero throttle" user="Advanced">
</param>
<param humanName="Terminate Pin" name="AFS_TERM_PIN" documentation="This sets a digital output pin to set high on flight termination" user="Advanced">
</param>
<param humanName="AMSL limit" name="AFS_AMSL_LIMIT" documentation="This sets the AMSL (above mean sea level) altitude limit. If the pressure altitude determined by QNH exceeds this limit then flight termination will be forced. Note that this limit is in meters, whereas pressure altitude limits are often quoted in feet. A value of zero disables the pressure altitude limit." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Error margin for GPS based AMSL limit" name="AFS_AMSL_ERR_GPS" documentation="This sets margin for error in GPS derived altitude limit. This error margin is only used if the barometer has failed. If the barometer fails then the GPS will be used to enforce the AMSL_LIMIT, but this margin will be subtracted from the AMSL_LIMIT first, to ensure that even with the given amount of GPS altitude error the pressure altitude is not breached. OBC users should set this to comply with their D2 safety case. A value of -1 will mean that barometer failure will lead to immediate termination." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="QNH pressure" name="AFS_QNH_PRESSURE" documentation="This sets the QNH pressure in millibars to be used for pressure altitude in the altitude limit. A value of zero disables the altitude limit." user="Advanced">
<field name="Units">mbar</field>
<field name="UnitText">millibar</field>
</param>
<param humanName="Maximum number of GPS loss events" name="AFS_MAX_GPS_LOSS" documentation="Maximum number of GPS loss events before the aircraft stops returning to mission on GPS recovery. Use zero to allow for any number of GPS loss events." user="Advanced">
</param>
<param humanName="Maximum number of comms loss events" name="AFS_MAX_COM_LOSS" documentation="Maximum number of comms loss events before the aircraft stops returning to mission on comms recovery. Use zero to allow for any number of comms loss events." user="Advanced">
</param>
<param humanName="Enable geofence Advanced Failsafe" name="AFS_GEOFENCE" documentation="This enables the geofence part of the AFS. Will only be in effect if AFS_ENABLE is also 1" user="Advanced">
</param>
<param humanName="Enable RC Advanced Failsafe" name="AFS_RC" documentation="This enables the RC part of the AFS. Will only be in effect if AFS_ENABLE is also 1" user="Advanced">
</param>
<param humanName="Enable RC Termination only in manual control modes" name="AFS_RC_MAN_ONLY" documentation="If this parameter is set to 1, then an RC loss will only cause the plane to terminate in manual control modes. If it is 0, then the plane will terminate in any flight mode." user="Advanced">
</param>
<param humanName="Enable dual loss terminate due to failure of both GCS and GPS simultaneously" name="AFS_DUAL_LOSS" documentation='This enables the dual loss termination part of the AFS system. If this parameter is 1 and both GPS and the ground control station fail simultaneously, this will be considered a "dual loss" and cause termination.' user="Advanced">
</param>
<param humanName="RC failure time" name="AFS_RC_FAIL_TIME" documentation="This is the time in seconds in manual mode that failsafe termination will activate if RC input is lost. For the OBC rules this should be (1.5). Use 0 to disable." user="Advanced">
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
</parameters>
<parameters name="AHRS_">
<param humanName="AHRS GPS gain" name="AHRS_GPS_GAIN" documentation="This controls how much to use the GPS to correct the attitude. This should never be set to zero for a plane as it would result in the plane losing control in turns. For a plane please use the default value of 1.0." user="Advanced">
<field name="Range">0.0 1.0</field>
<field name="Increment">.01</field>
</param>
<param humanName="AHRS use GPS for navigation" name="AHRS_GPS_USE" documentation="This controls whether to use dead-reckoning or GPS based navigation. If set to 0 then the GPS won't be used for navigation, and only dead reckoning will be used. A value of zero should never be used for normal flight." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Yaw P" name="AHRS_YAW_P" documentation="This controls the weight the compass or GPS has on the heading. A higher value means the heading will track the yaw source (GPS or compass) more rapidly." user="Advanced">
<field name="Range">0.1 0.4</field>
<field name="Increment">.01</field>
</param>
<param humanName="AHRS RP_P" name="AHRS_RP_P" documentation="This controls how fast the accelerometers correct the attitude" user="Advanced">
<field name="Range">0.1 0.4</field>
<field name="Increment">.01</field>
</param>
<param humanName="Maximum wind" name="AHRS_WIND_MAX" documentation="This sets the maximum allowable difference between ground speed and airspeed. This allows the plane to cope with a failing airspeed sensor. A value of zero means to use the airspeed as is." user="Advanced">
<field name="Range">0 127</field>
<field name="Increment">1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
911
912
913
914
915
916
917
918
919
920
921
922
923
924
925
926
927
928
929
930
931
932
933
934
935
936
937
938
939
940
941
942
943
944
945
946
947
948
949
950
951
952
953
954
955
956
957
958
959
960
961
962
963
964
965
966
967
968
969
970
971
972
973
974
975
976
977
978
979
980
<param humanName="AHRS Trim Roll" name="AHRS_TRIM_X" documentation="Compensates for the roll angle difference between the control board and the frame. Positive values make the vehicle roll right." user="Standard">
<field name="Range">-0.1745 +0.1745</field>
<field name="Increment">0.01</field>
<field name="Units">rad</field>
<field name="UnitText">radians</field>
</param>
<param humanName="AHRS Trim Pitch" name="AHRS_TRIM_Y" documentation="Compensates for the pitch angle difference between the control board and the frame. Positive values make the vehicle pitch up/back." user="Standard">
<field name="Range">-0.1745 +0.1745</field>
<field name="Increment">0.01</field>
<field name="Units">rad</field>
<field name="UnitText">radians</field>
</param>
<param humanName="AHRS Trim Yaw" name="AHRS_TRIM_Z" documentation="Not Used" user="Advanced">
<field name="Range">-0.1745 +0.1745</field>
<field name="Increment">0.01</field>
<field name="Units">rad</field>
<field name="UnitText">radians</field>
</param>
<param humanName="Board Orientation" name="AHRS_ORIENTATION" documentation="Overall board orientation relative to the standard orientation for the board type. This rotates the IMU and compass readings to allow the board to be oriented in your vehicle at any 90 or 45 degree angle. This option takes affect on next boot. After changing you will need to re-level your vehicle." user="Advanced">
<values>
<value code="0">None</value>
<value code="1">Yaw45</value>
<value code="2">Yaw90</value>
<value code="3">Yaw135</value>
<value code="4">Yaw180</value>
<value code="5">Yaw225</value>
<value code="6">Yaw270</value>
<value code="7">Yaw315</value>
<value code="8">Roll180</value>
<value code="9">Roll180Yaw45</value>
<value code="10">Roll180Yaw90</value>
<value code="11">Roll180Yaw135</value>
<value code="12">Pitch180</value>
<value code="13">Roll180Yaw225</value>
<value code="14">Roll180Yaw270</value>
<value code="15">Roll180Yaw315</value>
<value code="16">Roll90</value>
<value code="17">Roll90Yaw45</value>
<value code="18">Roll90Yaw90</value>
<value code="19">Roll90Yaw135</value>
<value code="20">Roll270</value>
<value code="21">Roll270Yaw45</value>
<value code="22">Roll270Yaw90</value>
<value code="23">Roll270Yaw136</value>
<value code="24">Pitch90</value>
<value code="25">Pitch270</value>
<value code="26">Pitch180Yaw90</value>
<value code="27">Pitch180Yaw270</value>
<value code="28">Roll90Pitch90</value>
<value code="29">Roll180Pitch90</value>
<value code="30">Roll270Pitch90</value>
<value code="31">Roll90Pitch180</value>
<value code="32">Roll270Pitch180</value>
<value code="33">Roll90Pitch270</value>
<value code="34">Roll180Pitch270</value>
<value code="35">Roll270Pitch270</value>
<value code="36">Roll90Pitch180Yaw90</value>
<value code="37">Roll90Yaw270</value>
</values>
</param>
<param humanName="AHRS Velocity Complementary Filter Beta Coefficient" name="AHRS_COMP_BETA" documentation="This controls the time constant for the cross-over frequency used to fuse AHRS (airspeed and heading) and GPS data to estimate ground velocity. Time constant is 0.1/beta. A larger time constant will use GPS data less and a small time constant will use air data less." user="Advanced">
<field name="Range">0.001 0.5</field>
<field name="Increment">.01</field>
</param>
<param humanName="AHRS GPS Minimum satellites" name="AHRS_GPS_MINSATS" documentation="Minimum number of satellites visible to use GPS for velocity based corrections attitude correction. This defaults to 6, which is about the point at which the velocity numbers from a GPS become too unreliable for accurate correction of the accelerometers." user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
</param>
<param humanName="Use NavEKF Kalman filter for attitude and position estimation" name="AHRS_EKF_TYPE" documentation="This controls which NavEKF Kalman filter version is used for attitude and position estimation" user="Advanced">
<values>
981
982
983
984
985
986
987
988
989
990
991
992
993
994
995
996
997
998
999
1000
1001
1002
1003
1004
1005
1006
1007
1008
1009
1010
1011
1012
1013
1014
1015
1016
1017
1018
1019
1020
1021
1022
1023
1024
1025
1026
1027
1028
1029
1030
1031
1032
1033
1034
1035
1036
1037
1038
1039
1040
1041
1042
1043
1044
1045
1046
1047
1048
1049
1050
<value code="0">Disabled</value>
<value code="2">Enable EKF2</value>
<value code="3">Enable EKF3</value>
</values>
</param>
</parameters>
<parameters name="ARMING_">
<param humanName="Rudder Arming" name="ARMING_RUDDER" documentation="Control arm/disarm by rudder input. When enabled arming is done with right rudder, disarming with left rudder. Rudder arming only works in manual throttle modes with throttle at zero +- deadzone (RCx_DZ)" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">ArmingOnly</value>
<value code="2">ArmOrDisarm</value>
</values>
</param>
<param humanName="Require Arming Motors " name="ARMING_REQUIRE" documentation="Arming disabled until some requirements are met. If 0, there are no requirements (arm immediately). If 1, require rudder stick or GCS arming before arming motors and sends the minimum throttle PWM value to the throttle channel when disarmed. If 2, require rudder stick or GCS arming and send 0 PWM to throttle channel when disarmed. See the ARMING_CHECK_* parameters to see what checks are done before arming. Note, if setting this parameter to 0 a reboot is required to arm the plane. Also note, even with this parameter at 0, if ARMING_CHECK parameter is not also zero the plane may fail to arm throttle at boot due to a pre-arm check failure. This parameter is relevant for ArduPlane only." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">THR_MIN PWM when disarmed</value>
<value code="2">0 PWM when disarmed</value>
</values>
</param>
<param humanName="Arm Checks to Peform (bitmask)" name="ARMING_CHECK" documentation="Checks prior to arming motor. This is a bitmask of checks that will be performed before allowing arming. The default is no checks, allowing arming at any time. You can select whatever checks you prefer by adding together the values of each check type to set this parameter. For example, to only allow arming when you have GPS lock and no RC failsafe you would set ARMING_CHECK to 72. For most users it is recommended that you set this to 1 to enable all checks." user="Standard">
<field name="Bitmask">0:All,1:Barometer,2:Compass,3:GPS lock,4:INS,5:Parameters,6:RC,7:Board voltage,8:Battery Level,9:Airspeed,10:Logging Available,11:Hardware safety switch,12:GPS Configuration</field>
<values>
<value code="0">None</value>
<value code="1">All</value>
<value code="2">Barometer</value>
<value code="4">Compass</value>
<value code="8">GPS Lock</value>
<value code="16">INS(INertial Sensors - accels & gyros)</value>
<value code="32">Parameters(unused)</value>
<value code="64">RC Failsafe</value>
<value code="128">Board voltage</value>
<value code="256">Battery Level</value>
<value code="512">Airspeed</value>
<value code="1024">LoggingAvailable</value>
<value code="2048">Hardware safety switch</value>
<value code="4096">GPS configuration</value>
</values>
</param>
<param humanName="Accelerometer error threshold" name="ARMING_ACCTHRESH" documentation="Accelerometer error threshold used to determine inconsistent accelerometers. Compares this error range to other accelerometers to detect a hardware or calibration error. Lower value means tighter check and harder to pass arming check. Not all accelerometers are created equal." user="Advanced">
<field name="Range">0.25 3.0</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Arming voltage minimum on the first battery" name="ARMING_VOLT_MIN" documentation="The minimum voltage on the first battery to arm, 0 disables the check" user="Standard">
<field name="Increment">0.1 </field>
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
<param humanName="Arming voltage minimum on the second battery" name="ARMING_VOLT2_MIN" documentation="The minimum voltage on the first battery to arm, 0 disables the check" user="Standard">
<field name="Increment">0.1 </field>
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
</parameters>
<parameters name="ARSPD">
<param humanName="Airspeed type" name="ARSPD_TYPE" documentation="Type of airspeed sensor" user="Standard">
<values>
<value code="0">None</value>
<value code="1">I2C-MS4525D0</value>
<value code="2">Analog</value>
<value code="3">I2C-MS5525</value>
<value code="4">I2C-MS5525 (0x76)</value>
<value code="5">I2C-MS5525 (0x77)</value>
<value code="6">I2C-SDP3X</value>
</values>
</param>
<param humanName="Airspeed use" name="ARSPD_USE" documentation="use airspeed for flight control. When set to 0 airspeed sensor can be logged and displayed on a GCS but won't be used for flight. When set to 1 it will be logged and used. When set to 2 it will be only used when the throttle is zero, which can be useful in gliders with airspeed sensors behind a propeller" user="Standard">
<values>
1051
1052
1053
1054
1055
1056
1057
1058
1059
1060
1061
1062
1063
1064
1065
1066
1067
1068
1069
1070
1071
1072
1073
1074
1075
1076
1077
1078
1079
1080
1081
1082
1083
1084
1085
1086
1087
1088
1089
1090
1091
1092
1093
1094
1095
1096
1097
1098
1099
1100
1101
1102
1103
1104
1105
1106
1107
1108
1109
1110
1111
1112
1113
1114
1115
1116
1117
1118
1119
1120
<value code="0">Don't Use</value>
<value code="1">use</value>
<value code="2">UseWhenZeroThrottle</value>
</values>
</param>
<param humanName="Airspeed offset" name="ARSPD_OFFSET" documentation="Airspeed calibration offset" user="Advanced">
<field name="Increment">0.1</field>
</param>
<param humanName="Airspeed ratio" name="ARSPD_RATIO" documentation="Airspeed calibration ratio" user="Advanced">
<field name="Increment">0.1</field>
</param>
<param humanName="Airspeed pin" name="ARSPD_PIN" documentation="The pin number that the airspeed sensor is connected to for analog sensors. Set to 15 on the Pixhawk for the analog airspeed port. " user="Advanced">
</param>
<param humanName="Automatic airspeed ratio calibration" name="ARSPD_AUTOCAL" documentation="If this is enabled then the APM will automatically adjust the ARSPD_RATIO during flight, based upon an estimation filter using ground speed and true airspeed. The automatic calibration will save the new ratio to EEPROM every 2 minutes if it changes by more than 5%. This option should be enabled for a calibration flight then disabled again when calibration is complete. Leaving it enabled all the time is not recommended." user="Advanced">
</param>
<param humanName="Control pitot tube order" name="ARSPD_TUBE_ORDER" documentation="This parameter allows you to control whether the order in which the tubes are attached to your pitot tube matters. If you set this to 0 then the top connector on the sensor needs to be the dynamic pressure. If set to 1 then the bottom connector needs to be the dynamic pressure. If set to 2 (the default) then the airspeed driver will accept either order. The reason you may wish to specify the order is it will allow your airspeed sensor to detect if the aircraft it receiving excessive pressure on the static port, which would otherwise be seen as a positive airspeed." user="Advanced">
</param>
<param humanName="Skip airspeed calibration on startup" name="ARSPD_SKIP_CAL" documentation="This parameter allows you to skip airspeed offset calibration on startup, instead using the offset from the last calibration. This may be desirable if the offset variance between flights for your sensor is low and you want to avoid having to cover the pitot tube on each boot." user="Advanced">
<values>
<value code="0">Disable</value>
<value code="1">Enable</value>
</values>
</param>
<param humanName="The PSI range of the device" name="ARSPD_PSI_RANGE" documentation="This parameter allows you to to set the PSI (pounds per square inch) range for your sensor. You should not change this unless you examine the datasheet for your device" user="Advanced">
</param>
<param humanName="Airspeed I2C bus" name="ARSPD_BUS" documentation="The bus number of the I2C bus to look for the sensor on" user="Advanced">
<values>
<value code="0">Bus0(internal)</value>
<value code="1">Bus1(external)</value>
<value code="2">Bus2(auxillary)</value>
</values>
</param>
<param humanName="Primary airspeed sensor" name="ARSPD_PRIMARY" documentation="This selects which airspeed sensor will be the primary if multiple sensors are found" user="Advanced">
<values>
<value code="0">FirstSensor</value>
<value code="1">2ndSensor</value>
</values>
</param>
<param humanName="Second Airspeed type" name="ARSPD2_TYPE" documentation="Type of 2nd airspeed sensor" user="Standard">
<values>
<value code="0">None</value>
<value code="1">I2C-MS4525D0</value>
<value code="2">Analog</value>
<value code="3">I2C-MS5525</value>
<value code="4">I2C-SDP3X</value>
</values>
</param>
<param humanName="Enable use of 2nd airspeed sensor" name="ARSPD2_USE" documentation="use airspeed for flight control. When set to 0 airspeed sensor can be logged and displayed on a GCS but won't be used for flight. When set to 1 it will be logged and used. When set to 2 it will be only used when the throttle is zero, which can be useful in gliders with airspeed sensors behind a propeller" user="Standard">
<values>
<value code="0">Don't Use</value>
<value code="1">use</value>
<value code="2">UseWhenZeroThrottle</value>
</values>
</param>
<param humanName="Airspeed offset for 2nd airspeed sensor" name="ARSPD2_OFFSET" documentation="Airspeed calibration offset" user="Advanced">
<field name="Increment">0.1</field>
</param>
<param humanName="Airspeed ratio for 2nd airspeed sensor" name="ARSPD2_RATIO" documentation="Airspeed calibration ratio" user="Advanced">
<field name="Increment">0.1</field>
</param>
<param humanName="Airspeed pin for 2nd airspeed sensor" name="ARSPD2_PIN" documentation="The pin number that the airspeed sensor is connected to for analog sensors. Set to 15 on the Pixhawk for the analog airspeed port. " user="Advanced">
</param>
<param humanName="Automatic airspeed ratio calibration for 2nd airspeed sensor" name="ARSPD2_AUTOCAL" documentation="If this is enabled then the APM will automatically adjust the ARSPD_RATIO during flight, based upon an estimation filter using ground speed and true airspeed. The automatic calibration will save the new ratio to EEPROM every 2 minutes if it changes by more than 5%. This option should be enabled for a calibration flight then disabled again when calibration is complete. Leaving it enabled all the time is not recommended." user="Advanced">
</param>
<param humanName="Control pitot tube order of 2nd airspeed sensor" name="ARSPD2_TUBE_ORDR" documentation="This parameter allows you to control whether the order in which the tubes are attached to your pitot tube matters. If you set this to 0 then the top connector on the sensor needs to be the dynamic pressure. If set to 1 then the bottom connector needs to be the dynamic pressure. If set to 2 (the default) then the airspeed driver will accept either order. The reason you may wish to specify the order is it will allow your airspeed sensor to detect if the aircraft it receiving excessive pressure on the static port, which would otherwise be seen as a positive airspeed." user="Advanced">
</param>
<param humanName="Skip airspeed calibration on startup for 2nd sensor" name="ARSPD2_SKIP_CAL" documentation="This parameter allows you to skip airspeed offset calibration on startup, instead using the offset from the last calibration. This may be desirable if the offset variance between flights for your sensor is low and you want to avoid having to cover the pitot tube on each boot." user="Advanced">
<values>
<value code="0">Disable</value>
<value code="1">Enable</value>
1121
1122
1123
1124
1125
1126
1127
1128
1129
1130
1131
1132
1133
1134
1135
1136
1137
1138
1139
1140
1141
1142
1143
1144
1145
1146
1147
1148
1149
1150
1151
1152
1153
1154
1155
1156
1157
1158
1159
1160
1161
1162
1163
1164
1165
1166
1167
1168
1169
1170
1171
1172
1173
1174
1175
1176
1177
1178
1179
1180
1181
1182
1183
1184
1185
1186
1187
1188
1189
1190
</values>
</param>
<param humanName="The PSI range of the device for 2nd sensor" name="ARSPD2_PSI_RANGE" documentation="This parameter allows you to to set the PSI (pounds per square inch) range for your sensor. You should not change this unless you examine the datasheet for your device" user="Advanced">
</param>
<param humanName="Airspeed I2C bus for 2nd sensor" name="ARSPD2_BUS" documentation="The bus number of the I2C bus to look for the sensor on" user="Advanced">
<values>
<value code="0">Bus0(internal)</value>
<value code="1">Bus1(external)</value>
<value code="2">Bus2(auxillary)</value>
</values>
</param>
</parameters>
<parameters name="AVD_">
<param humanName="Enable Avoidance using ADSB" name="AVD_ENABLE" documentation="Enable Avoidance using ADSB" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Recovery behaviour after a fail event" name="AVD_F_RCVRY" documentation="Determines what the aircraft will do after a fail event is resolved" user="Advanced">
<values>
<value code="0">Remain in AVOID_ADSB</value>
<value code="1">Resume previous flight mode</value>
<value code="2">RTL</value>
<value code="3">Resume if AUTO else Loiter</value>
</values>
</param>
<param humanName="Maximum number of obstacles to track" name="AVD_OBS_MAX" documentation="Maximum number of obstacles to track" user="Advanced">
</param>
<param humanName="Time Horizon Warn" name="AVD_W_TIME" documentation="Aircraft velocity vectors are multiplied by this time to determine closest approach. If this results in an approach closer than W_DIST_XY or W_DIST_Z then W_ACTION is undertaken (assuming F_ACTION is not undertaken)" user="Advanced">
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Time Horizon Fail" name="AVD_F_TIME" documentation="Aircraft velocity vectors are multiplied by this time to determine closest approach. If this results in an approach closer than F_DIST_XY or F_DIST_Z then F_ACTION is undertaken" user="Advanced">
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Distance Warn XY" name="AVD_W_DIST_XY" documentation="Closest allowed projected distance before W_ACTION is undertaken" user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Distance Fail XY" name="AVD_F_DIST_XY" documentation="Closest allowed projected distance before F_ACTION is undertaken" user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Distance Warn Z" name="AVD_W_DIST_Z" documentation="Closest allowed projected distance before BEHAVIOUR_W is undertaken" user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Distance Fail Z" name="AVD_F_DIST_Z" documentation="Closest allowed projected distance before BEHAVIOUR_F is undertaken" user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
</parameters>
<parameters name="BATT">
<param humanName="Battery monitoring" name="BATT_MONITOR" documentation="Controls enabling monitoring of the battery's voltage and current" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="3">Analog Voltage Only</value>
<value code="4">Analog Voltage and Current</value>
<value code="5">Solo</value>
<value code="6">Bebop</value>
<value code="7">SMBus-Maxell</value>
</values>
</param>
<param humanName="Battery Voltage sensing pin" name="BATT_VOLT_PIN" documentation="Setting this to 0 ~ 13 will enable battery voltage sensing on pins A0 ~ A13. On the PX4-v1 it should be set to 100. On the Pixhawk, Pixracer and NAVIO boards it should be set to 2, Pixhawk2 Power2 is 13." user="Standard">
<values>
<value code="-1">Disabled</value>
<value code=" 0">A0</value>
<value code=" 1">A1</value>
1191
1192
1193
1194
1195
1196
1197
1198
1199
1200
1201
1202
1203
1204
1205
1206
1207
1208
1209
1210
1211
1212
1213
1214
1215
1216
1217
1218
1219
1220
1221
1222
1223
1224
1225
1226
1227
1228
1229
1230
1231
1232
1233
1234
1235
1236
1237
1238
1239
1240
1241
1242
1243
1244
1245
1246
1247
1248
1249
1250
1251
1252
1253
1254
1255
1256
1257
1258
1259
1260
<value code=" 2">Pixhawk/Pixracer/Navio2/Pixhawk2_PM1</value>
<value code=" 13">Pixhawk2_PM2</value>
<value code=" 100">PX4-v1</value>
</values>
</param>
<param humanName="Battery Current sensing pin" name="BATT_CURR_PIN" documentation="Setting this to 0 ~ 13 will enable battery current sensing on pins A0 ~ A13. On the PX4-v1 it should be set to 101. On the Pixhawk, Pixracer and NAVIO boards it should be set to 3, Pixhawk2 Power2 is 14." user="Standard">
<values>
<value code="-1">Disabled</value>
<value code=" 1">A1</value>
<value code=" 2">A2</value>
<value code=" 3">Pixhawk/Pixracer/Navio2/Pixhawk2_PM1</value>
<value code=" 14">Pixhawk2_PM2</value>
<value code=" 101">PX4-v1</value>
</values>
</param>
<param humanName="Voltage Multiplier" name="BATT_VOLT_MULT" documentation="Used to convert the voltage of the voltage sensing pin (BATT_VOLT_PIN) to the actual battery's voltage (pin_voltage * VOLT_MULT). For the 3DR Power brick on APM2 or Pixhawk, this should be set to 10.1. For the Pixhawk with the 3DR 4in1 ESC this should be 12.02. For the PX4 using the PX4IO power supply this should be set to 1." user="Advanced">
</param>
<param humanName="Amps per volt" name="BATT_AMP_PERVOLT" documentation="Number of amps that a 1V reading on the current sensor corresponds to. On the APM2 or Pixhawk using the 3DR Power brick this should be set to 17. For the Pixhawk with the 3DR 4in1 ESC this should be 17." user="Standard">
<field name="Units">A/V</field>
<field name="UnitText">ampere per volt</field>
</param>
<param humanName="AMP offset" name="BATT_AMP_OFFSET" documentation="Voltage offset at zero current on current sensor" user="Standard">
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
<param humanName="Battery capacity" name="BATT_CAPACITY" documentation="Capacity of the battery in mAh when full" user="Standard">
<field name="Increment">50</field>
<field name="Units">mA.h</field>
<field name="UnitText">milliampere hour</field>
</param>
<param humanName="Maximum allowed power (Watts)" name="BATT_WATT_MAX" documentation="If battery wattage (voltage * current) exceeds this value then the system will reduce max throttle (THR_MAX, TKOFF_THR_MAX and THR_MIN for reverse thrust) to satisfy this limit. This helps limit high current to low C rated batteries regardless of battery voltage. The max throttle will slowly grow back to THR_MAX (or TKOFF_THR_MAX ) and THR_MIN if demanding the current max and under the watt max. Use 0 to disable." user="Advanced">
<field name="Increment">1</field>
<field name="Units">W</field>
<field name="UnitText">watt</field>
</param>
<param humanName="Battery serial number" name="BATT_SERIAL_NUM" documentation="Battery serial number, automatically filled in for SMBus batteries, otherwise will be -1" user="Advanced">
</param>
<param humanName="Battery monitoring" name="BATT2_MONITOR" documentation="Controls enabling monitoring of the battery's voltage and current" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="3">Analog Voltage Only</value>
<value code="4">Analog Voltage and Current</value>
<value code="5">Solo</value>
<value code="6">Bebop</value>
<value code="7">SMBus-Maxell</value>
</values>
</param>
<param humanName="Battery Voltage sensing pin" name="BATT2_VOLT_PIN" documentation="Setting this to 0 ~ 13 will enable battery voltage sensing on pins A0 ~ A13. On the PX4-v1 it should be set to 100. On the Pixhawk, Pixracer and NAVIO boards it should be set to 2, Pixhawk2 Power2 is 13." user="Standard">
<values>
<value code="-1">Disabled</value>
<value code=" 0">A0</value>
<value code=" 1">A1</value>
<value code=" 2">Pixhawk/Pixracer/Navio2/Pixhawk2_PM1</value>
<value code=" 13">Pixhawk2_PM2</value>
<value code=" 100">PX4-v1</value>
</values>
</param>
<param humanName="Battery Current sensing pin" name="BATT2_CURR_PIN" documentation="Setting this to 0 ~ 13 will enable battery current sensing on pins A0 ~ A13. On the PX4-v1 it should be set to 101. On the Pixhawk, Pixracer and NAVIO boards it should be set to 3, Pixhawk2 Power2 is 14." user="Standard">
<values>
<value code="-1">Disabled</value>
<value code=" 1">A1</value>
<value code=" 2">A2</value>
<value code=" 3">Pixhawk/Pixracer/Navio2/Pixhawk2_PM1</value>
<value code=" 14">Pixhawk2_PM2</value>
<value code=" 101">PX4-v1</value>
</values>
</param>
<param humanName="Voltage Multiplier" name="BATT2_VOLT_MULT" documentation="Used to convert the voltage of the voltage sensing pin (BATT_VOLT_PIN) to the actual battery's voltage (pin_voltage * VOLT_MULT). For the 3DR Power brick on APM2 or Pixhawk, this should be set to 10.1. For the Pixhawk with the 3DR 4in1 ESC this should be 12.02. For the PX4 using the PX4IO power supply this should be set to 1." user="Advanced">
</param>
<param humanName="Amps per volt" name="BATT2_AMP_PERVOL" documentation="Number of amps that a 1V reading on the current sensor corresponds to. On the APM2 or Pixhawk using the 3DR Power brick this should be set to 17. For the Pixhawk with the 3DR 4in1 ESC this should be 17." user="Standard">
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<field name="Units">A/V</field>
<field name="UnitText">ampere per volt</field>
</param>
<param humanName="AMP offset" name="BATT2_AMP_OFFSET" documentation="Voltage offset at zero current on current sensor" user="Standard">
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
<param humanName="Battery capacity" name="BATT2_CAPACITY" documentation="Capacity of the battery in mAh when full" user="Standard">
<field name="Increment">50</field>
<field name="Units">mA.h</field>
<field name="UnitText">milliampere hour</field>
</param>
<param humanName="Maximum allowed current" name="BATT2_WATT_MAX" documentation="If battery wattage (voltage * current) exceeds this value then the system will reduce max throttle (THR_MAX, TKOFF_THR_MAX and THR_MIN for reverse thrust) to satisfy this limit. This helps limit high current to low C rated batteries regardless of battery voltage. The max throttle will slowly grow back to THR_MAX (or TKOFF_THR_MAX ) and THR_MIN if demanding the current max and under the watt max. Use 0 to disable." user="Advanced">
<field name="Increment">1</field>
<field name="Units">A</field>
<field name="UnitText">ampere</field>
</param>
<param humanName="Battery serial number" name="BATT2_SERIAL_NUM" documentation="Battery serial number, automatically filled in for SMBus batteries, otherwise will be -1" user="Advanced">
</param>
<param humanName="Low voltage timeout" name="BATT_LOW_TIMER" documentation="This is the timeout in seconds before a low voltage event will be triggered. For aircraft with low C batteries it may be necessary to raise this in order to cope with low voltage on long takeoffs. A value of zero disables low voltage errors." user="Advanced">
<field name="Range">0 120</field>
<field name="Increment">1</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Low voltage type" name="BATT_LOW_TYPE" documentation="Voltage type used for detection of low voltage event" user="Advanced">
<values>
<value code="0">Raw Voltage</value>
<value code=" 1">Sag Compensated Voltage</value>
</values>
</param>
</parameters>
<parameters name="BRD_">
<param humanName="Auxiliary pin config" name="BRD_PWM_COUNT" documentation="Control assigning of FMU pins to PWM output, timer capture and GPIO. All unassigned pins can be used for GPIO" user="Advanced">
<values>
<value code="0">No PWMs</value>
<value code="2">Two PWMs</value>
<value code="4">Four PWMs</value>
<value code="6">Six PWMs</value>
<value code="7">Three PWMs and One Capture</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Serial 1 flow control" name="BRD_SER1_RTSCTS" documentation="Enable flow control on serial 1 (telemetry 1) on Pixhawk. You must have the RTS and CTS pins connected to your radio. The standard DF13 6 pin connector for a 3DR radio does have those pins connected. If this is set to 2 then flow control will be auto-detected by checking for the output buffer filling on startup. Note that the PX4v1 does not have hardware flow control pins on this port, so you should leave this disabled." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
<value code="2">Auto</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Serial 2 flow control" name="BRD_SER2_RTSCTS" documentation="Enable flow control on serial 2 (telemetry 2) on Pixhawk and PX4. You must have the RTS and CTS pins connected to your radio. The standard DF13 6 pin connector for a 3DR radio does have those pins connected. If this is set to 2 then flow control will be auto-detected by checking for the output buffer filling on startup." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
<value code="2">Auto</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Enable use of safety arming switch" name="BRD_SAFETYENABLE" documentation="This controls the default state of the safety switch at startup. When set to 1 the safety switch will start in the safe state (flashing) at boot. When set to zero the safety switch will start in the unsafe state (solid) at startup. Note that if a safety switch is fitted the user can still control the safety state after startup using the switch. The safety state can also be controlled in software using a MAVLink message." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName=" SBUS output rate" name="BRD_SBUS_OUT" documentation="This sets the SBUS output frame rate in Hz" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">50Hz</value>
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<value code="2">75Hz</value>
<value code="3">100Hz</value>
<value code="4">150Hz</value>
<value code="5">200Hz</value>
<value code="6">250Hz</value>
<value code="7">300Hz</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="User-defined serial number" name="BRD_SERIAL_NUM" documentation="User-defined serial number of this vehicle, it can be any arbitrary number you want and has no effect on the autopilot" user="Standard">
<field name="Range">-32768 32767</field>
</param>
<param humanName="Channels to which ignore the safety switch state" name="BRD_SAFETY_MASK" documentation="A bitmask which controls what channels can move while the safety switch has not been pressed" user="Advanced">
<field name="Bitmask">0:Ch1,1:Ch2,2:Ch3,3:Ch4,4:Ch5,5:Ch6,6:Ch7,7:Ch8,8:Ch9,9:Ch10,10:Ch11,11:Ch12,12:Ch13,13:Ch14</field>
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Target IMU temperature" name="BRD_IMU_TARGTEMP" documentation="This sets the target IMU temperature for boards with controllable IMU heating units. A value of -1 disables heating." user="Advanced">
<field name="Range">-1 80</field>
<field name="Units">degC</field>
<field name="UnitText">degrees Celsius</field>
</param>
<param humanName="Board type" name="BRD_TYPE" documentation="This allows selection of a PX4 or VRBRAIN board type. If set to zero then the board type is auto-detected (PX4)" user="Advanced">
<values>
<value code="0">AUTO</value>
<value code="1">PX4V1</value>
<value code="2">Pixhawk</value>
<value code="3">Pixhawk2</value>
<value code="4">Pixracer</value>
<value code="5">PixhawkMini</value>
<value code="6">Pixhawk2Slim</value>
<value code="7">VRBrain 5.1</value>
<value code="8">VRBrain 5.2</value>
<value code="9">VR Micro Brain 5.1</value>
<value code="10">VR Micro Brain 5.2</value>
<value code="11">VRBrain Core 1.0</value>
<value code="12">VRBrain 5.4</value>
<value code="13">Intel Aero FC</value>
<value code="20">AUAV2.1</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Enable IO co-processor" name="BRD_IO_ENABLE" documentation="This allows for the IO co-processor on FMUv1 and FMUv2 to be disabled" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Options for safety button behavior" name="BRD_SAFETYOPTION" documentation="This controls the activation of the safety button. It allows you to control if the safety button can be used for safety enable and/or disable, and whether the button is only active when disarmed" user="Standard">
<field name="Bitmask">0:ActiveForSafetyEnable,1:ActiveForSafetyDisable,2:ActiveWhenDisarmed</field>
</param>
</parameters>
<parameters name="BTN_">
<param humanName="Enable button reporting" name="BTN_ENABLE" documentation="This enables the button checking module. When this is disabled the parameters for setting button inputs are not visible" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code=" 1">Enabled</value>
</values>
</param>
<param humanName="First button Pin" name="BTN_PIN1" documentation="Digital pin number for first button input. " user="Standard">
<values>
<value code="-1">Disabled</value>
<value code="50">Pixhawk AUXOUT1</value>
<value code="51">Pixhawk AUXOUT2</value>
<value code="52">Pixhawk AUXOUT3</value>
<value code="53">Pixhawk AUXOUT4</value>
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<value code="54">Pixhawk AUXOUT5</value>
<value code="55">Pixhawk AUXOUT6</value>
<value code="111">PX4 FMU Relay1</value>
<value code="112">PX4 FMU Relay2</value>
<value code="113">PX4IO Relay1</value>
<value code="114">PX4IO Relay2</value>
<value code="115">PX4IO ACC1</value>
<value code="116">PX4IO ACC2</value>
</values>
</param>
<param humanName="Second button Pin" name="BTN_PIN2" documentation="Digital pin number for second button input. " user="Standard">
<values>
<value code="-1">Disabled</value>
<value code="50">Pixhawk AUXOUT1</value>
<value code="51">Pixhawk AUXOUT2</value>
<value code="52">Pixhawk AUXOUT3</value>
<value code="53">Pixhawk AUXOUT4</value>
<value code="54">Pixhawk AUXOUT5</value>
<value code="55">Pixhawk AUXOUT6</value>
<value code="111">PX4 FMU Relay1</value>
<value code="112">PX4 FMU Relay2</value>
<value code="113">PX4IO Relay1</value>
<value code="114">PX4IO Relay2</value>
<value code="115">PX4IO ACC1</value>
<value code="116">PX4IO ACC2</value>
</values>
</param>
<param humanName="Third button Pin" name="BTN_PIN3" documentation="Digital pin number for third button input. " user="Standard">
<values>
<value code="-1">Disabled</value>
<value code="50">Pixhawk AUXOUT1</value>
<value code="51">Pixhawk AUXOUT2</value>
<value code="52">Pixhawk AUXOUT3</value>
<value code="53">Pixhawk AUXOUT4</value>
<value code="54">Pixhawk AUXOUT5</value>
<value code="55">Pixhawk AUXOUT6</value>
<value code="111">PX4 FMU Relay1</value>
<value code="112">PX4 FMU Relay2</value>
<value code="113">PX4IO Relay1</value>
<value code="114">PX4IO Relay2</value>
<value code="115">PX4IO ACC1</value>
<value code="116">PX4IO ACC2</value>
</values>
</param>
<param humanName="Fourth button Pin" name="BTN_PIN4" documentation="Digital pin number for fourth button input. " user="Standard">
<values>
<value code="-1">Disabled</value>
<value code="50">Pixhawk AUXOUT1</value>
<value code="51">Pixhawk AUXOUT2</value>
<value code="52">Pixhawk AUXOUT3</value>
<value code="53">Pixhawk AUXOUT4</value>
<value code="54">Pixhawk AUXOUT5</value>
<value code="55">Pixhawk AUXOUT6</value>
<value code="111">PX4 FMU Relay1</value>
<value code="112">PX4 FMU Relay2</value>
<value code="113">PX4IO Relay1</value>
<value code="114">PX4IO Relay2</value>
<value code="115">PX4IO ACC1</value>
<value code="116">PX4IO ACC2</value>
</values>
</param>
<param humanName="Report send time" name="BTN_REPORT_SEND" documentation="The duration in seconds that a BUTTON_CHANGE report is repeatedly sent to the GCS regarding a button changing state. Note that the BUTTON_CHANGE message is MAVLink2 only." user="Standard">
<field name="Range">0 3600</field>
</param>
</parameters>
<parameters name="CAM_">
<param humanName="Camera shutter (trigger) type" name="CAM_TRIGG_TYPE" documentation="how to trigger the camera to take a picture" user="Standard">
<values>
<value code="0">Servo</value>
<value code="1">Relay</value>
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</values>
</param>
<param humanName="Duration that shutter is held open" name="CAM_DURATION" documentation="How long the shutter will be held open in 10ths of a second (i.e. enter 10 for 1second, 50 for 5seconds)" user="Standard">
<field name="Range">0 50</field>
<field name="Units">ds</field>
<field name="UnitText">deciseconds</field>
</param>
<param humanName="Servo ON PWM value" name="CAM_SERVO_ON" documentation="PWM value in microseconds to move servo to when shutter is activated" user="Standard">
<field name="Range">1000 2000</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo OFF PWM value" name="CAM_SERVO_OFF" documentation="PWM value in microseconds to move servo to when shutter is deactivated" user="Standard">
<field name="Range">1000 2000</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Camera trigger distance" name="CAM_TRIGG_DIST" documentation="Distance in meters between camera triggers. If this value is non-zero then the camera will trigger whenever the GPS position changes by this number of meters regardless of what mode the APM is in. Note that this parameter can also be set in an auto mission using the DO_SET_CAM_TRIGG_DIST command, allowing you to enable/disable the triggering of the camera during the flight." user="Standard">
<field name="Range">0 1000</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Relay ON value" name="CAM_RELAY_ON" documentation="This sets whether the relay goes high or low when it triggers. Note that you should also set RELAY_DEFAULT appropriately for your camera" user="Standard">
<values>
<value code="0">Low</value>
<value code="1">High</value>
</values>
</param>
<param humanName="Minimum time between photos" name="CAM_MIN_INTERVAL" documentation="Postpone shooting if previous picture was taken less than preset time(ms) ago." user="Standard">
<field name="Range">0 10000</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
</param>
<param humanName="Maximum photo roll angle." name="CAM_MAX_ROLL" documentation="Postpone shooting if roll is greater than limit. (0=Disable, will shoot regardless of roll)." user="Standard">
<field name="Range">0 180</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Camera feedback pin" name="CAM_FEEDBACK_PIN" documentation="pin number to use for save accurate camera feedback messages. If set to -1 then don't use a pin flag for this, otherwise this is a pin number which if held high after a picture trigger order, will save camera messages when camera really takes a picture. A universal camera hot shoe is needed. The pin should be held high for at least 2 milliseconds for reliable trigger detection. See also the CAM_FEEDBACK_POL option. If using AUX4 pin on a Pixhawk then a fast capture method is used that allows for the trigger time to be as short as one microsecond." user="Standard">
<values>
<value code="-1">Disabled</value>
<value code="50">PX4 AUX1</value>
<value code="51">PX4 AUX2</value>
<value code="52">PX4 AUX3</value>
<value code="53">PX4 AUX4(fast capture)</value>
<value code="54">PX4 AUX5</value>
<value code="55">PX4 AUX6</value>
</values>
</param>
<param humanName="Camera feedback pin polarity" name="CAM_FEEDBACK_POL" documentation="Polarity for feedback pin. If this is 1 then the feedback pin should go high on trigger. If set to 0 then it should go low" user="Standard">
<values>
<value code="0">TriggerLow</value>
<value code="1">TriggerHigh</value>
</values>
</param>
</parameters>
<parameters name="CAN_D1_">
<param humanName="Index of virtual driver to be used with physical CAN interface" name="CAN_D1_DRIVER" documentation="Enabling this option enables use of CAN buses." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">First driver</value>
<value code="2">Second driver</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Bitrate of CAN interface" name="CAN_D1_BITRATE" documentation="Bit rate can be set up to from 10000 to 1000000" user="Advanced">
<field name="Range">10000 1000000</field>
</param>
<param humanName="Level of debug for CAN devices" name="CAN_D1_DEBUG" documentation="Enabling this option will provide debug messages" user="Advanced">
<values>
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1610
<value code="0">Disabled</value>
<value code="1">Major messages</value>
<value code="2">All messages</value>
</values>
</param>
<param humanName="Enable use of specific protocol over virtual driver" name="CAN_D1_PROTOCOL" documentation="Enabling this option starts selected protocol that will use this virtual driver" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">UAVCAN</value>
</values>
<field name="RebootRequired">True</field>
</param>
</parameters>
<parameters name="CAN_D1_UC_">
<param humanName="UAVCAN node that is used for this network" name="CAN_D1_UC_NODE" documentation="UAVCAN node should be set implicitly" user="Advanced">
<field name="Range">1 250</field>
</param>
<param humanName="RC Out channels to be transmitted as servo over UAVCAN" name="CAN_D1_UC_SRV_BM" documentation="Bitmask with one set for channel to be transmitted as a servo command over UAVCAN" user="Advanced">
<field name="Bitmask">0: Servo 1, 1: Servo 2, 2: Servo 3, 3: Servo 4, 4: Servo 5, 5: Servo 6, 6: Servo 7, 7: Servo 8, 8: Servo 9, 9: Servo 10, 10: Servo 11, 11: Servo 12, 12: Servo 13, 13: Servo 14, 14: Servo 15</field>
</param>
<param humanName="RC Out channels to be transmitted as ESC over UAVCAN" name="CAN_D1_UC_ESC_BM" documentation="Bitmask with one set for channel to be transmitted as a ESC command over UAVCAN" user="Advanced">
<field name="Bitmask">0: ESC 1, 1: ESC 2, 2: ESC 3, 3: ESC 4, 4: ESC 5, 5: ESC 6, 6: ESC 7, 7: ESC 8, 8: ESC 9, 9: ESC 10, 10: ESC 11, 11: ESC 12, 12: ESC 13, 13: ESC 14, 14: ESC 15, 15: ESC 16</field>
</param>
</parameters>
<parameters name="CAN_D2_">
<param humanName="Index of virtual driver to be used with physical CAN interface" name="CAN_D2_DRIVER" documentation="Enabling this option enables use of CAN buses." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">First driver</value>
<value code="2">Second driver</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Bitrate of CAN interface" name="CAN_D2_BITRATE" documentation="Bit rate can be set up to from 10000 to 1000000" user="Advanced">
<field name="Range">10000 1000000</field>
</param>
<param humanName="Level of debug for CAN devices" name="CAN_D2_DEBUG" documentation="Enabling this option will provide debug messages" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Major messages</value>
<value code="2">All messages</value>
</values>
</param>
<param humanName="Enable use of specific protocol over virtual driver" name="CAN_D2_PROTOCOL" documentation="Enabling this option starts selected protocol that will use this virtual driver" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">UAVCAN</value>
</values>
<field name="RebootRequired">True</field>
</param>
</parameters>
<parameters name="CAN_D2_UC_">
<param humanName="UAVCAN node that is used for this network" name="CAN_D2_UC_NODE" documentation="UAVCAN node should be set implicitly" user="Advanced">
<field name="Range">1 250</field>
</param>
<param humanName="RC Out channels to be transmitted as servo over UAVCAN" name="CAN_D2_UC_SRV_BM" documentation="Bitmask with one set for channel to be transmitted as a servo command over UAVCAN" user="Advanced">
<field name="Bitmask">0: Servo 1, 1: Servo 2, 2: Servo 3, 3: Servo 4, 4: Servo 5, 5: Servo 6, 6: Servo 7, 7: Servo 8, 8: Servo 9, 9: Servo 10, 10: Servo 11, 11: Servo 12, 12: Servo 13, 13: Servo 14, 14: Servo 15</field>
</param>
<param humanName="RC Out channels to be transmitted as ESC over UAVCAN" name="CAN_D2_UC_ESC_BM" documentation="Bitmask with one set for channel to be transmitted as a ESC command over UAVCAN" user="Advanced">
<field name="Bitmask">0: ESC 1, 1: ESC 2, 2: ESC 3, 3: ESC 4, 4: ESC 5, 5: ESC 6, 6: ESC 7, 7: ESC 8, 8: ESC 9, 9: ESC 10, 10: ESC 11, 11: ESC 12, 12: ESC 13, 13: ESC 14, 14: ESC 15, 15: ESC 16</field>
</param>
</parameters>
<parameters name="CAN_D3_">
<param humanName="Index of virtual driver to be used with physical CAN interface" name="CAN_D3_DRIVER" documentation="Enabling this option enables use of CAN buses." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">First driver</value>
<value code="2">Second driver</value>
</values>
<field name="RebootRequired">True</field>
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</param>
<param humanName="Bitrate of CAN interface" name="CAN_D3_BITRATE" documentation="Bit rate can be set up to from 10000 to 1000000" user="Advanced">
<field name="Range">10000 1000000</field>
</param>
<param humanName="Level of debug for CAN devices" name="CAN_D3_DEBUG" documentation="Enabling this option will provide debug messages" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Major messages</value>
<value code="2">All messages</value>
</values>
</param>
<param humanName="Enable use of specific protocol over virtual driver" name="CAN_D3_PROTOCOL" documentation="Enabling this option starts selected protocol that will use this virtual driver" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">UAVCAN</value>
</values>
<field name="RebootRequired">True</field>
</param>
</parameters>
<parameters name="CAN_D3_UC_">
<param humanName="UAVCAN node that is used for this network" name="CAN_D3_UC_NODE" documentation="UAVCAN node should be set implicitly" user="Advanced">
<field name="Range">1 250</field>
</param>
<param humanName="RC Out channels to be transmitted as servo over UAVCAN" name="CAN_D3_UC_SRV_BM" documentation="Bitmask with one set for channel to be transmitted as a servo command over UAVCAN" user="Advanced">
<field name="Bitmask">0: Servo 1, 1: Servo 2, 2: Servo 3, 3: Servo 4, 4: Servo 5, 5: Servo 6, 6: Servo 7, 7: Servo 8, 8: Servo 9, 9: Servo 10, 10: Servo 11, 11: Servo 12, 12: Servo 13, 13: Servo 14, 14: Servo 15</field>
</param>
<param humanName="RC Out channels to be transmitted as ESC over UAVCAN" name="CAN_D3_UC_ESC_BM" documentation="Bitmask with one set for channel to be transmitted as a ESC command over UAVCAN" user="Advanced">
<field name="Bitmask">0: ESC 1, 1: ESC 2, 2: ESC 3, 3: ESC 4, 4: ESC 5, 5: ESC 6, 6: ESC 7, 7: ESC 8, 8: ESC 9, 9: ESC 10, 10: ESC 11, 11: ESC 12, 12: ESC 13, 13: ESC 14, 14: ESC 15, 15: ESC 16</field>
</param>
</parameters>
<parameters name="CAN_P1_">
<param humanName="Index of virtual driver to be used with physical CAN interface" name="CAN_P1_DRIVER" documentation="Enabling this option enables use of CAN buses." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">First driver</value>
<value code="2">Second driver</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Bitrate of CAN interface" name="CAN_P1_BITRATE" documentation="Bit rate can be set up to from 10000 to 1000000" user="Advanced">
<field name="Range">10000 1000000</field>
</param>
<param humanName="Level of debug for CAN devices" name="CAN_P1_DEBUG" documentation="Enabling this option will provide debug messages" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Major messages</value>
<value code="2">All messages</value>
</values>
</param>
<param humanName="Enable use of specific protocol over virtual driver" name="CAN_P1_PROTOCOL" documentation="Enabling this option starts selected protocol that will use this virtual driver" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">UAVCAN</value>
</values>
<field name="RebootRequired">True</field>
</param>
</parameters>
<parameters name="CAN_P1_UC_">
<param humanName="UAVCAN node that is used for this network" name="CAN_P1_UC_NODE" documentation="UAVCAN node should be set implicitly" user="Advanced">
<field name="Range">1 250</field>
</param>
<param humanName="RC Out channels to be transmitted as servo over UAVCAN" name="CAN_P1_UC_SRV_BM" documentation="Bitmask with one set for channel to be transmitted as a servo command over UAVCAN" user="Advanced">
<field name="Bitmask">0: Servo 1, 1: Servo 2, 2: Servo 3, 3: Servo 4, 4: Servo 5, 5: Servo 6, 6: Servo 7, 7: Servo 8, 8: Servo 9, 9: Servo 10, 10: Servo 11, 11: Servo 12, 12: Servo 13, 13: Servo 14, 14: Servo 15</field>
</param>
<param humanName="RC Out channels to be transmitted as ESC over UAVCAN" name="CAN_P1_UC_ESC_BM" documentation="Bitmask with one set for channel to be transmitted as a ESC command over UAVCAN" user="Advanced">
<field name="Bitmask">0: ESC 1, 1: ESC 2, 2: ESC 3, 3: ESC 4, 4: ESC 5, 5: ESC 6, 6: ESC 7, 7: ESC 8, 8: ESC 9, 9: ESC 10, 10: ESC 11, 11: ESC 12, 12: ESC 13, 13: ESC 14, 14: ESC 15, 15: ESC 16</field>
</param>
</parameters>
<parameters name="CAN_P2_">
<param humanName="Index of virtual driver to be used with physical CAN interface" name="CAN_P2_DRIVER" documentation="Enabling this option enables use of CAN buses." user="Standard">
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<values>
<value code="0">Disabled</value>
<value code="1">First driver</value>
<value code="2">Second driver</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Bitrate of CAN interface" name="CAN_P2_BITRATE" documentation="Bit rate can be set up to from 10000 to 1000000" user="Advanced">
<field name="Range">10000 1000000</field>
</param>
<param humanName="Level of debug for CAN devices" name="CAN_P2_DEBUG" documentation="Enabling this option will provide debug messages" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Major messages</value>
<value code="2">All messages</value>
</values>
</param>
<param humanName="Enable use of specific protocol over virtual driver" name="CAN_P2_PROTOCOL" documentation="Enabling this option starts selected protocol that will use this virtual driver" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">UAVCAN</value>
</values>
<field name="RebootRequired">True</field>
</param>
</parameters>
<parameters name="CAN_P2_UC_">
<param humanName="UAVCAN node that is used for this network" name="CAN_P2_UC_NODE" documentation="UAVCAN node should be set implicitly" user="Advanced">
<field name="Range">1 250</field>
</param>
<param humanName="RC Out channels to be transmitted as servo over UAVCAN" name="CAN_P2_UC_SRV_BM" documentation="Bitmask with one set for channel to be transmitted as a servo command over UAVCAN" user="Advanced">
<field name="Bitmask">0: Servo 1, 1: Servo 2, 2: Servo 3, 3: Servo 4, 4: Servo 5, 5: Servo 6, 6: Servo 7, 7: Servo 8, 8: Servo 9, 9: Servo 10, 10: Servo 11, 11: Servo 12, 12: Servo 13, 13: Servo 14, 14: Servo 15</field>
</param>
<param humanName="RC Out channels to be transmitted as ESC over UAVCAN" name="CAN_P2_UC_ESC_BM" documentation="Bitmask with one set for channel to be transmitted as a ESC command over UAVCAN" user="Advanced">
<field name="Bitmask">0: ESC 1, 1: ESC 2, 2: ESC 3, 3: ESC 4, 4: ESC 5, 5: ESC 6, 6: ESC 7, 7: ESC 8, 8: ESC 9, 9: ESC 10, 10: ESC 11, 11: ESC 12, 12: ESC 13, 13: ESC 14, 14: ESC 15, 15: ESC 16</field>
</param>
</parameters>
<parameters name="CAN_P3_">
<param humanName="Index of virtual driver to be used with physical CAN interface" name="CAN_P3_DRIVER" documentation="Enabling this option enables use of CAN buses." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">First driver</value>
<value code="2">Second driver</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Bitrate of CAN interface" name="CAN_P3_BITRATE" documentation="Bit rate can be set up to from 10000 to 1000000" user="Advanced">
<field name="Range">10000 1000000</field>
</param>
<param humanName="Level of debug for CAN devices" name="CAN_P3_DEBUG" documentation="Enabling this option will provide debug messages" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Major messages</value>
<value code="2">All messages</value>
</values>
</param>
<param humanName="Enable use of specific protocol over virtual driver" name="CAN_P3_PROTOCOL" documentation="Enabling this option starts selected protocol that will use this virtual driver" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">UAVCAN</value>
</values>
<field name="RebootRequired">True</field>
</param>
</parameters>
<parameters name="CAN_P3_UC_">
<param humanName="UAVCAN node that is used for this network" name="CAN_P3_UC_NODE" documentation="UAVCAN node should be set implicitly" user="Advanced">
<field name="Range">1 250</field>
</param>
<param humanName="RC Out channels to be transmitted as servo over UAVCAN" name="CAN_P3_UC_SRV_BM" documentation="Bitmask with one set for channel to be transmitted as a servo command over UAVCAN" user="Advanced">
<field name="Bitmask">0: Servo 1, 1: Servo 2, 2: Servo 3, 3: Servo 4, 4: Servo 5, 5: Servo 6, 6: Servo 7, 7: Servo 8, 8: Servo 9, 9: Servo 10, 10: Servo 11, 11: Servo 12, 12: Servo 13, 13: Servo 14, 14: Servo 15</field>
</param>
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<param humanName="RC Out channels to be transmitted as ESC over UAVCAN" name="CAN_P3_UC_ESC_BM" documentation="Bitmask with one set for channel to be transmitted as a ESC command over UAVCAN" user="Advanced">
<field name="Bitmask">0: ESC 1, 1: ESC 2, 2: ESC 3, 3: ESC 4, 4: ESC 5, 5: ESC 6, 6: ESC 7, 7: ESC 8, 8: ESC 9, 9: ESC 10, 10: ESC 11, 11: ESC 12, 12: ESC 13, 13: ESC 14, 14: ESC 15, 15: ESC 16</field>
</param>
</parameters>
<parameters name="CHUTE_">
<param humanName="Parachute release enabled or disabled" name="CHUTE_ENABLED" documentation="Parachute release enabled or disabled" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Parachute release mechanism type (relay or servo)" name="CHUTE_TYPE" documentation="Parachute release mechanism type (relay or servo)" user="Standard">
<values>
<value code="0">First Relay</value>
<value code="1">Second Relay</value>
<value code="2">Third Relay</value>
<value code="3">Fourth Relay</value>
<value code="10">Servo</value>
</values>
</param>
<param humanName="Parachute Servo ON PWM value" name="CHUTE_SERVO_ON" documentation="Parachute Servo PWM value in microseconds when parachute is released" user="Standard">
<field name="Range">1000 2000</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo OFF PWM value" name="CHUTE_SERVO_OFF" documentation="Parachute Servo PWM value in microseconds when parachute is not released" user="Standard">
<field name="Range">1000 2000</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Parachute min altitude in meters above home" name="CHUTE_ALT_MIN" documentation="Parachute min altitude above home. Parachute will not be released below this altitude. 0 to disable alt check." user="Standard">
<field name="Range">0 32000</field>
<field name="Increment">1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Parachute release delay" name="CHUTE_DELAY_MS" documentation="Delay in millseconds between motor stop and chute release" user="Standard">
<field name="Range">0 5000</field>
<field name="Increment">1</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
</param>
</parameters>
<parameters name="COMPASS_">
<param humanName="Compass offsets in milligauss on the X axis" name="COMPASS_OFS_X" documentation="Offset to be added to the compass x-axis values to compensate for metal in the frame" user="Advanced">
<field name="Range">-400 400</field>
<field name="Increment">1</field>
<field name="Units">mGauss</field>
<field name="UnitText">milligauss</field>
</param>
<param humanName="Compass offsets in milligauss on the Y axis" name="COMPASS_OFS_Y" documentation="Offset to be added to the compass y-axis values to compensate for metal in the frame" user="Advanced">
<field name="Range">-400 400</field>
<field name="Increment">1</field>
<field name="Units">mGauss</field>
<field name="UnitText">milligauss</field>
</param>
<param humanName="Compass offsets in milligauss on the Z axis" name="COMPASS_OFS_Z" documentation="Offset to be added to the compass z-axis values to compensate for metal in the frame" user="Advanced">
<field name="Range">-400 400</field>
<field name="Increment">1</field>
<field name="Units">mGauss</field>
<field name="UnitText">milligauss</field>
</param>
<param humanName="Compass declination" name="COMPASS_DEC" documentation="An angle to compensate between the true north and magnetic north" user="Standard">
<field name="Range">-3.142 3.142</field>
<field name="Increment">0.01</field>
<field name="Units">rad</field>
<field name="UnitText">radians</field>
</param>
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<param humanName="Learn compass offsets automatically" name="COMPASS_LEARN" documentation="Enable or disable the automatic learning of compass offsets. You can enable learning either using a compass-only method that is suitable only for fixed wing aircraft or using the offsets learnt by the active EKF state estimator. If this option is enabled then the learnt offsets are saved when you disarm the vehicle." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Internal-Learning</value>
<value code="2">EKF-Learning</value>
</values>
</param>
<param humanName="Use compass for yaw" name="COMPASS_USE" documentation="Enable or disable the use of the compass (instead of the GPS) for determining heading" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Auto Declination" name="COMPASS_AUTODEC" documentation="Enable or disable the automatic calculation of the declination based on gps location" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Motor interference compensation type" name="COMPASS_MOTCT" documentation="Set motor interference compensation type to disabled, throttle or current. Do not change manually." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Use Throttle</value>
<value code="2">Use Current</value>
</values>
</param>
<param humanName="Motor interference compensation for body frame X axis" name="COMPASS_MOT_X" documentation="Multiplied by the current throttle and added to the compass's x-axis values to compensate for motor interference (Offset per Amp or at Full Throttle)" user="Advanced">
<field name="Range">-1000 1000</field>
<field name="Increment">1</field>
<field name="Units">mGauss/A</field>
<field name="UnitText">milligauss per ampere</field>
</param>
<param humanName="Motor interference compensation for body frame Y axis" name="COMPASS_MOT_Y" documentation="Multiplied by the current throttle and added to the compass's y-axis values to compensate for motor interference (Offset per Amp or at Full Throttle)" user="Advanced">
<field name="Range">-1000 1000</field>
<field name="Increment">1</field>
<field name="Units">mGauss/A</field>
<field name="UnitText">milligauss per ampere</field>
</param>
<param humanName="Motor interference compensation for body frame Z axis" name="COMPASS_MOT_Z" documentation="Multiplied by the current throttle and added to the compass's z-axis values to compensate for motor interference (Offset per Amp or at Full Throttle)" user="Advanced">
<field name="Range">-1000 1000</field>
<field name="Increment">1</field>
<field name="Units">mGauss/A</field>
<field name="UnitText">milligauss per ampere</field>
</param>
<param humanName="Compass orientation" name="COMPASS_ORIENT" documentation="The orientation of the compass relative to the autopilot board. This will default to the right value for each board type, but can be changed if you have an external compass. See the documentation for your external compass for the right value. The correct orientation should give the X axis forward, the Y axis to the right and the Z axis down. So if your aircraft is pointing west it should show a positive value for the Y axis, and a value close to zero for the X axis. On a PX4 or Pixhawk with an external compass the correct value is zero if the compass is correctly oriented. NOTE: This orientation is combined with any AHRS_ORIENTATION setting." user="Advanced">
<values>
<value code="0">None</value>
<value code="1">Yaw45</value>
<value code="2">Yaw90</value>
<value code="3">Yaw135</value>
<value code="4">Yaw180</value>
<value code="5">Yaw225</value>
<value code="6">Yaw270</value>
<value code="7">Yaw315</value>
<value code="8">Roll180</value>
<value code="9">Roll180Yaw45</value>
<value code="10">Roll180Yaw90</value>
<value code="11">Roll180Yaw135</value>
<value code="12">Pitch180</value>
<value code="13">Roll180Yaw225</value>
<value code="14">Roll180Yaw270</value>
<value code="15">Roll180Yaw315</value>
<value code="16">Roll90</value>
<value code="17">Roll90Yaw45</value>
<value code="18">Roll90Yaw90</value>
<value code="19">Roll90Yaw135</value>
<value code="20">Roll270</value>
<value code="21">Roll270Yaw45</value>
<value code="22">Roll270Yaw90</value>
<value code="23">Roll270Yaw136</value>
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<value code="24">Pitch90</value>
<value code="25">Pitch270</value>
<value code="26">Pitch180Yaw90</value>
<value code="27">Pitch180Yaw270</value>
<value code="28">Roll90Pitch90</value>
<value code="29">Roll180Pitch90</value>
<value code="30">Roll270Pitch90</value>
<value code="31">Roll90Pitch180</value>
<value code="32">Roll270Pitch180</value>
<value code="33">Roll90Pitch270</value>
<value code="34">Roll180Pitch270</value>
<value code="35">Roll270Pitch270</value>
<value code="36">Roll90Pitch180Yaw90</value>
<value code="37">Roll90Yaw270</value>
<value code="38">Yaw293Pitch68Roll90</value>
</values>
</param>
<param humanName="Compass is attached via an external cable" name="COMPASS_EXTERNAL" documentation="Configure compass so it is attached externally. This is auto-detected on PX4 and Pixhawk. Set to 1 if the compass is externally connected. When externally connected the COMPASS_ORIENT option operates independently of the AHRS_ORIENTATION board orientation option. If set to 0 or 1 then auto-detection by bus connection can override the value. If set to 2 then auto-detection will be disabled." user="Advanced">
<values>
<value code="0">Internal</value>
<value code="1">External</value>
<value code="2">ForcedExternal</value>
</values>
</param>
<param humanName="Compass2 offsets in milligauss on the X axis" name="COMPASS_OFS2_X" documentation="Offset to be added to compass2's x-axis values to compensate for metal in the frame" user="Advanced">
<field name="Range">-400 400</field>
<field name="Increment">1</field>
<field name="Units">mGauss</field>
<field name="UnitText">milligauss</field>
</param>
<param humanName="Compass2 offsets in milligauss on the Y axis" name="COMPASS_OFS2_Y" documentation="Offset to be added to compass2's y-axis values to compensate for metal in the frame" user="Advanced">
<field name="Range">-400 400</field>
<field name="Increment">1</field>
<field name="Units">mGauss</field>
<field name="UnitText">milligauss</field>
</param>
<param humanName="Compass2 offsets in milligauss on the Z axis" name="COMPASS_OFS2_Z" documentation="Offset to be added to compass2's z-axis values to compensate for metal in the frame" user="Advanced">
<field name="Range">-400 400</field>
<field name="Increment">1</field>
<field name="Units">mGauss</field>
<field name="UnitText">milligauss</field>
</param>
<param humanName="Motor interference compensation to compass2 for body frame X axis" name="COMPASS_MOT2_X" documentation="Multiplied by the current throttle and added to compass2's x-axis values to compensate for motor interference (Offset per Amp or at Full Throttle)" user="Advanced">
<field name="Range">-1000 1000</field>
<field name="Increment">1</field>
<field name="Units">mGauss/A</field>
<field name="UnitText">milligauss per ampere</field>
</param>
<param humanName="Motor interference compensation to compass2 for body frame Y axis" name="COMPASS_MOT2_Y" documentation="Multiplied by the current throttle and added to compass2's y-axis values to compensate for motor interference (Offset per Amp or at Full Throttle)" user="Advanced">
<field name="Range">-1000 1000</field>
<field name="Increment">1</field>
<field name="Units">mGauss/A</field>
<field name="UnitText">milligauss per ampere</field>
</param>
<param humanName="Motor interference compensation to compass2 for body frame Z axis" name="COMPASS_MOT2_Z" documentation="Multiplied by the current throttle and added to compass2's z-axis values to compensate for motor interference (Offset per Amp or at Full Throttle)" user="Advanced">
<field name="Range">-1000 1000</field>
<field name="Increment">1</field>
<field name="Units">mGauss/A</field>
<field name="UnitText">milligauss per ampere</field>
</param>
<param humanName="Choose primary compass" name="COMPASS_PRIMARY" documentation="If more than one compass is available this selects which compass is the primary. Normally 0=External, 1=Internal. If no External compass is attached this parameter is ignored" user="Advanced">
<values>
<value code="0">FirstCompass</value>
<value code="1">SecondCompass</value>
<value code="2">ThirdCompass</value>
</values>
</param>
<param humanName="Compass3 offsets in milligauss on the X axis" name="COMPASS_OFS3_X" documentation="Offset to be added to compass3's x-axis values to compensate for metal in the frame" user="Advanced">
<field name="Range">-400 400</field>
<field name="Increment">1</field>
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<field name="Units">mGauss</field>
<field name="UnitText">milligauss</field>
</param>
<param humanName="Compass3 offsets in milligauss on the Y axis" name="COMPASS_OFS3_Y" documentation="Offset to be added to compass3's y-axis values to compensate for metal in the frame" user="Advanced">
<field name="Range">-400 400</field>
<field name="Increment">1</field>
<field name="Units">mGauss</field>
<field name="UnitText">milligauss</field>
</param>
<param humanName="Compass3 offsets in milligauss on the Z axis" name="COMPASS_OFS3_Z" documentation="Offset to be added to compass3's z-axis values to compensate for metal in the frame" user="Advanced">
<field name="Range">-400 400</field>
<field name="Increment">1</field>
<field name="Units">mGauss</field>
<field name="UnitText">milligauss</field>
</param>
<param humanName="Motor interference compensation to compass3 for body frame X axis" name="COMPASS_MOT3_X" documentation="Multiplied by the current throttle and added to compass3's x-axis values to compensate for motor interference (Offset per Amp or at Full Throttle)" user="Advanced">
<field name="Range">-1000 1000</field>
<field name="Increment">1</field>
<field name="Units">mGauss/A</field>
<field name="UnitText">milligauss per ampere</field>
</param>
<param humanName="Motor interference compensation to compass3 for body frame Y axis" name="COMPASS_MOT3_Y" documentation="Multiplied by the current throttle and added to compass3's y-axis values to compensate for motor interference (Offset per Amp or at Full Throttle)" user="Advanced">
<field name="Range">-1000 1000</field>
<field name="Increment">1</field>
<field name="Units">mGauss/A</field>
<field name="UnitText">milligauss per ampere</field>
</param>
<param humanName="Motor interference compensation to compass3 for body frame Z axis" name="COMPASS_MOT3_Z" documentation="Multiplied by the current throttle and added to compass3's z-axis values to compensate for motor interference (Offset per Amp or at Full Throttle)" user="Advanced">
<field name="Range">-1000 1000</field>
<field name="Increment">1</field>
<field name="Units">mGauss/A</field>
<field name="UnitText">milligauss per ampere</field>
</param>
<param humanName="Compass device id" name="COMPASS_DEV_ID" documentation="Compass device id. Automatically detected, do not set manually" user="Advanced">
</param>
<param humanName="Compass2 device id" name="COMPASS_DEV_ID2" documentation="Second compass's device id. Automatically detected, do not set manually" user="Advanced">
</param>
<param humanName="Compass3 device id" name="COMPASS_DEV_ID3" documentation="Third compass's device id. Automatically detected, do not set manually" user="Advanced">
</param>
<param humanName="Compass2 used for yaw" name="COMPASS_USE2" documentation="Enable or disable the second compass for determining heading." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Compass2 orientation" name="COMPASS_ORIENT2" documentation="The orientation of the second compass relative to the frame (if external) or autopilot board (if internal)." user="Advanced">
<values>
<value code="0">None</value>
<value code="1">Yaw45</value>
<value code="2">Yaw90</value>
<value code="3">Yaw135</value>
<value code="4">Yaw180</value>
<value code="5">Yaw225</value>
<value code="6">Yaw270</value>
<value code="7">Yaw315</value>
<value code="8">Roll180</value>
<value code="9">Roll180Yaw45</value>
<value code="10">Roll180Yaw90</value>
<value code="11">Roll180Yaw135</value>
<value code="12">Pitch180</value>
<value code="13">Roll180Yaw225</value>
<value code="14">Roll180Yaw270</value>
<value code="15">Roll180Yaw315</value>
<value code="16">Roll90</value>
<value code="17">Roll90Yaw45</value>
<value code="18">Roll90Yaw90</value>
<value code="19">Roll90Yaw135</value>
<value code="20">Roll270</value>
<value code="21">Roll270Yaw45</value>
<value code="22">Roll270Yaw90</value>
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<value code="23">Roll270Yaw136</value>
<value code="24">Pitch90</value>
<value code="25">Pitch270</value>
<value code="26">Pitch180Yaw90</value>
<value code="27">Pitch180Yaw270</value>
<value code="28">Roll90Pitch90</value>
<value code="29">Roll180Pitch90</value>
<value code="30">Roll270Pitch90</value>
<value code="31">Roll90Pitch180</value>
<value code="32">Roll270Pitch180</value>
<value code="33">Roll90Pitch270</value>
<value code="34">Roll180Pitch270</value>
<value code="35">Roll270Pitch270</value>
<value code="36">Roll90Pitch180Yaw90</value>
<value code="37">Roll90Yaw270</value>
<value code="38">Yaw293Pitch68Roll90</value>
</values>
</param>
<param humanName="Compass2 is attached via an external cable" name="COMPASS_EXTERN2" documentation="Configure second compass so it is attached externally. This is auto-detected on PX4 and Pixhawk. If set to 0 or 1 then auto-detection by bus connection can override the value. If set to 2 then auto-detection will be disabled." user="Advanced">
<values>
<value code="0">Internal</value>
<value code="1">External</value>
<value code="2">ForcedExternal</value>
</values>
</param>
<param humanName="Compass3 used for yaw" name="COMPASS_USE3" documentation="Enable or disable the third compass for determining heading." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Compass3 orientation" name="COMPASS_ORIENT3" documentation="The orientation of the third compass relative to the frame (if external) or autopilot board (if internal)." user="Advanced">
<values>
<value code="0">None</value>
<value code="1">Yaw45</value>
<value code="2">Yaw90</value>
<value code="3">Yaw135</value>
<value code="4">Yaw180</value>
<value code="5">Yaw225</value>
<value code="6">Yaw270</value>
<value code="7">Yaw315</value>
<value code="8">Roll180</value>
<value code="9">Roll180Yaw45</value>
<value code="10">Roll180Yaw90</value>
<value code="11">Roll180Yaw135</value>
<value code="12">Pitch180</value>
<value code="13">Roll180Yaw225</value>
<value code="14">Roll180Yaw270</value>
<value code="15">Roll180Yaw315</value>
<value code="16">Roll90</value>
<value code="17">Roll90Yaw45</value>
<value code="18">Roll90Yaw90</value>
<value code="19">Roll90Yaw135</value>
<value code="20">Roll270</value>
<value code="21">Roll270Yaw45</value>
<value code="22">Roll270Yaw90</value>
<value code="23">Roll270Yaw136</value>
<value code="24">Pitch90</value>
<value code="25">Pitch270</value>
<value code="26">Pitch180Yaw90</value>
<value code="27">Pitch180Yaw270</value>
<value code="28">Roll90Pitch90</value>
<value code="29">Roll180Pitch90</value>
<value code="30">Roll270Pitch90</value>
<value code="31">Roll90Pitch180</value>
<value code="32">Roll270Pitch180</value>
<value code="33">Roll90Pitch270</value>
<value code="34">Roll180Pitch270</value>
<value code="35">Roll270Pitch270</value>
<value code="36">Roll90Pitch180Yaw90</value>
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<value code="37">Roll90Yaw270</value>
<value code="38">Yaw293Pitch68Roll90</value>
</values>
</param>
<param humanName="Compass3 is attached via an external cable" name="COMPASS_EXTERN3" documentation="Configure third compass so it is attached externally. This is auto-detected on PX4 and Pixhawk. If set to 0 or 1 then auto-detection by bus connection can override the value. If set to 2 then auto-detection will be disabled." user="Advanced">
<values>
<value code="0">Internal</value>
<value code="1">External</value>
<value code="2">ForcedExternal</value>
</values>
</param>
<param humanName="Compass soft-iron diagonal X component" name="COMPASS_DIA_X" documentation="DIA_X in the compass soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass soft-iron diagonal Y component" name="COMPASS_DIA_Y" documentation="DIA_Y in the compass soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass soft-iron diagonal Z component" name="COMPASS_DIA_Z" documentation="DIA_Z in the compass soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass soft-iron off-diagonal X component" name="COMPASS_ODI_X" documentation="ODI_X in the compass soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass soft-iron off-diagonal Y component" name="COMPASS_ODI_Y" documentation="ODI_Y in the compass soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass soft-iron off-diagonal Z component" name="COMPASS_ODI_Z" documentation="ODI_Z in the compass soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass2 soft-iron diagonal X component" name="COMPASS_DIA2_X" documentation="DIA_X in the compass2 soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass2 soft-iron diagonal Y component" name="COMPASS_DIA2_Y" documentation="DIA_Y in the compass2 soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass2 soft-iron diagonal Z component" name="COMPASS_DIA2_Z" documentation="DIA_Z in the compass2 soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass2 soft-iron off-diagonal X component" name="COMPASS_ODI2_X" documentation="ODI_X in the compass2 soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass2 soft-iron off-diagonal Y component" name="COMPASS_ODI2_Y" documentation="ODI_Y in the compass2 soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass2 soft-iron off-diagonal Z component" name="COMPASS_ODI2_Z" documentation="ODI_Z in the compass2 soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass3 soft-iron diagonal X component" name="COMPASS_DIA3_X" documentation="DIA_X in the compass3 soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass3 soft-iron diagonal Y component" name="COMPASS_DIA3_Y" documentation="DIA_Y in the compass3 soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass3 soft-iron diagonal Z component" name="COMPASS_DIA3_Z" documentation="DIA_Z in the compass3 soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass3 soft-iron off-diagonal X component" name="COMPASS_ODI3_X" documentation="ODI_X in the compass3 soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass3 soft-iron off-diagonal Y component" name="COMPASS_ODI3_Y" documentation="ODI_Y in the compass3 soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass3 soft-iron off-diagonal Z component" name="COMPASS_ODI3_Z" documentation="ODI_Z in the compass3 soft-iron calibration matrix: [[DIA_X, ODI_X, ODI_Y], [ODI_X, DIA_Y, ODI_Z], [ODI_Y, ODI_Z, DIA_Z]]" user="Advanced">
</param>
<param humanName="Compass calibration fitness" name="COMPASS_CAL_FIT" documentation="This controls the fitness level required for a successful compass calibration. A lower value makes for a stricter fit (less likely to pass). This is the value used for the primary magnetometer. Other magnetometers get double the value." user="Advanced">
<field name="Range">4 32</field>
<values>
<value code="4">Very Strict</value>
<value code="8">Strict</value>
<value code="16">Default</value>
<value code="32">Relaxed</value>
</values>
<field name="Increment">0.1</field>
</param>
<param humanName="Compass maximum offset" name="COMPASS_OFFS_MAX" documentation="This sets the maximum allowed compass offset in calibration and arming checks" user="Advanced">
<field name="Range">500 3000</field>
<field name="Increment">1</field>
</param>
<param humanName="Compass disable driver type mask" name="COMPASS_TYPEMASK" documentation="This is a bitmask of driver types to disable. If a driver type is set in this mask then that driver will not try to find a sensor at startup" user="Advanced">
<field name="Bitmask">0:HMC5883,1:LSM303D,2:AK8963,3:BMM150,4:LSM9DS1,5:LIS3MDL,6:AK09916,7:IST8310,8:ICM20948,9:MMC3416,10:QFLIGHT,11:UAVCAN,12:QMC5883</field>
</param>
</parameters>
<parameters name="EK2_">
<param humanName="Enable EKF2" name="EK2_ENABLE" documentation="This enables EKF2. Enabling EKF2 only makes the maths run, it does not mean it will be used for flight control. To use it for flight control set AHRS_EKF_TYPE=2. A reboot or restart will need to be performed after changing the value of EK2_ENABLE for it to take effect." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code=" 1">Enabled</value>
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</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="GPS mode control" name="EK2_GPS_TYPE" documentation="This controls use of GPS measurements : 0 = use 3D velocity & 2D position, 1 = use 2D velocity and 2D position, 2 = use 2D position, 3 = Inhibit GPS use - this can be useful when flying with an optical flow sensor in an environment where GPS quality is poor and subject to large multipath errors." user="Advanced">
<values>
<value code="0">GPS 3D Vel and 2D Pos</value>
<value code=" 1">GPS 2D vel and 2D pos</value>
<value code=" 2">GPS 2D pos</value>
<value code=" 3">No GPS</value>
</values>
</param>
<param humanName="GPS horizontal velocity measurement noise (m/s)" name="EK2_VELNE_M_NSE" documentation="This sets a lower limit on the speed accuracy reported by the GPS receiver that is used to set horizontal velocity observation noise. If the model of receiver used does not provide a speed accurcy estimate, then the parameter value will be used. Increasing it reduces the weighting of the GPS horizontal velocity measurements." user="Advanced">
<field name="Range">0.05 5.0</field>
<field name="Increment">0.05</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="GPS vertical velocity measurement noise (m/s)" name="EK2_VELD_M_NSE" documentation="This sets a lower limit on the speed accuracy reported by the GPS receiver that is used to set vertical velocity observation noise. If the model of receiver used does not provide a speed accurcy estimate, then the parameter value will be used. Increasing it reduces the weighting of the GPS vertical velocity measurements." user="Advanced">
<field name="Range">0.05 5.0</field>
<field name="Increment">0.05</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="GPS velocity innovation gate size" name="EK2_VEL_I_GATE" documentation="This sets the percentage number of standard deviations applied to the GPS velocity measurement innovation consistency check. Decreasing it makes it more likely that good measurements willbe rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="GPS horizontal position measurement noise (m)" name="EK2_POSNE_M_NSE" documentation="This sets the GPS horizontal position observation noise. Increasing it reduces the weighting of GPS horizontal position measurements." user="Advanced">
<field name="Range">0.1 10.0</field>
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="GPS position measurement gate size" name="EK2_POS_I_GATE" documentation="This sets the percentage number of standard deviations applied to the GPS position measurement innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="GPS glitch radius gate size (m)" name="EK2_GLITCH_RAD" documentation="This controls the maximum radial uncertainty in position between the value predicted by the filter and the value measured by the GPS before the filter position and velocity states are reset to the GPS. Making this value larger allows the filter to ignore larger GPS glitches but also means that non-GPS errors such as IMU and compass can create a larger error in position before the filter is forced back to the GPS position." user="Advanced">
<field name="Range">10 100</field>
<field name="Increment">5</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="GPS measurement delay (msec)" name="EK2_GPS_DELAY" documentation="This is the number of msec that the GPS measurements lag behind the inertial measurements." user="Advanced">
<field name="Range">0 250</field>
<field name="Increment">10</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Primary altitude sensor source" name="EK2_ALT_SOURCE" documentation="This parameter controls the primary height sensor used by the EKF. If the selected option cannot be used, it will default to Baro as the primary height source. Setting 0 will use the baro altitude at all times. Setting 1 uses the range finder and is only available in combination with optical flow navigation (EK2_GPS_TYPE = 3). Setting 2 uses GPS. Setting 3 uses the range beacon data. NOTE - the EK2_RNG_USE_HGT parameter can be used to switch to range-finder when close to the ground." user="Advanced">
<values>
<value code="0">Use Baro</value>
<value code=" 1">Use Range Finder</value>
<value code=" 2">Use GPS</value>
<value code=" 3">Use Range Beacon</value>
</values>
</param>
<param humanName="Altitude measurement noise (m)" name="EK2_ALT_M_NSE" documentation="This is the RMS value of noise in the altitude measurement. Increasing it reduces the weighting of the baro measurement and will make the filter respond more slowly to baro measurement errors, but will make it more sensitive to GPS and accelerometer errors." user="Advanced">
<field name="Range">0.1 10.0</field>
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Height measurement gate size" name="EK2_HGT_I_GATE" documentation="This sets the percentage number of standard deviations applied to the height measurement innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Height measurement delay (msec)" name="EK2_HGT_DELAY" documentation="This is the number of msec that the Height measurements lag behind the inertial measurements." user="Advanced">
<field name="Range">0 250</field>
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<field name="Increment">10</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Magnetometer measurement noise (Gauss)" name="EK2_MAG_M_NSE" documentation="This is the RMS value of noise in magnetometer measurements. Increasing it reduces the weighting on these measurements." user="Advanced">
<field name="Range">0.01 0.5</field>
<field name="Increment">0.01</field>
<field name="Units">Gauss</field>
<field name="UnitText">gauss</field>
</param>
<param humanName="Magnetometer default fusion mode" name="EK2_MAG_CAL" documentation="This determines when the filter will use the 3-axis magnetometer fusion model that estimates both earth and body fixed magnetic field states and when it will use a simpler magnetic heading fusion model that does not use magnetic field states. The 3-axis magnetometer fusion is only suitable for use when the external magnetic field environment is stable. EK2_MAG_CAL = 0 uses heading fusion on ground, 3-axis fusion in-flight, and is the default setting for Plane users. EK2_MAG_CAL = 1 uses 3-axis fusion only when manoeuvring. EK2_MAG_CAL = 2 uses heading fusion at all times, is recommended if the external magnetic field is varying and is the default for rovers. EK2_MAG_CAL = 3 uses heading fusion on the ground and 3-axis fusion after the first in-air field and yaw reset has completed, and is the default for copters. EK2_MAG_CAL = 4 uses 3-axis fusion at all times. NOTE : Use of simple heading magnetometer fusion makes vehicle compass calibration and alignment errors harder for the EKF to detect which reduces the sensitivity of the Copter EKF failsafe algorithm. NOTE: The fusion mode can be forced to 2 for specific EKF cores using the EK2_MAG_MASK parameter." user="Advanced">
<values>
<value code="0">When flying</value>
<value code="1">When manoeuvring</value>
<value code="2">Never</value>
<value code="3">After first climb yaw reset</value>
<value code="4">Always</value>
</values>
</param>
<param humanName="Magnetometer measurement gate size" name="EK2_MAG_I_GATE" documentation="This sets the percentage number of standard deviations applied to the magnetometer measurement innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Equivalent airspeed measurement noise (m/s)" name="EK2_EAS_M_NSE" documentation="This is the RMS value of noise in equivalent airspeed measurements used by planes. Increasing it reduces the weighting of airspeed measurements and will make wind speed estimates less noisy and slower to converge. Increasing also increases navigation errors when dead-reckoning without GPS measurements." user="Advanced">
<field name="Range">0.5 5.0</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Airspeed measurement gate size" name="EK2_EAS_I_GATE" documentation="This sets the percentage number of standard deviations applied to the airspeed measurement innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Range finder measurement noise (m)" name="EK2_RNG_M_NSE" documentation="This is the RMS value of noise in the range finder measurement. Increasing it reduces the weighting on this measurement." user="Advanced">
<field name="Range">0.1 10.0</field>
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Range finder measurement gate size" name="EK2_RNG_I_GATE" documentation="This sets the percentage number of standard deviations applied to the range finder innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Maximum valid optical flow rate" name="EK2_MAX_FLOW" documentation="This sets the magnitude maximum optical flow rate in rad/sec that will be accepted by the filter" user="Advanced">
<field name="Range">1.0 4.0</field>
<field name="Increment">0.1</field>
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Optical flow measurement noise (rad/s)" name="EK2_FLOW_M_NSE" documentation="This is the RMS value of noise and errors in optical flow measurements. Increasing it reduces the weighting on these measurements." user="Advanced">
<field name="Range">0.05 1.0</field>
<field name="Increment">0.05</field>
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Optical Flow measurement gate size" name="EK2_FLOW_I_GATE" documentation="This sets the percentage number of standard deviations applied to the optical flow innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Optical Flow measurement delay (msec)" name="EK2_FLOW_DELAY" documentation="This is the number of msec that the optical flow measurements lag behind the inertial measurements. It is the time from the end of the optical flow averaging period and does not include the time delay due to the 100msec of averaging within the flow sensor." user="Advanced">
<field name="Range">0 127</field>
<field name="Increment">10</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Rate gyro noise (rad/s)" name="EK2_GYRO_P_NSE" documentation="This control disturbance noise controls the growth of estimated error due to gyro measurement errors excluding bias. Increasing it makes the flter trust the gyro measurements less and other measurements more." user="Advanced">
<field name="Range">0.0001 0.1</field>
<field name="Increment">0.0001</field>
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<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Accelerometer noise (m/s^2)" name="EK2_ACC_P_NSE" documentation="This control disturbance noise controls the growth of estimated error due to accelerometer measurement errors excluding bias. Increasing it makes the flter trust the accelerometer measurements less and other measurements more." user="Advanced">
<field name="Range">0.01 1.0</field>
<field name="Increment">0.01</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Rate gyro bias stability (rad/s/s)" name="EK2_GBIAS_P_NSE" documentation="This state process noise controls growth of the gyro delta angle bias state error estimate. Increasing it makes rate gyro bias estimation faster and noisier." user="Advanced">
<field name="Range">0.00001 0.001</field>
<field name="Units">rad/s/s</field>
<field name="UnitText">radians per square second</field>
</param>
<param humanName="Rate gyro scale factor stability (1/s)" name="EK2_GSCL_P_NSE" documentation="This noise controls the rate of gyro scale factor learning. Increasing it makes rate gyro scale factor estimation faster and noisier." user="Advanced">
<field name="Range">0.000001 0.001</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Accelerometer bias stability (m/s^3)" name="EK2_ABIAS_P_NSE" documentation="This noise controls the growth of the vertical accelerometer delta velocity bias state error estimate. Increasing it makes accelerometer bias estimation faster and noisier." user="Advanced">
<field name="Range">0.00001 0.001</field>
<field name="Units">m/s/s/s</field>
<field name="UnitText">meters per cubic second</field>
</param>
<param humanName="Wind velocity process noise (m/s^2)" name="EK2_WIND_P_NSE" documentation="This state process noise controls the growth of wind state error estimates. Increasing it makes wind estimation faster and noisier." user="Advanced">
<field name="Range">0.01 1.0</field>
<field name="Increment">0.1</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Height rate to wind process noise scaler" name="EK2_WIND_PSCALE" documentation="This controls how much the process noise on the wind states is increased when gaining or losing altitude to take into account changes in wind speed and direction with altitude. Increasing this parameter increases how rapidly the wind states adapt when changing altitude, but does make wind velocity estimation noiser." user="Advanced">
<field name="Range">0.0 1.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="GPS preflight check" name="EK2_GPS_CHECK" documentation="This is a 1 byte bitmap controlling which GPS preflight checks are performed. Set to 0 to bypass all checks. Set to 255 perform all checks. Set to 3 to check just the number of satellites and HDoP. Set to 31 for the most rigorous checks that will still allow checks to pass when the copter is moving, eg launch from a boat." user="Advanced">
<field name="Bitmask">0:NSats,1:HDoP,2:speed error,3:position error,4:yaw error,5:pos drift,6:vert speed,7:horiz speed</field>
</param>
<param humanName="Bitmask of active IMUs" name="EK2_IMU_MASK" documentation="1 byte bitmap of IMUs to use in EKF2. A separate instance of EKF2 will be started for each IMU selected. Set to 1 to use the first IMU only (default), set to 2 to use the second IMU only, set to 3 to use the first and second IMU. Additional IMU's can be used up to a maximum of 6 if memory and processing resources permit. There may be insufficient memory and processing resources to run multiple instances. If this occurs EKF2 will fail to start." user="Advanced">
<field name="Bitmask">0:FirstIMU,1:SecondIMU,2:ThirdIMU,3:FourthIMU,4:FifthIMU,5:SixthIMU</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="GPS accuracy check scaler (%)" name="EK2_CHECK_SCALE" documentation="This scales the thresholds that are used to check GPS accuracy before it is used by the EKF. A value of 100 is the default. Values greater than 100 increase and values less than 100 reduce the maximum GPS error the EKF will accept. A value of 200 will double the allowable GPS error." user="Advanced">
<field name="Range">50 200</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Non-GPS operation position uncertainty (m)" name="EK2_NOAID_M_NSE" documentation="This sets the amount of position variation that the EKF allows for when operating without external measurements (eg GPS or optical flow). Increasing this parameter makes the EKF attitude estimate less sensitive to vehicle manoeuvres but more sensitive to IMU errors." user="Advanced">
<field name="Range">0.5 50.0</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="EKF sensor logging IMU mask" name="EK2_LOG_MASK" documentation="This sets the IMU mask of sensors to do full logging for" user="Advanced">
<field name="Bitmask">0:FirstIMU,1:SecondIMU,2:ThirdIMU,3:FourthIMU,4:FifthIMU,5:SixthIMU</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Yaw measurement noise (rad)" name="EK2_YAW_M_NSE" documentation="This is the RMS value of noise in yaw measurements from the magnetometer. Increasing it reduces the weighting on these measurements." user="Advanced">
<field name="Range">0.05 1.0</field>
<field name="Increment">0.05</field>
<field name="Units">rad</field>
<field name="UnitText">radians</field>
</param>
<param humanName="Yaw measurement gate size" name="EK2_YAW_I_GATE" documentation="This sets the percentage number of standard deviations applied to the magnetometer yaw measurement innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Output complementary filter time constant (centi-sec)" name="EK2_TAU_OUTPUT" documentation="Sets the time constant of the output complementary filter/predictor in centi-seconds." user="Advanced">
<field name="Range">10 50</field>
<field name="Increment">5</field>
<field name="Units">cs</field>
<field name="UnitText">centiseconds</field>
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</param>
<param humanName="Earth magnetic field process noise (gauss/s)" name="EK2_MAGE_P_NSE" documentation="This state process noise controls the growth of earth magnetic field state error estimates. Increasing it makes earth magnetic field estimation faster and noisier." user="Advanced">
<field name="Range">0.00001 0.01</field>
<field name="Units">Gauss/s</field>
<field name="UnitText">gauss per second</field>
</param>
<param humanName="Body magnetic field process noise (gauss/s)" name="EK2_MAGB_P_NSE" documentation="This state process noise controls the growth of body magnetic field state error estimates. Increasing it makes magnetometer bias error estimation faster and noisier." user="Advanced">
<field name="Range">0.00001 0.01</field>
<field name="Units">Gauss/s</field>
<field name="UnitText">gauss per second</field>
</param>
<param humanName="Range finder switch height percentage" name="EK2_RNG_USE_HGT" documentation="The range finder will be used as the primary height source when below a specified percentage of the sensor maximum as set by the RNGFND_MAX_CM parameter. Set to -1 to prevent range finder use." user="Advanced">
<field name="Range">-1 70</field>
<field name="Increment">1</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Maximum terrain gradient" name="EK2_TERR_GRAD" documentation="Specifies the maximum gradient of the terrain below the vehicle when it is using range finder as a height reference" user="Advanced">
<field name="Range">0 0.2</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Range beacon measurement noise (m)" name="EK2_BCN_M_NSE" documentation="This is the RMS value of noise in the range beacon measurement. Increasing it reduces the weighting on this measurement." user="Advanced">
<field name="Range">0.1 10.0</field>
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Range beacon measurement gate size" name="EK2_BCN_I_GTE" documentation="This sets the percentage number of standard deviations applied to the range beacon measurement innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Range beacon measurement delay (msec)" name="EK2_BCN_DELAY" documentation="This is the number of msec that the range beacon measurements lag behind the inertial measurements. It is the time from the end of the optical flow averaging period and does not include the time delay due to the 100msec of averaging within the flow sensor." user="Advanced">
<field name="Range">0 127</field>
<field name="Increment">10</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Range finder max ground speed" name="EK2_RNG_USE_SPD" documentation="The range finder will not be used as the primary height source when the horizontal ground speed is greater than this value." user="Advanced">
<field name="Range">2.0 6.0</field>
<field name="Increment">0.5</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Bitmask of active EKF cores that will always use heading fusion" name="EK2_MAG_MASK" documentation="1 byte bitmap of EKF cores that will disable magnetic field states and use simple magnetic heading fusion at all times. This parameter enables specified cores to be used as a backup for flight into an environment with high levels of external magnetic interference which may degrade the EKF attitude estimate when using 3-axis magnetometer fusion. NOTE : Use of a different magnetometer fusion algorithm on different cores makes unwanted EKF core switches due to magnetometer errors more likely." user="Advanced">
<field name="Bitmask">0:FirstEKF,1:SecondEKF,2:ThirdEKF,3:FourthEKF,4:FifthEKF,5:SixthEKF</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Bitmask control of EKF reference height correction" name="EK2_OGN_HGT_MASK" documentation="When a height sensor other than GPS is used as the primary height source by the EKF, the position of the zero height datum is defined by that sensor and its frame of reference. If a GPS height measurement is also available, then the height of the WGS-84 height datum used by the EKF can be corrected so that the height returned by the getLLH() function is compensated for primary height sensor drift and change in datum over time. The first two bit positions control when the height datum will be corrected. Correction is performed using a Bayes filter and only operates when GPS quality permits. The third bit position controls where the corrections to the GPS reference datum are applied. Corrections can be applied to the local vertical position or to the reported EKF origin height (default)." user="Advanced">
<field name="Bitmask">0:Correct when using Baro height,1:Correct when using range finder height,2:Apply corrections to local position</field>
<field name="RebootRequired">True</field>
</param>
</parameters>
<parameters name="EK3_">
<param humanName="Enable EKF3" name="EK3_ENABLE" documentation="This enables EKF3. Enabling EKF3 only makes the maths run, it does not mean it will be used for flight control. To use it for flight control set AHRS_EKF_TYPE=3. A reboot or restart will need to be performed after changing the value of EK3_ENABLE for it to take effect." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code=" 1">Enabled</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="GPS mode control" name="EK3_GPS_TYPE" documentation="This controls use of GPS measurements : 0 = use 3D velocity & 2D position, 1 = use 2D velocity and 2D position, 2 = use 2D position, 3 = Inhibit GPS use - this can be useful when flying with an optical flow sensor in an environment where GPS quality is poor and subject to large multipath errors." user="Advanced">
<values>
<value code="0">GPS 3D Vel and 2D Pos</value>
<value code=" 1">GPS 2D vel and 2D pos</value>
<value code=" 2">GPS 2D pos</value>
<value code=" 3">No GPS</value>
</values>
</param>
<param humanName="GPS horizontal velocity measurement noise (m/s)" name="EK3_VELNE_M_NSE" documentation="This sets a lower limit on the speed accuracy reported by the GPS receiver that is used to set horizontal velocity observation noise. If the model of receiver used does not provide a speed accurcy estimate, then the parameter value will be used. Increasing it reduces the weighting of the GPS horizontal velocity measurements." user="Advanced">
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<field name="Range">0.05 5.0</field>
<field name="Increment">0.05</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="GPS vertical velocity measurement noise (m/s)" name="EK3_VELD_M_NSE" documentation="This sets a lower limit on the speed accuracy reported by the GPS receiver that is used to set vertical velocity observation noise. If the model of receiver used does not provide a speed accurcy estimate, then the parameter value will be used. Increasing it reduces the weighting of the GPS vertical velocity measurements." user="Advanced">
<field name="Range">0.05 5.0</field>
<field name="Increment">0.05</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="GPS velocity innovation gate size" name="EK3_VEL_I_GATE" documentation="This sets the percentage number of standard deviations applied to the GPS velocity measurement innovation consistency check. Decreasing it makes it more likely that good measurements willbe rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="GPS horizontal position measurement noise (m)" name="EK3_POSNE_M_NSE" documentation="This sets the GPS horizontal position observation noise. Increasing it reduces the weighting of GPS horizontal position measurements." user="Advanced">
<field name="Range">0.1 10.0</field>
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="GPS position measurement gate size" name="EK3_POS_I_GATE" documentation="This sets the percentage number of standard deviations applied to the GPS position measurement innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="GPS glitch radius gate size (m)" name="EK3_GLITCH_RAD" documentation="This controls the maximum radial uncertainty in position between the value predicted by the filter and the value measured by the GPS before the filter position and velocity states are reset to the GPS. Making this value larger allows the filter to ignore larger GPS glitches but also means that non-GPS errors such as IMU and compass can create a larger error in position before the filter is forced back to the GPS position." user="Advanced">
<field name="Range">10 100</field>
<field name="Increment">5</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Primary altitude sensor source" name="EK3_ALT_SOURCE" documentation="This parameter controls the primary height sensor used by the EKF. If the selected option cannot be used, it will default to Baro as the primary height source. Setting 0 will use the baro altitude at all times. Setting 1 uses the range finder and is only available in combination with optical flow navigation (EK3_GPS_TYPE = 3). Setting 2 uses GPS. Setting 3 uses the range beacon data. NOTE - the EK3_RNG_USE_HGT parameter can be used to switch to range-finder when close to the ground." user="Advanced">
<values>
<value code="0">Use Baro</value>
<value code=" 1">Use Range Finder</value>
<value code=" 2">Use GPS</value>
<value code=" 3">Use Range Beacon</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Altitude measurement noise (m)" name="EK3_ALT_M_NSE" documentation="This is the RMS value of noise in the altitude measurement. Increasing it reduces the weighting of the baro measurement and will make the filter respond more slowly to baro measurement errors, but will make it more sensitive to GPS and accelerometer errors." user="Advanced">
<field name="Range">0.1 10.0</field>
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Height measurement gate size" name="EK3_HGT_I_GATE" documentation="This sets the percentage number of standard deviations applied to the height measurement innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Height measurement delay (msec)" name="EK3_HGT_DELAY" documentation="This is the number of msec that the Height measurements lag behind the inertial measurements." user="Advanced">
<field name="Range">0 250</field>
<field name="Increment">10</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Magnetometer measurement noise (Gauss)" name="EK3_MAG_M_NSE" documentation="This is the RMS value of noise in magnetometer measurements. Increasing it reduces the weighting on these measurements." user="Advanced">
<field name="Range">0.01 0.5</field>
<field name="Increment">0.01</field>
<field name="Units">Gauss</field>
<field name="UnitText">gauss</field>
</param>
<param humanName="Magnetometer default fusion mode" name="EK3_MAG_CAL" documentation="This determines when the filter will use the 3-axis magnetometer fusion model that estimates both earth and body fixed magnetic field states and when it will use a simpler magnetic heading fusion model that does not use magnetic field states. The 3-axis magnetometer fusion is only suitable for use when the external magnetic field environment is stable. EK3_MAG_CAL = 0 uses heading fusion on ground, 3-axis fusion in-flight, and is the default setting for Plane users. EK3_MAG_CAL = 1 uses 3-axis fusion only when manoeuvring. EK3_MAG_CAL = 2 uses heading fusion at all times, is recommended if the external magnetic field is varying and is the default for rovers. EK3_MAG_CAL = 3 uses heading fusion on the ground and 3-axis fusion after the first in-air field and yaw reset has completed, and is the default for copters. EK3_MAG_CAL = 4 uses 3-axis fusion at all times. NOTE : Use of simple heading magnetometer fusion makes vehicle compass calibration and alignment errors harder for the EKF to detect which reduces the sensitivity of the Copter EKF failsafe algorithm. NOTE: The fusion mode can be forced to 2 for specific EKF cores using the EK3_MAG_MASK parameter." user="Advanced">
<values>
<value code="0">When flying</value>
<value code="1">When manoeuvring</value>
<value code="2">Never</value>
<value code="3">After first climb yaw reset</value>
<value code="4">Always</value>
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</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Magnetometer measurement gate size" name="EK3_MAG_I_GATE" documentation="This sets the percentage number of standard deviations applied to the magnetometer measurement innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Equivalent airspeed measurement noise (m/s)" name="EK3_EAS_M_NSE" documentation="This is the RMS value of noise in equivalent airspeed measurements used by planes. Increasing it reduces the weighting of airspeed measurements and will make wind speed estimates less noisy and slower to converge. Increasing also increases navigation errors when dead-reckoning without GPS measurements." user="Advanced">
<field name="Range">0.5 5.0</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Airspeed measurement gate size" name="EK3_EAS_I_GATE" documentation="This sets the percentage number of standard deviations applied to the airspeed measurement innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Range finder measurement noise (m)" name="EK3_RNG_M_NSE" documentation="This is the RMS value of noise in the range finder measurement. Increasing it reduces the weighting on this measurement." user="Advanced">
<field name="Range">0.1 10.0</field>
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Range finder measurement gate size" name="EK3_RNG_I_GATE" documentation="This sets the percentage number of standard deviations applied to the range finder innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Maximum valid optical flow rate" name="EK3_MAX_FLOW" documentation="This sets the magnitude maximum optical flow rate in rad/sec that will be accepted by the filter" user="Advanced">
<field name="Range">1.0 4.0</field>
<field name="Increment">0.1</field>
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Optical flow measurement noise (rad/s)" name="EK3_FLOW_M_NSE" documentation="This is the RMS value of noise and errors in optical flow measurements. Increasing it reduces the weighting on these measurements." user="Advanced">
<field name="Range">0.05 1.0</field>
<field name="Increment">0.05</field>
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Optical Flow measurement gate size" name="EK3_FLOW_I_GATE" documentation="This sets the percentage number of standard deviations applied to the optical flow innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Optical Flow measurement delay (msec)" name="EK3_FLOW_DELAY" documentation="This is the number of msec that the optical flow measurements lag behind the inertial measurements. It is the time from the end of the optical flow averaging period and does not include the time delay due to the 100msec of averaging within the flow sensor." user="Advanced">
<field name="Range">0 250</field>
<field name="Increment">10</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Rate gyro noise (rad/s)" name="EK3_GYRO_P_NSE" documentation="This control disturbance noise controls the growth of estimated error due to gyro measurement errors excluding bias. Increasing it makes the flter trust the gyro measurements less and other measurements more." user="Advanced">
<field name="Range">0.0001 0.1</field>
<field name="Increment">0.0001</field>
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Accelerometer noise (m/s^2)" name="EK3_ACC_P_NSE" documentation="This control disturbance noise controls the growth of estimated error due to accelerometer measurement errors excluding bias. Increasing it makes the flter trust the accelerometer measurements less and other measurements more." user="Advanced">
<field name="Range">0.01 1.0</field>
<field name="Increment">0.01</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Rate gyro bias stability (rad/s/s)" name="EK3_GBIAS_P_NSE" documentation="This state process noise controls growth of the gyro delta angle bias state error estimate. Increasing it makes rate gyro bias estimation faster and noisier." user="Advanced">
<field name="Range">0.00001 0.001</field>
<field name="Units">rad/s/s</field>
<field name="UnitText">radians per square second</field>
</param>
<param humanName="Accelerometer bias stability (m/s^3)" name="EK3_ABIAS_P_NSE" documentation="This noise controls the growth of the vertical accelerometer delta velocity bias state error estimate. Increasing it makes accelerometer bias estimation faster and noisier." user="Advanced">
<field name="Range">0.00001 0.001</field>
<field name="Units">m/s/s/s</field>
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<field name="UnitText">meters per cubic second</field>
</param>
<param humanName="Wind velocity process noise (m/s^2)" name="EK3_WIND_P_NSE" documentation="This state process noise controls the growth of wind state error estimates. Increasing it makes wind estimation faster and noisier." user="Advanced">
<field name="Range">0.01 1.0</field>
<field name="Increment">0.1</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Height rate to wind process noise scaler" name="EK3_WIND_PSCALE" documentation="This controls how much the process noise on the wind states is increased when gaining or losing altitude to take into account changes in wind speed and direction with altitude. Increasing this parameter increases how rapidly the wind states adapt when changing altitude, but does make wind velocity estimation noiser." user="Advanced">
<field name="Range">0.0 1.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="GPS preflight check" name="EK3_GPS_CHECK" documentation="This is a 1 byte bitmap controlling which GPS preflight checks are performed. Set to 0 to bypass all checks. Set to 255 perform all checks. Set to 3 to check just the number of satellites and HDoP. Set to 31 for the most rigorous checks that will still allow checks to pass when the copter is moving, eg launch from a boat." user="Advanced">
<field name="Bitmask">0:NSats,1:HDoP,2:speed error,3:position error,4:yaw error,5:pos drift,6:vert speed,7:horiz speed</field>
</param>
<param humanName="Bitmask of active IMUs" name="EK3_IMU_MASK" documentation="1 byte bitmap of IMUs to use in EKF3. A separate instance of EKF3 will be started for each IMU selected. Set to 1 to use the first IMU only (default), set to 2 to use the second IMU only, set to 3 to use the first and second IMU. Additional IMU's can be used up to a maximum of 6 if memory and processing resources permit. There may be insufficient memory and processing resources to run multiple instances. If this occurs EKF3 will fail to start." user="Advanced">
<field name="Bitmask">0:FirstIMU,1:SecondIMU,2:ThirdIMU,3:FourthIMU,4:FifthIMU,5:SixthIMU</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="GPS accuracy check scaler (%)" name="EK3_CHECK_SCALE" documentation="This scales the thresholds that are used to check GPS accuracy before it is used by the EKF. A value of 100 is the default. Values greater than 100 increase and values less than 100 reduce the maximum GPS error the EKF will accept. A value of 200 will double the allowable GPS error." user="Advanced">
<field name="Range">50 200</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Non-GPS operation position uncertainty (m)" name="EK3_NOAID_M_NSE" documentation="This sets the amount of position variation that the EKF allows for when operating without external measurements (eg GPS or optical flow). Increasing this parameter makes the EKF attitude estimate less sensitive to vehicle manoeuvres but more sensitive to IMU errors." user="Advanced">
<field name="Range">0.5 50.0</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="EKF sensor logging IMU mask" name="EK3_LOG_MASK" documentation="This sets the IMU mask of sensors to do full logging for" user="Advanced">
<field name="Bitmask">0:FirstIMU,1:SecondIMU,2:ThirdIMU,3:FourthIMU,4:FifthIMU,5:SixthIMU</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Yaw measurement noise (rad)" name="EK3_YAW_M_NSE" documentation="This is the RMS value of noise in yaw measurements from the magnetometer. Increasing it reduces the weighting on these measurements." user="Advanced">
<field name="Range">0.05 1.0</field>
<field name="Increment">0.05</field>
<field name="Units">rad</field>
<field name="UnitText">radians</field>
</param>
<param humanName="Yaw measurement gate size" name="EK3_YAW_I_GATE" documentation="This sets the percentage number of standard deviations applied to the magnetometer yaw measurement innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Output complementary filter time constant (centi-sec)" name="EK3_TAU_OUTPUT" documentation="Sets the time constant of the output complementary filter/predictor in centi-seconds." user="Advanced">
<field name="Range">10 50</field>
<field name="Increment">5</field>
<field name="Units">cs</field>
<field name="UnitText">centiseconds</field>
</param>
<param humanName="Earth magnetic field process noise (gauss/s)" name="EK3_MAGE_P_NSE" documentation="This state process noise controls the growth of earth magnetic field state error estimates. Increasing it makes earth magnetic field estimation faster and noisier." user="Advanced">
<field name="Range">0.00001 0.01</field>
<field name="Units">Gauss/s</field>
<field name="UnitText">gauss per second</field>
</param>
<param humanName="Body magnetic field process noise (gauss/s)" name="EK3_MAGB_P_NSE" documentation="This state process noise controls the growth of body magnetic field state error estimates. Increasing it makes magnetometer bias error estimation faster and noisier." user="Advanced">
<field name="Range">0.00001 0.01</field>
<field name="Units">Gauss/s</field>
<field name="UnitText">gauss per second</field>
</param>
<param humanName="Range finder switch height percentage" name="EK3_RNG_USE_HGT" documentation="The range finder will be used as the primary height source when below a specified percentage of the sensor maximum as set by the RNGFND_MAX_CM parameter. Set to -1 to prevent range finder use." user="Advanced">
<field name="Range">-1 70</field>
<field name="Increment">1</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Maximum terrain gradient" name="EK3_TERR_GRAD" documentation="Specifies the maximum gradient of the terrain below the vehicle when it is using range finder as a height reference" user="Advanced">
<field name="Range">0 0.2</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Range beacon measurement noise (m)" name="EK3_BCN_M_NSE" documentation="This is the RMS value of noise in the range beacon measurement. Increasing it reduces the weighting on this measurement." user="Advanced">
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<field name="Range">0.1 10.0</field>
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Range beacon measurement gate size" name="EK3_BCN_I_GTE" documentation="This sets the percentage number of standard deviations applied to the range beacon measurement innovation consistency check. Decreasing it makes it more likely that good measurements will be rejected. Increasing it makes it more likely that bad measurements will be accepted." user="Advanced">
<field name="Range">100 1000</field>
<field name="Increment">25</field>
</param>
<param humanName="Range beacon measurement delay (msec)" name="EK3_BCN_DELAY" documentation="This is the number of msec that the range beacon measurements lag behind the inertial measurements." user="Advanced">
<field name="Range">0 250</field>
<field name="Increment">10</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Range finder max ground speed" name="EK3_RNG_USE_SPD" documentation="The range finder will not be used as the primary height source when the horizontal ground speed is greater than this value." user="Advanced">
<field name="Range">2.0 6.0</field>
<field name="Increment">0.5</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Accelerometer bias limit" name="EK3_ACC_BIAS_LIM" documentation="The accelerometer bias state will be limited to +- this value" user="Advanced">
<field name="Range">0.5 2.5</field>
<field name="Increment">0.1</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Bitmask of active EKF cores that will always use heading fusion" name="EK3_MAG_MASK" documentation="1 byte bitmap of EKF cores that will disable magnetic field states and use simple magnetic heading fusion at all times. This parameter enables specified cores to be used as a backup for flight into an environment with high levels of external magnetic interference which may degrade the EKF attitude estimate when using 3-axis magnetometer fusion. NOTE : Use of a different magnetometer fusion algorithm on different cores makes unwanted EKF core switches due to magnetometer errors more likely." user="Advanced">
<field name="Bitmask">0:FirstEKF,1:SecondEKF,2:ThirdEKF,3:FourthEKF,4:FifthEKF,5:SixthEKF</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Bitmask control of EKF reference height correction" name="EK3_OGN_HGT_MASK" documentation="When a height sensor other than GPS is used as the primary height source by the EKF, the position of the zero height datum is defined by that sensor and its frame of reference. If a GPS height measurement is also available, then the height of the WGS-84 height datum used by the EKF can be corrected so that the height returned by the getLLH() function is compensated for primary height sensor drift and change in datum over time. The first two bit positions control when the height datum will be corrected. Correction is performed using a Bayes filter and only operates when GPS quality permits. The third bit position controls where the corrections to the GPS reference datum are applied. Corrections can be applied to the local vertical position or to the reported EKF origin height (default)." user="Advanced">
<field name="Bitmask">0:Correct when using Baro height,1:Correct when using range finder height,2:Apply corrections to local position</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Visual odometry minimum velocity error" name="EK3_VIS_VERR_MIN" documentation="This is the 1-STD odometry velocity observation error that will be assumed when maximum quality is reported by the sensor. When quality is between max and min, the error will be calculated using linear interpolation between VIS_VERR_MIN and VIS_VERR_MAX." user="Advanced">
<field name="Range">0.05 0.5</field>
<field name="Increment">0.05</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Visual odometry maximum velocity error" name="EK3_VIS_VERR_MAX" documentation="This is the 1-STD odometry velocity observation error that will be assumed when minimum quality is reported by the sensor. When quality is between max and min, the error will be calculated using linear interpolation between VIS_VERR_MIN and VIS_VERR_MAX." user="Advanced">
<field name="Range">0.5 5.0</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Wheel odometry velocity error" name="EK3_WENC_VERR" documentation="This is the 1-STD odometry velocity observation error that will be assumed when wheel encoder data is being fused." user="Advanced">
<field name="Range">0.01 1.0</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
</parameters>
<parameters name="FLOW">
<param humanName="Optical flow enable/disable" name="FLOW_ENABLE" documentation="Setting this to Enabled(1) will enable optical flow. Setting this to Disabled(0) will disable optical flow" user="Standard">
<values>
<value code="0">Disabled</value>
<value code=" 1">Enabled</value>
</values>
</param>
<param humanName="X axis optical flow scale factor correction" name="FLOW_FXSCALER" documentation="This sets the parts per thousand scale factor correction applied to the flow sensor X axis optical rate. It can be used to correct for variations in effective focal length. Each positive increment of 1 increases the scale factor applied to the X axis optical flow reading by 0.1%. Negative values reduce the scale factor." user="Standard">
<field name="Range">-200 +200</field>
<field name="Increment">1</field>
</param>
<param humanName="Y axis optical flow scale factor correction" name="FLOW_FYSCALER" documentation="This sets the parts per thousand scale factor correction applied to the flow sensor Y axis optical rate. It can be used to correct for variations in effective focal length. Each positive increment of 1 increases the scale factor applied to the Y axis optical flow reading by 0.1%. Negative values reduce the scale factor." user="Standard">
<field name="Range">-200 +200</field>
<field name="Increment">1</field>
</param>
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<param humanName="Flow sensor yaw alignment" name="FLOW_ORIENT_YAW" documentation="Specifies the number of centi-degrees that the flow sensor is yawed relative to the vehicle. A sensor with its X-axis pointing to the right of the vehicle X axis has a positive yaw angle." user="Standard">
<field name="Range">-18000 +18000</field>
<field name="Increment">1</field>
</param>
<param humanName=" X position offset" name="FLOW_POS_X" documentation="X position of the optical flow sensor focal point in body frame. Positive X is forward of the origin." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Y position offset" name="FLOW_POS_Y" documentation="Y position of the optical flow sensor focal point in body frame. Positive Y is to the right of the origin." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Z position offset" name="FLOW_POS_Z" documentation="Z position of the optical flow sensor focal point in body frame. Positive Z is down from the origin." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="ID on the bus" name="FLOW_BUS_ID" documentation="This is used to select between multiple possible bus IDs for some sensor types. For PX4Flow you can choose 0 to 7 for the 8 possible addresses on the I2C bus." user="Advanced">
<field name="Range">0 127</field>
</param>
</parameters>
<parameters name="GND_">
<param humanName="Absolute Pressure" name="GND_ABS_PRESS" documentation="calibrated ground pressure in Pascals" user="Advanced">
<field name="ReadOnly">True</field>
<field name="Volatile">True</field>
<field name="Increment">1</field>
<field name="Units">Pa</field>
<field name="UnitText">pascal</field>
</param>
<param humanName="ground temperature" name="GND_TEMP" documentation="User provided ambient ground temperature in degrees Celsius. This is used to improve the calculation of the altitude the vehicle is at. This parameter is not persistent and will be reset to 0 every time the vehicle is rebooted. A value of 0 means use the internal measurement ambient temperature." user="Advanced">
<field name="Volatile">True</field>
<field name="Increment">1</field>
<field name="Units">degC</field>
<field name="UnitText">degrees Celsius</field>
</param>
<param humanName="altitude offset" name="GND_ALT_OFFSET" documentation="altitude offset in meters added to barometric altitude. This is used to allow for automatic adjustment of the base barometric altitude by a ground station equipped with a barometer. The value is added to the barometric altitude read by the aircraft. It is automatically reset to 0 when the barometer is calibrated on each reboot or when a preflight calibration is performed." user="Advanced">
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Primary barometer" name="GND_PRIMARY" documentation="This selects which barometer will be the primary if multiple barometers are found" user="Advanced">
<values>
<value code="0">FirstBaro</value>
<value code="1">2ndBaro</value>
<value code="2">3rdBaro</value>
</values>
</param>
<param humanName="External baro bus" name="GND_EXT_BUS" documentation="This selects the bus number for looking for an I2C barometer" user="Advanced">
<values>
<value code="-1">Disabled</value>
<value code="0">Bus0</value>
<value code="1">Bus1</value>
</values>
</param>
<param humanName="Specific Gravity (For water depth measurement)" name="GND_SPEC_GRAV" documentation="This sets the specific gravity of the fluid when flying an underwater ROV.">
<field name="Values">1.0:Freshwater,1.024:Saltwater</field>
</param>
<param humanName="Absolute Pressure" name="GND_ABS_PRESS2" documentation="calibrated ground pressure in Pascals" user="Advanced">
<field name="ReadOnly">True</field>
<field name="Volatile">True</field>
<field name="Increment">1</field>
<field name="Units">Pa</field>
<field name="UnitText">pascal</field>
</param>
<param humanName="Absolute Pressure" name="GND_ABS_PRESS3" documentation="calibrated ground pressure in Pascals" user="Advanced">
<field name="ReadOnly">True</field>
<field name="Volatile">True</field>
<field name="Increment">1</field>
<field name="Units">Pa</field>
<field name="UnitText">pascal</field>
</param>
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</parameters>
<parameters name="GPS_">
<param humanName="GPS type" name="GPS_TYPE" documentation="GPS type" user="Advanced">
<values>
<value code="0">None</value>
<value code="1">AUTO</value>
<value code="2">uBlox</value>
<value code="3">MTK</value>
<value code="4">MTK19</value>
<value code="5">NMEA</value>
<value code="6">SiRF</value>
<value code="7">HIL</value>
<value code="8">SwiftNav</value>
<value code="9">UAVCAN</value>
<value code="10">SBF</value>
<value code="11">GSOF</value>
<value code="12">QURT</value>
<value code="13">ERB</value>
<value code="14">MAV</value>
<value code="15">NOVA</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="2nd GPS type" name="GPS_TYPE2" documentation="GPS type of 2nd GPS" user="Advanced">
<values>
<value code="0">None</value>
<value code="1">AUTO</value>
<value code="2">uBlox</value>
<value code="3">MTK</value>
<value code="4">MTK19</value>
<value code="5">NMEA</value>
<value code="6">SiRF</value>
<value code="7">HIL</value>
<value code="8">SwiftNav</value>
<value code="9">UAVCAN</value>
<value code="10">SBF</value>
<value code="11">GSOF</value>
<value code="12">QURT</value>
<value code="13">ERB</value>
<value code="14">MAV</value>
<value code="15">NOVA</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Navigation filter setting" name="GPS_NAVFILTER" documentation="Navigation filter engine setting" user="Advanced">
<values>
<value code="0">Portable</value>
<value code="2">Stationary</value>
<value code="3">Pedestrian</value>
<value code="4">Automotive</value>
<value code="5">Sea</value>
<value code="6">Airborne1G</value>
<value code="7">Airborne2G</value>
<value code="8">Airborne4G</value>
</values>
</param>
<param humanName="Automatic Switchover Setting" name="GPS_AUTO_SWITCH" documentation="Automatic switchover to GPS reporting best lock" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">UseBest</value>
<value code="2">Blend</value>
</values>
</param>
<param humanName="Minimum Lock Type Accepted for DGPS" name="GPS_MIN_DGPS" documentation="Sets the minimum type of differential GPS corrections required before allowing to switch into DGPS mode." user="Advanced">
<values>
<value code="0">Any</value>
<value code="50">FloatRTK</value>
<value code="100">IntegerRTK</value>
</values>
<field name="RebootRequired">True</field>
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</param>
<param humanName="SBAS Mode" name="GPS_SBAS_MODE" documentation="This sets the SBAS (satellite based augmentation system) mode if available on this GPS. If set to 2 then the SBAS mode is not changed in the GPS. Otherwise the GPS will be reconfigured to enable/disable SBAS. Disabling SBAS may be worthwhile in some parts of the world where an SBAS signal is available but the baseline is too long to be useful." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
<value code="2">NoChange</value>
</values>
</param>
<param humanName="Minimum elevation" name="GPS_MIN_ELEV" documentation="This sets the minimum elevation of satellites above the horizon for them to be used for navigation. Setting this to -100 leaves the minimum elevation set to the GPS modules default." user="Advanced">
<field name="Range">-100 90</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Destination for GPS_INJECT_DATA MAVLink packets" name="GPS_INJECT_TO" documentation="The GGS can send raw serial packets to inject data to multiple GPSes." user="Advanced">
<values>
<value code="0">send to first GPS</value>
<value code="1">send to 2nd GPS</value>
<value code="127">send to all</value>
</values>
</param>
<param humanName="Swift Binary Protocol Logging Mask" name="GPS_SBP_LOGMASK" documentation="Masked with the SBP msg_type field to determine whether SBR1/SBR2 data is logged" user="Advanced">
<values>
<value code="0">None (0x0000)</value>
<value code="-1">All (0xFFFF)</value>
<value code="-256">External only (0xFF00)</value>
</values>
</param>
<param humanName="Raw data logging" name="GPS_RAW_DATA" documentation="Enable logging of RXM raw data from uBlox which includes carrier phase and pseudo range information. This allows for post processing of dataflash logs for more precise positioning. Note that this requires a raw capable uBlox such as the 6P or 6T." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">log every sample</value>
<value code="5">log every 5 samples</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="GNSS system configuration" name="GPS_GNSS_MODE" documentation="Bitmask for what GNSS system to use on the first GPS (all unchecked or zero to leave GPS as configured)" user="Advanced">
<field name="Bitmask">0:GPS,1:SBAS,2:Galileo,3:Beidou,4:IMES,5:QZSS,6:GLOSNASS</field>
<values>
<value code="0">Leave as currently configured</value>
<value code=" 1">GPS-NoSBAS</value>
<value code=" 3">GPS+SBAS</value>
<value code=" 4">Galileo-NoSBAS</value>
<value code=" 6">Galileo+SBAS</value>
<value code=" 8">Beidou</value>
<value code=" 51">GPS+IMES+QZSS+SBAS (Japan Only)</value>
<value code=" 64">GLONASS</value>
<value code=" 66">GLONASS+SBAS</value>
<value code=" 67">GPS+GLONASS+SBAS</value>
</values>
</param>
<param humanName="Save GPS configuration" name="GPS_SAVE_CFG" documentation="Determines whether the configuration for this GPS should be written to non-volatile memory on the GPS. Currently working for UBlox 6 series and above." user="Advanced">
<values>
<value code="0">Do not save config</value>
<value code="1">Save config</value>
<value code="2">Save only when needed</value>
</values>
</param>
<param humanName="GNSS system configuration" name="GPS_GNSS_MODE2" documentation="Bitmask for what GNSS system to use on the second GPS (all unchecked or zero to leave GPS as configured)" user="Advanced">
<field name="Bitmask">0:GPS,1:SBAS,2:Galileo,3:Beidou,4:IMES,5:QZSS,6:GLOSNASS</field>
<values>
<value code="0">Leave as currently configured</value>
<value code=" 1">GPS-NoSBAS</value>
<value code=" 3">GPS+SBAS</value>
<value code=" 4">Galileo-NoSBAS</value>
<value code=" 6">Galileo+SBAS</value>
<value code=" 8">Beidou</value>
<value code=" 51">GPS+IMES+QZSS+SBAS (Japan Only)</value>
<value code=" 64">GLONASS</value>
<value code=" 66">GLONASS+SBAS</value>
<value code=" 67">GPS+GLONASS+SBAS</value>
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3001
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</values>
</param>
<param humanName="Automatic GPS configuration" name="GPS_AUTO_CONFIG" documentation="Controls if the autopilot should automatically configure the GPS based on the parameters and default settings" user="Advanced">
<values>
<value code="0">Disables automatic configuration</value>
<value code="1">Enable automatic configuration</value>
</values>
</param>
<param humanName="GPS update rate in milliseconds" name="GPS_RATE_MS" documentation="Controls how often the GPS should provide a position update. Lowering below 5Hz is not allowed" user="Advanced">
<field name="Range">50 200</field>
<values>
<value code="100">10Hz</value>
<value code="125">8Hz</value>
<value code="200">5Hz</value>
</values>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
</param>
<param humanName="GPS 2 update rate in milliseconds" name="GPS_RATE_MS2" documentation="Controls how often the GPS should provide a position update. Lowering below 5Hz is not allowed" user="Advanced">
<field name="Range">50 200</field>
<values>
<value code="100">10Hz</value>
<value code="125">8Hz</value>
<value code="200">5Hz</value>
</values>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
</param>
<param humanName="Antenna X position offset" name="GPS_POS1_X" documentation="X position of the first GPS antenna in body frame. Positive X is forward of the origin. Use antenna phase centroid location if provided by the manufacturer." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Antenna Y position offset" name="GPS_POS1_Y" documentation="Y position of the first GPS antenna in body frame. Positive Y is to the right of the origin. Use antenna phase centroid location if provided by the manufacturer." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Antenna Z position offset" name="GPS_POS1_Z" documentation="Z position of the first GPS antenna in body frame. Positive Z is down from the origin. Use antenna phase centroid location if provided by the manufacturer." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Antenna X position offset" name="GPS_POS2_X" documentation="X position of the second GPS antenna in body frame. Positive X is forward of the origin. Use antenna phase centroid location if provided by the manufacturer." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Antenna Y position offset" name="GPS_POS2_Y" documentation="Y position of the second GPS antenna in body frame. Positive Y is to the right of the origin. Use antenna phase centroid location if provided by the manufacturer." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Antenna Z position offset" name="GPS_POS2_Z" documentation="Z position of the second GPS antenna in body frame. Positive Z is down from the origin. Use antenna phase centroid location if provided by the manufacturer." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="GPS delay in milliseconds" name="GPS_DELAY_MS" documentation="Controls the amount of GPS measurement delay that the autopilot compensates for. Set to zero to use the default delay for the detected GPS type." user="Advanced">
<field name="Range">0 250</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="GPS 2 delay in milliseconds" name="GPS_DELAY_MS2" documentation="Controls the amount of GPS measurement delay that the autopilot compensates for. Set to zero to use the default delay for the detected GPS type." user="Advanced">
<field name="Range">0 250</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Multi GPS Blending Mask" name="GPS_BLEND_MASK" documentation="Determines which of the accuracy measures Horizontal position, Vertical Position and Speed are used to calculate the weighting on each GPS receiver when soft switching has been selected by setting GPS_AUTO_SWITCH to 2" user="Advanced">
<field name="Bitmask">0:Horiz Pos,1:Vert Pos,2:Speed</field>
</param>
<param humanName="Blending time constant" name="GPS_BLEND_TC" documentation="Controls the slowest time constant applied to the calculation of GPS position and height offsets used to adjust different GPS receivers for steady state position differences." user="Advanced">
<field name="Range">5.0 30.0</field>
<field name="Units">s</field>
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3080
<field name="UnitText">seconds</field>
</param>
</parameters>
<parameters name="ICE_">
<param humanName="Enable ICEngine control" name="ICE_ENABLE" documentation="This enables internal combusion engine control" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code=" 1">Enabled</value>
</values>
</param>
<param humanName="Input channel for engine start" name="ICE_START_CHAN" documentation="This is an RC input channel for requesting engine start. Engine will try to start when channel is at or above 1700. Engine will stop when channel is at or below 1300. Between 1301 and 1699 the engine will not change state unless a MAVLink command or mission item commands a state change, or the vehicle is disamed." user="Standard">
<values>
<value code="0">None</value>
<value code="1">Chan1</value>
<value code="2">Chan2</value>
<value code="3">Chan3</value>
<value code="4">Chan4</value>
<value code="5">Chan5</value>
<value code="6">Chan6</value>
<value code="7">Chan7</value>
<value code="8">Chan8</value>
<value code="9">Chan9</value>
<value code="10">Chan10</value>
<value code="11">Chan11</value>
<value code="12">Chan12</value>
<value code="13">Chan13</value>
<value code="14">Chan14</value>
<value code="15">Chan15</value>
<value code="16">Chan16</value>
</values>
</param>
<param humanName="Time to run starter" name="ICE_STARTER_TIME" documentation="This is the number of seconds to run the starter when trying to start the engine" user="Standard">
<field name="Range">0.1 5</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Time to wait between starts" name="ICE_START_DELAY" documentation="Delay between start attempts" user="Standard">
<field name="Range">1 10</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="RPM threshold" name="ICE_RPM_THRESH" documentation="This is the measured RPM above which tne engine is considered to be running" user="Standard">
<field name="Range">100 100000</field>
</param>
<param humanName="PWM value for ignition on" name="ICE_PWM_IGN_ON" documentation="This is the value sent to the ignition channel when on" user="Standard">
<field name="Range">1000 2000</field>
</param>
<param humanName="PWM value for ignition off" name="ICE_PWM_IGN_OFF" documentation="This is the value sent to the ignition channel when off" user="Standard">
<field name="Range">1000 2000</field>
</param>
<param humanName="PWM value for starter on" name="ICE_PWM_STRT_ON" documentation="This is the value sent to the starter channel when on" user="Standard">
<field name="Range">1000 2000</field>
</param>
<param humanName="PWM value for starter off" name="ICE_PWM_STRT_OFF" documentation="This is the value sent to the starter channel when off" user="Standard">
<field name="Range">1000 2000</field>
</param>
<param humanName="RPM instance channel to use" name="ICE_RPM_CHAN" documentation="This is which of the RPM instances to use for detecting the RPM of the engine" user="Standard">
<values>
<value code="0">None</value>
<value code="1">RPM1</value>
<value code="2">RPM2</value>
</values>
</param>
<param humanName="Throttle percentage for engine start" name="ICE_START_PCT" documentation="This is the percentage throttle output for engine start" user="Standard">
<field name="Range">0 100</field>
</param>
</parameters>
<parameters name="INS_">
<param humanName="IMU Product ID" name="INS_PRODUCT_ID" documentation="unused" user="Advanced">
</param>
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<param humanName="Gyro offsets of X axis" name="INS_GYROFFS_X" documentation="Gyro sensor offsets of X axis. This is setup on each boot during gyro calibrations" user="Advanced">
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Gyro offsets of Y axis" name="INS_GYROFFS_Y" documentation="Gyro sensor offsets of Y axis. This is setup on each boot during gyro calibrations" user="Advanced">
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Gyro offsets of Z axis" name="INS_GYROFFS_Z" documentation="Gyro sensor offsets of Z axis. This is setup on each boot during gyro calibrations" user="Advanced">
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Gyro2 offsets of X axis" name="INS_GYR2OFFS_X" documentation="Gyro2 sensor offsets of X axis. This is setup on each boot during gyro calibrations" user="Advanced">
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Gyro2 offsets of Y axis" name="INS_GYR2OFFS_Y" documentation="Gyro2 sensor offsets of Y axis. This is setup on each boot during gyro calibrations" user="Advanced">
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Gyro2 offsets of Z axis" name="INS_GYR2OFFS_Z" documentation="Gyro2 sensor offsets of Z axis. This is setup on each boot during gyro calibrations" user="Advanced">
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Gyro3 offsets of X axis" name="INS_GYR3OFFS_X" documentation="Gyro3 sensor offsets of X axis. This is setup on each boot during gyro calibrations" user="Advanced">
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Gyro3 offsets of Y axis" name="INS_GYR3OFFS_Y" documentation="Gyro3 sensor offsets of Y axis. This is setup on each boot during gyro calibrations" user="Advanced">
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Gyro3 offsets of Z axis" name="INS_GYR3OFFS_Z" documentation="Gyro3 sensor offsets of Z axis. This is setup on each boot during gyro calibrations" user="Advanced">
<field name="Units">rad/s</field>
<field name="UnitText">radians per second</field>
</param>
<param humanName="Accelerometer scaling of X axis" name="INS_ACCSCAL_X" documentation="Accelerometer scaling of X axis. Calculated during acceleration calibration routine" user="Advanced">
<field name="Range">0.8 1.2</field>
</param>
<param humanName="Accelerometer scaling of Y axis" name="INS_ACCSCAL_Y" documentation="Accelerometer scaling of Y axis Calculated during acceleration calibration routine" user="Advanced">
<field name="Range">0.8 1.2</field>
</param>
<param humanName="Accelerometer scaling of Z axis" name="INS_ACCSCAL_Z" documentation="Accelerometer scaling of Z axis Calculated during acceleration calibration routine" user="Advanced">
<field name="Range">0.8 1.2</field>
</param>
<param humanName="Accelerometer offsets of X axis" name="INS_ACCOFFS_X" documentation="Accelerometer offsets of X axis. This is setup using the acceleration calibration or level operations" user="Advanced">
<field name="Range">-3.5 3.5</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Accelerometer offsets of Y axis" name="INS_ACCOFFS_Y" documentation="Accelerometer offsets of Y axis. This is setup using the acceleration calibration or level operations" user="Advanced">
<field name="Range">-3.5 3.5</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Accelerometer offsets of Z axis" name="INS_ACCOFFS_Z" documentation="Accelerometer offsets of Z axis. This is setup using the acceleration calibration or level operations" user="Advanced">
<field name="Range">-3.5 3.5</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Accelerometer2 scaling of X axis" name="INS_ACC2SCAL_X" documentation="Accelerometer2 scaling of X axis. Calculated during acceleration calibration routine" user="Advanced">
<field name="Range">0.8 1.2</field>
</param>
<param humanName="Accelerometer2 scaling of Y axis" name="INS_ACC2SCAL_Y" documentation="Accelerometer2 scaling of Y axis Calculated during acceleration calibration routine" user="Advanced">
<field name="Range">0.8 1.2</field>
</param>
<param humanName="Accelerometer2 scaling of Z axis" name="INS_ACC2SCAL_Z" documentation="Accelerometer2 scaling of Z axis Calculated during acceleration calibration routine" user="Advanced">
<field name="Range">0.8 1.2</field>
</param>
<param humanName="Accelerometer2 offsets of X axis" name="INS_ACC2OFFS_X" documentation="Accelerometer2 offsets of X axis. This is setup using the acceleration calibration or level operations" user="Advanced">
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<field name="Range">-3.5 3.5</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Accelerometer2 offsets of Y axis" name="INS_ACC2OFFS_Y" documentation="Accelerometer2 offsets of Y axis. This is setup using the acceleration calibration or level operations" user="Advanced">
<field name="Range">-3.5 3.5</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Accelerometer2 offsets of Z axis" name="INS_ACC2OFFS_Z" documentation="Accelerometer2 offsets of Z axis. This is setup using the acceleration calibration or level operations" user="Advanced">
<field name="Range">-3.5 3.5</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Accelerometer3 scaling of X axis" name="INS_ACC3SCAL_X" documentation="Accelerometer3 scaling of X axis. Calculated during acceleration calibration routine" user="Advanced">
<field name="Range">0.8 1.2</field>
</param>
<param humanName="Accelerometer3 scaling of Y axis" name="INS_ACC3SCAL_Y" documentation="Accelerometer3 scaling of Y axis Calculated during acceleration calibration routine" user="Advanced">
<field name="Range">0.8 1.2</field>
</param>
<param humanName="Accelerometer3 scaling of Z axis" name="INS_ACC3SCAL_Z" documentation="Accelerometer3 scaling of Z axis Calculated during acceleration calibration routine" user="Advanced">
<field name="Range">0.8 1.2</field>
</param>
<param humanName="Accelerometer3 offsets of X axis" name="INS_ACC3OFFS_X" documentation="Accelerometer3 offsets of X axis. This is setup using the acceleration calibration or level operations" user="Advanced">
<field name="Range">-3.5 3.5</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Accelerometer3 offsets of Y axis" name="INS_ACC3OFFS_Y" documentation="Accelerometer3 offsets of Y axis. This is setup using the acceleration calibration or level operations" user="Advanced">
<field name="Range">-3.5 3.5</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Accelerometer3 offsets of Z axis" name="INS_ACC3OFFS_Z" documentation="Accelerometer3 offsets of Z axis. This is setup using the acceleration calibration or level operations" user="Advanced">
<field name="Range">-3.5 3.5</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
<param humanName="Gyro filter cutoff frequency" name="INS_GYRO_FILTER" documentation="Filter cutoff frequency for gyroscopes. This can be set to a lower value to try to cope with very high vibration levels in aircraft. This option takes effect on the next reboot. A value of zero means no filtering (not recommended!)" user="Advanced">
<field name="Range">0 127</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Accel filter cutoff frequency" name="INS_ACCEL_FILTER" documentation="Filter cutoff frequency for accelerometers. This can be set to a lower value to try to cope with very high vibration levels in aircraft. This option takes effect on the next reboot. A value of zero means no filtering (not recommended!)" user="Advanced">
<field name="Range">0 127</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Use first IMU for attitude, velocity and position estimates" name="INS_USE" documentation="Use first IMU for attitude, velocity and position estimates" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Use second IMU for attitude, velocity and position estimates" name="INS_USE2" documentation="Use second IMU for attitude, velocity and position estimates" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Use third IMU for attitude, velocity and position estimates" name="INS_USE3" documentation="Use third IMU for attitude, velocity and position estimates" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Stillness threshold for detecting if we are moving" name="INS_STILL_THRESH" documentation="Threshold to tolerate vibration to determine if vehicle is motionless. This depends on the frame type and if there is a constant vibration due to motors before launch or after landing. Total motionless is about 0.05. Suggested values: Planes/rover use 0.1, multirotors use 1, tradHeli uses 5" user="Advanced">
<field name="Range">0.05 50</field>
</param>
<param humanName="Gyro Calibration scheme" name="INS_GYR_CAL" documentation="Conrols when automatic gyro calibration is performed" user="Advanced">
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<values>
<value code="0">Never</value>
<value code=" 1">Start-up only</value>
</values>
</param>
<param humanName="Accel cal trim option" name="INS_TRIM_OPTION" documentation="Specifies how the accel cal routine determines the trims" user="Advanced">
<values>
<value code="0">Don't adjust the trims</value>
<value code="1">Assume first orientation was level</value>
<value code="2">Assume ACC_BODYFIX is perfectly aligned to the vehicle</value>
</values>
</param>
<param humanName="Body-fixed accelerometer" name="INS_ACC_BODYFIX" documentation="The body-fixed accelerometer to be used for trim calculation" user="Advanced">
<values>
<value code="1">IMU 1</value>
<value code="2">IMU 2</value>
<value code="3">IMU 3</value>
</values>
</param>
<param humanName="IMU accelerometer X position" name="INS_POS1_X" documentation="X position of the first IMU Accelerometer in body frame. Positive X is forward of the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="IMU accelerometer Y position" name="INS_POS1_Y" documentation="Y position of the first IMU accelerometer in body frame. Positive Y is to the right of the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="IMU accelerometer Z position" name="INS_POS1_Z" documentation="Z position of the first IMU accelerometer in body frame. Positive Z is down from the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="IMU accelerometer X position" name="INS_POS2_X" documentation="X position of the second IMU accelerometer in body frame. Positive X is forward of the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="IMU accelerometer Y position" name="INS_POS2_Y" documentation="Y position of the second IMU accelerometer in body frame. Positive Y is to the right of the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="IMU accelerometer Z position" name="INS_POS2_Z" documentation="Z position of the second IMU accelerometer in body frame. Positive Z is down from the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="IMU accelerometer X position" name="INS_POS3_X" documentation="X position of the third IMU accelerometer in body frame. Positive X is forward of the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="IMU accelerometer Y position" name="INS_POS3_Y" documentation="Y position of the third IMU accelerometer in body frame. Positive Y is to the right of the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="IMU accelerometer Z position" name="INS_POS3_Z" documentation="Z position of the third IMU accelerometer in body frame. Positive Z is down from the origin. Attention: The IMU should be located as close to the vehicle c.g. as practical so that the value of this parameter is minimised. Failure to do so can result in noisy navigation velocity measurements due to vibration and IMU gyro noise. If the IMU cannot be moved and velocity noise is a problem, a location closer to the IMU can be used as the body frame origin." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Gyro ID" name="INS_GYR_ID" documentation="Gyro sensor ID, taking into account its type, bus and instance" user="Advanced">
<field name="ReadOnly">True</field>
</param>
<param humanName="Gyro2 ID" name="INS_GYR2_ID" documentation="Gyro2 sensor ID, taking into account its type, bus and instance" user="Advanced">
<field name="ReadOnly">True</field>
</param>
<param humanName="Gyro3 ID" name="INS_GYR3_ID" documentation="Gyro3 sensor ID, taking into account its type, bus and instance" user="Advanced">
<field name="ReadOnly">True</field>
</param>
<param humanName="Accelerometer ID" name="INS_ACC_ID" documentation="Accelerometer sensor ID, taking into account its type, bus and instance" user="Advanced">
<field name="ReadOnly">True</field>
</param>
<param humanName="Accelerometer2 ID" name="INS_ACC2_ID" documentation="Accelerometer2 sensor ID, taking into account its type, bus and instance" user="Advanced">
<field name="ReadOnly">True</field>
</param>
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<param humanName="Accelerometer3 ID" name="INS_ACC3_ID" documentation="Accelerometer3 sensor ID, taking into account its type, bus and instance" user="Advanced">
<field name="ReadOnly">True</field>
</param>
<param humanName="Fast sampling mask" name="INS_FAST_SAMPLE" documentation="Mask of IMUs to enable fast sampling on, if available" user="Advanced">
</param>
</parameters>
<parameters name="LAND_">
<param humanName="Landing slope re-calc threshold" name="LAND_SLOPE_RCALC" documentation="This parameter is used when using a rangefinder during landing for altitude correction from baro drift (RNGFND_LANDING=1) and the altitude correction indicates your altitude is lower than the intended slope path. This value is the threshold of the correction to re-calculate the landing approach slope. Set to zero to keep the original slope all the way down and any detected baro drift will be corrected by pitching/throttling up to snap back to resume the original slope path. Otherwise, when a rangefinder altitude correction exceeds this threshold it will trigger a slope re-calculate to give a shallower slope. This also smoothes out the approach when flying over objects such as trees. Recommend a value of 2m." user="Advanced">
<field name="Range">0 5</field>
<field name="Increment">0.5</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Landing auto-abort slope threshold" name="LAND_ABORT_DEG" documentation="This parameter is used when using a rangefinder during landing for altitude correction from baro drift (RNGFND_LANDING=1) and the altitude correction indicates your actual altitude is higher than the intended slope path. Normally it would pitch down steeply but that can result in a crash with high airspeed so this allows remembering the baro offset and self-abort the landing and come around for another landing with the correct baro offset applied for a perfect slope. An auto-abort go-around will only happen once, next attempt will not auto-abort again. This operation happens entirely automatically in AUTO mode. This value is the delta degrees threshold to trigger the go-around compared to the original slope. Example: if set to 5 deg and the mission planned slope is 15 deg then if the new slope is 21 then it will go-around. Set to 0 to disable. Requires LAND_SLOPE_RCALC > 0." user="Advanced">
<field name="Range">0 90</field>
<field name="Increment">0.1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Landing Pitch" name="LAND_PITCH_CD" documentation="Used in autoland to give the minimum pitch in the final stage of landing (after the flare). This parameter can be used to ensure that the final landing attitude is appropriate for the type of undercarriage on the aircraft. Note that it is a minimum pitch only - the landing code will control pitch above this value to try to achieve the configured landing sink rate." user="Advanced">
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Landing flare altitude" name="LAND_FLARE_ALT" documentation="Altitude in autoland at which to lock heading and flare to the LAND_PITCH_CD pitch. Note that this option is secondary to LAND_FLARE_SEC. For a good landing it preferable that the flare is triggered by LAND_FLARE_SEC." user="Advanced">
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Landing flare time" name="LAND_FLARE_SEC" documentation="Vertical time before landing point at which to lock heading and flare with the motor stopped. This is vertical time, and is calculated based solely on the current height above the ground and the current descent rate. Set to 0 if you only wish to flare based on altitude (see LAND_FLARE_ALT)." user="Advanced">
<field name="Increment">0.1</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Landing pre-flare altitude" name="LAND_PF_ALT" documentation="Altitude to trigger pre-flare flight stage where LAND_PF_ARSPD controls airspeed. The pre-flare flight stage trigger works just like LAND_FLARE_ALT but higher. Disabled when LAND_PF_ARSPD is 0." user="Advanced">
<field name="Range">0 30</field>
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Landing pre-flare time" name="LAND_PF_SEC" documentation="Vertical time to ground to trigger pre-flare flight stage where LAND_PF_ARSPD controls airspeed. This pre-flare flight stage trigger works just like LAND_FLARE_SEC but earlier. Disabled when LAND_PF_ARSPD is 0." user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">0.1</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Landing pre-flare airspeed" name="LAND_PF_ARSPD" documentation="Desired airspeed during pre-flare flight stage. This is useful to reduce airspeed just before the flare. Use 0 to disable." user="Advanced">
<field name="Range">0 30</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Landing throttle slew rate" name="LAND_THR_SLEW" documentation="This parameter sets the slew rate for the throttle during auto landing. When this is zero the THR_SLEWRATE parameter is used during landing. The value is a percentage throttle change per second, so a value of 20 means to advance the throttle over 5 seconds on landing. Values below 50 are not recommended as it may cause a stall when airspeed is low and you can not throttle up fast enough." user="User">
<field name="Range">0 127</field>
<field name="Increment">1</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Landing disarm delay" name="LAND_DISARMDELAY" documentation="After a landing has completed using a LAND waypoint, automatically disarm after this many seconds have passed. Use 0 to not disarm." user="Advanced">
<field name="Range">0 127</field>
<field name="Increment">1</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Set servos to neutral after landing" name="LAND_THEN_NEUTRL" documentation="When enabled, after an autoland and auto-disarm via LAND_DISARMDELAY happens then set all servos to neutral. This is helpful when an aircraft has a rough landing upside down or a crazy angle causing the servos to strain." user="Advanced">
<values>
<value code="0">Disabled</value>
<value code=" 1">Servos to Neutral</value>
<value code=" 2">Servos to Zero PWM</value>
</values>
</param>
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<param humanName="Landing abort using throttle" name="LAND_ABORT_THR" documentation="Allow a landing abort to trigger with a throttle > 95%" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code=" 1">Enabled</value>
</values>
</param>
<param humanName="Landing flap percentage" name="LAND_FLAP_PERCNT" documentation="The amount of flaps (as a percentage) to apply in the landing approach and flare of an automatic landing" user="Advanced">
<field name="Range">0 100</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Auto-landing type" name="LAND_TYPE" documentation="Specifies the auto-landing type to use" user="Standard">
<values>
<value code="0">Standard Glide Slope</value>
<value code=" 1">Deepstall</value>
</values>
</param>
</parameters>
<parameters name="LAND_DS_">
<param humanName="Deepstall forward velocity" name="LAND_DS_V_FWD" documentation="The forward velocity of the aircraft while stalled" user="Advanced">
<field name="Range">0 20</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Deepstall slope a" name="LAND_DS_SLOPE_A" documentation="The a component of distance = a*wind + b" user="Advanced">
</param>
<param humanName="Deepstall slope b" name="LAND_DS_SLOPE_B" documentation="The a component of distance = a*wind + b" user="Advanced">
</param>
<param humanName="Deepstall approach extension" name="LAND_DS_APP_EXT" documentation="The forward velocity of the aircraft while stalled" user="Advanced">
<field name="Range">10 200</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Deepstall veloicty down" name="LAND_DS_V_DWN" documentation="The downward velocity of the aircraft while stalled" user="Advanced">
<field name="Range">0 20</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Deepstall slew speed" name="LAND_DS_SLEW_SPD" documentation="The speed at which the elevator slews to deepstall" user="Advanced">
<field name="Range">0 2</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Deepstall elevator PWM" name="LAND_DS_ELEV_PWM" documentation="The PWM value in microseconds for the elevator at full deflection in deepstall" user="Advanced">
<field name="Range">900 2100</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Deepstall enabled airspeed" name="LAND_DS_ARSP_MAX" documentation="The maximum aispeed where the deepstall steering controller is allowed to have control" user="Advanced">
<field name="Range">5 20</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Deepstall minimum derating airspeed" name="LAND_DS_ARSP_MIN" documentation="Deepstall lowest airspeed where the deepstall controller isn't allowed full control" user="Advanced">
<field name="Range">5 20</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Deepstall L1 period" name="LAND_DS_L1" documentation="Deepstall L1 navigational controller period" user="Advanced">
<field name="Range">5 50</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Deepstall L1 I gain" name="LAND_DS_L1_I" documentation="Deepstall L1 integratior gain" user="Advanced">
<field name="Range">0 1</field>
</param>
</parameters>
<parameters name="LAND_DS_DS_">
<param humanName="PID Proportional Gain" name="LAND_DS_DS_P" documentation="P Gain which produces an output value that is proportional to the current error value">
</param>
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<param humanName="PID Integral Gain" name="LAND_DS_DS_I" documentation="I Gain which produces an output that is proportional to both the magnitude and the duration of the error">
</param>
<param humanName="PID Derivative Gain" name="LAND_DS_DS_D" documentation="D Gain which produces an output that is proportional to the rate of change of the error">
</param>
<param humanName="PID Integral Maximum" name="LAND_DS_DS_IMAX" documentation="The maximum/minimum value that the I term can output">
</param>
</parameters>
<parameters name="LOG">
<param humanName="DataFlash Backend Storage type" name="LOG_BACKEND_TYPE" documentation="0 for None, 1 for File, 2 for dataflash mavlink, 3 for both file and dataflash" user="Standard">
<values>
<value code="0">None</value>
<value code="1">File</value>
<value code="2">MAVLink</value>
<value code="3">BothFileAndMAVLink</value>
</values>
</param>
<param humanName="Maximum DataFlash File Backend buffer size (in kilobytes)" name="LOG_FILE_BUFSIZE" documentation='The DataFlash_File backend uses a buffer to store data before writing to the block device. Raising this value may reduce "gaps" in your SD card logging. This buffer size may be reduced depending on available memory. PixHawk requires at least 4 kilobytes. Maximum value available here is 64 kilobytes.' user="Standard">
</param>
<param humanName="Enable logging while disarmed" name="LOG_DISARMED" documentation="If LOG_DISARMED is set to 1 then logging will be enabled while disarmed. This can make for very large logfiles but can help a lot when tracking down startup issues" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Enable logging of information needed for Replay" name="LOG_REPLAY" documentation="If LOG_REPLAY is set to 1 then the EKF2 state estimator will log detailed information needed for diagnosing problems with the Kalman filter. It is suggested that you also raise LOG_FILE_BUFSIZE to give more buffer space for logging and use a high quality microSD card to ensure no sensor data is lost" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Stop logging to current file on disarm" name="LOG_FILE_DSRMROT" documentation="When set, the current log file is closed when the vehicle is disarmed. If LOG_DISARMED is set then a fresh log will be opened." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
</parameters>
<parameters name="MIS_">
<param humanName="Total mission commands" name="MIS_TOTAL" documentation="The number of mission mission items that has been loaded by the ground station. Do not change this manually." user="Advanced">
<field name="Range">0 32766</field>
<field name="Increment">1</field>
</param>
<param humanName="Mission Restart when entering Auto mode" name="MIS_RESTART" documentation="Controls mission starting point when entering Auto mode (either restart from beginning of mission or resume from last command run)" user="Advanced">
<values>
<value code="0">Resume Mission</value>
<value code=" 1">Restart Mission</value>
</values>
</param>
</parameters>
<parameters name="MNT">
<param humanName="Mount default operating mode" name="MNT_DEFLT_MODE" documentation="Mount default operating mode on startup and after control is returned from autopilot" user="Standard">
<values>
<value code="0">Retracted</value>
<value code="1">Neutral</value>
<value code="2">MavLink Targeting</value>
<value code="3">RC Targeting</value>
<value code="4">GPS Point</value>
</values>
</param>
<param humanName="Mount roll angle when in retracted position" name="MNT_RETRACT_X" documentation="Mount roll angle when in retracted position" user="Standard">
<field name="Range">-180.00 179.99</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Mount tilt/pitch angle when in retracted position" name="MNT_RETRACT_Y" documentation="Mount tilt/pitch angle when in retracted position" user="Standard">
<field name="Range">-180.00 179.99</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
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</param>
<param humanName="Mount yaw/pan angle when in retracted position" name="MNT_RETRACT_Z" documentation="Mount yaw/pan angle when in retracted position" user="Standard">
<field name="Range">-180.00 179.99</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Mount roll angle when in neutral position" name="MNT_NEUTRAL_X" documentation="Mount roll angle when in neutral position" user="Standard">
<field name="Range">-180.00 179.99</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Mount tilt/pitch angle when in neutral position" name="MNT_NEUTRAL_Y" documentation="Mount tilt/pitch angle when in neutral position" user="Standard">
<field name="Range">-180.00 179.99</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Mount pan/yaw angle when in neutral position" name="MNT_NEUTRAL_Z" documentation="Mount pan/yaw angle when in neutral position" user="Standard">
<field name="Range">-180.00 179.99</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Stabilize mount's roll angle" name="MNT_STAB_ROLL" documentation="enable roll stabilisation relative to Earth" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Stabilize mount's pitch/tilt angle" name="MNT_STAB_TILT" documentation="enable tilt/pitch stabilisation relative to Earth" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Stabilize mount pan/yaw angle" name="MNT_STAB_PAN" documentation="enable pan/yaw stabilisation relative to Earth" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="roll RC input channel" name="MNT_RC_IN_ROLL" documentation="0 for none, any other for the RC channel to be used to control roll movements" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="5">RC5</value>
<value code="6">RC6</value>
<value code="7">RC7</value>
<value code="8">RC8</value>
<value code="9">RC9</value>
<value code="10">RC10</value>
<value code="11">RC11</value>
<value code="12">RC12</value>
</values>
</param>
<param humanName="Minimum roll angle" name="MNT_ANGMIN_ROL" documentation="Minimum physical roll angular position of mount." user="Standard">
<field name="Range">-18000 17999</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Maximum roll angle" name="MNT_ANGMAX_ROL" documentation="Maximum physical roll angular position of the mount" user="Standard">
<field name="Range">-18000 17999</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="tilt (pitch) RC input channel" name="MNT_RC_IN_TILT" documentation="0 for none, any other for the RC channel to be used to control tilt (pitch) movements" user="Standard">
<values>
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<value code="0">Disabled</value>
<value code="5">RC5</value>
<value code="6">RC6</value>
<value code="7">RC7</value>
<value code="8">RC8</value>
<value code="9">RC9</value>
<value code="10">RC10</value>
<value code="11">RC11</value>
<value code="12">RC12</value>
</values>
</param>
<param humanName="Minimum tilt angle" name="MNT_ANGMIN_TIL" documentation="Minimum physical tilt (pitch) angular position of mount." user="Standard">
<field name="Range">-18000 17999</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Maximum tilt angle" name="MNT_ANGMAX_TIL" documentation="Maximum physical tilt (pitch) angular position of the mount" user="Standard">
<field name="Range">-18000 17999</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="pan (yaw) RC input channel" name="MNT_RC_IN_PAN" documentation="0 for none, any other for the RC channel to be used to control pan (yaw) movements" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="5">RC5</value>
<value code="6">RC6</value>
<value code="7">RC7</value>
<value code="8">RC8</value>
<value code="9">RC9</value>
<value code="10">RC10</value>
<value code="11">RC11</value>
<value code="12">RC12</value>
</values>
</param>
<param humanName="Minimum pan angle" name="MNT_ANGMIN_PAN" documentation="Minimum physical pan (yaw) angular position of mount." user="Standard">
<field name="Range">-18000 17999</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Maximum pan angle" name="MNT_ANGMAX_PAN" documentation="Maximum physical pan (yaw) angular position of the mount" user="Standard">
<field name="Range">-18000 17999</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="mount joystick speed" name="MNT_JSTICK_SPD" documentation="0 for position control, small for low speeds, 100 for max speed. A good general value is 10 which gives a movement speed of 3 degrees per second." user="Standard">
<field name="Range">0 100</field>
<field name="Increment">1</field>
</param>
<param humanName="Roll stabilization lead time" name="MNT_LEAD_RLL" documentation="Causes the servo angle output to lead the current angle of the vehicle by some amount of time based on current angular rate, compensating for servo delay. Increase until the servo is responsive but doesn't overshoot. Does nothing with pan stabilization enabled." user="Standard">
<field name="Range">0.0 0.2</field>
<field name="Increment">.005</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Pitch stabilization lead time" name="MNT_LEAD_PTCH" documentation="Causes the servo angle output to lead the current angle of the vehicle by some amount of time based on current angular rate. Increase until the servo is responsive but doesn't overshoot. Does nothing with pan stabilization enabled." user="Standard">
<field name="Range">0.0 0.2</field>
<field name="Increment">.005</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Mount Type" name="MNT_TYPE" documentation="Mount Type (None, Servo or MAVLink)" user="Standard">
<values>
<value code="0">None</value>
<value code=" 1">Servo</value>
<value code=" 2">3DR Solo</value>
<value code=" 3">Alexmos Serial</value>
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<value code=" 4">SToRM32 MAVLink</value>
<value code=" 5">SToRM32 Serial</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Mount default operating mode" name="MNT2_DEFLT_MODE" documentation="Mount default operating mode on startup and after control is returned from autopilot" user="Standard">
<values>
<value code="0">Retracted</value>
<value code="1">Neutral</value>
<value code="2">MavLink Targeting</value>
<value code="3">RC Targeting</value>
<value code="4">GPS Point</value>
</values>
</param>
<param humanName="Mount2 roll angle when in retracted position" name="MNT2_RETRACT_X" documentation="Mount2 roll angle when in retracted position" user="Standard">
<field name="Range">-180.00 179.99</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Mount2 tilt/pitch angle when in retracted position" name="MNT2_RETRACT_Y" documentation="Mount2 tilt/pitch angle when in retracted position" user="Standard">
<field name="Range">-180.00 179.99</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Mount2 yaw/pan angle when in retracted position" name="MNT2_RETRACT_Z" documentation="Mount2 yaw/pan angle when in retracted position" user="Standard">
<field name="Range">-180.00 179.99</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Mount2 roll angle when in neutral position" name="MNT2_NEUTRAL_X" documentation="Mount2 roll angle when in neutral position" user="Standard">
<field name="Range">-180.00 179.99</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Mount2 tilt/pitch angle when in neutral position" name="MNT2_NEUTRAL_Y" documentation="Mount2 tilt/pitch angle when in neutral position" user="Standard">
<field name="Range">-180.00 179.99</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Mount2 pan/yaw angle when in neutral position" name="MNT2_NEUTRAL_Z" documentation="Mount2 pan/yaw angle when in neutral position" user="Standard">
<field name="Range">-180.00 179.99</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Stabilize Mount2's roll angle" name="MNT2_STAB_ROLL" documentation="enable roll stabilisation relative to Earth" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Stabilize Mount2's pitch/tilt angle" name="MNT2_STAB_TILT" documentation="enable tilt/pitch stabilisation relative to Earth" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Stabilize mount2 pan/yaw angle" name="MNT2_STAB_PAN" documentation="enable pan/yaw stabilisation relative to Earth" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Mount2's roll RC input channel" name="MNT2_RC_IN_ROLL" documentation="0 for none, any other for the RC channel to be used to control roll movements" user="Standard">
<values>
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<value code="0">Disabled</value>
<value code="5">RC5</value>
<value code="6">RC6</value>
<value code="7">RC7</value>
<value code="8">RC8</value>
<value code="9">RC9</value>
<value code="10">RC10</value>
<value code="11">RC11</value>
<value code="12">RC12</value>
</values>
</param>
<param humanName="Mount2's minimum roll angle" name="MNT2_ANGMIN_ROL" documentation="Mount2's minimum physical roll angular position" user="Standard">
<field name="Range">-18000 17999</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Mount2's maximum roll angle" name="MNT2_ANGMAX_ROL" documentation="Mount2's maximum physical roll angular position" user="Standard">
<field name="Range">-18000 17999</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Mount2's tilt (pitch) RC input channel" name="MNT2_RC_IN_TILT" documentation="0 for none, any other for the RC channel to be used to control tilt (pitch) movements" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="5">RC5</value>
<value code="6">RC6</value>
<value code="7">RC7</value>
<value code="8">RC8</value>
<value code="9">RC9</value>
<value code="10">RC10</value>
<value code="11">RC11</value>
<value code="12">RC12</value>
</values>
</param>
<param humanName="Mount2's minimum tilt angle" name="MNT2_ANGMIN_TIL" documentation="Mount2's minimum physical tilt (pitch) angular position" user="Standard">
<field name="Range">-18000 17999</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Mount2's maximum tilt angle" name="MNT2_ANGMAX_TIL" documentation="Mount2's maximum physical tilt (pitch) angular position" user="Standard">
<field name="Range">-18000 17999</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Mount2's pan (yaw) RC input channel" name="MNT2_RC_IN_PAN" documentation="0 for none, any other for the RC channel to be used to control pan (yaw) movements" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="5">RC5</value>
<value code="6">RC6</value>
<value code="7">RC7</value>
<value code="8">RC8</value>
<value code="9">RC9</value>
<value code="10">RC10</value>
<value code="11">RC11</value>
<value code="12">RC12</value>
</values>
</param>
<param humanName="Mount2's minimum pan angle" name="MNT2_ANGMIN_PAN" documentation="Mount2's minimum physical pan (yaw) angular position" user="Standard">
<field name="Range">-18000 17999</field>
<field name="Increment">1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Mount2's maximum pan angle" name="MNT2_ANGMAX_PAN" documentation="MOunt2's maximum physical pan (yaw) angular position" user="Standard">
<field name="Range">-18000 17999</field>
<field name="Increment">1</field>
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3782
3783
3784
3785
3786
3787
3788
3789
3790
3791
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3793
3794
3795
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<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Mount2's Roll stabilization lead time" name="MNT2_LEAD_RLL" documentation="Causes the servo angle output to lead the current angle of the vehicle by some amount of time based on current angular rate, compensating for servo delay. Increase until the servo is responsive but doesn't overshoot. Does nothing with pan stabilization enabled." user="Standard">
<field name="Range">0.0 0.2</field>
<field name="Increment">.005</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Mount2's Pitch stabilization lead time" name="MNT2_LEAD_PTCH" documentation="Causes the servo angle output to lead the current angle of the vehicle by some amount of time based on current angular rate. Increase until the servo is responsive but doesn't overshoot. Does nothing with pan stabilization enabled." user="Standard">
<field name="Range">0.0 0.2</field>
<field name="Increment">.005</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Mount2 Type" name="MNT2_TYPE" documentation="Mount Type (None, Servo or MAVLink)" user="Standard">
<values>
<value code="0">None</value>
<value code=" 1">Servo</value>
<value code=" 2">3DR Solo</value>
<value code=" 3">Alexmos Serial</value>
<value code=" 4">SToRM32 MAVLink</value>
<value code=" 5">SToRM32 Serial</value>
</values>
</param>
</parameters>
<parameters name="NAVL1_">
<param humanName="L1 control period" name="NAVL1_PERIOD" documentation="Period in seconds of L1 tracking loop. This parameter is the primary control for agressiveness of turns in auto mode. This needs to be larger for less responsive airframes. The default of 20 is quite conservative, but for most RC aircraft will lead to reasonable flight. For smaller more agile aircraft a value closer to 15 is appropriate, or even as low as 10 for some very agile aircraft. When tuning, change this value in small increments, as a value that is much too small (say 5 or 10 below the right value) can lead to very radical turns, and a risk of stalling." user="Standard">
<field name="Range">1 60</field>
<field name="Increment">1</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="L1 control damping ratio" name="NAVL1_DAMPING" documentation="Damping ratio for L1 control. Increase this in increments of 0.05 if you are getting overshoot in path tracking. You should not need a value below 0.7 or above 0.85." user="Advanced">
<field name="Range">0.6 1.0</field>
<field name="Increment">0.05</field>
</param>
<param humanName="L1 control crosstrack integrator gain" name="NAVL1_XTRACK_I" documentation="Crosstrack error integrator gain. This gain is applied to the crosstrack error to ensure it converges to zero. Set to zero to disable. Smaller values converge slower, higher values will cause crosstrack error oscillation." user="Advanced">
<field name="Range">0 0.1</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Loiter Radius Bank Angle Limit" name="NAVL1_LIM_BANK" documentation="The sealevel bank angle limit for a continous loiter. (Used to calculate airframe loading limits at higher altitudes). Setting to 0, will instead just scale the loiter radius directly" user="Advanced">
<field name="Range">0 89</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
</parameters>
<parameters name="NTF_">
<param humanName="LED Brightness" name="NTF_LED_BRIGHT" documentation="Select the RGB LED brightness level. When USB is connected brightness will never be higher than low regardless of the setting." user="Advanced">
<values>
<value code="0">Off</value>
<value code="1">Low</value>
<value code="2">Medium</value>
<value code="3">High</value>
</values>
</param>
<param humanName="Buzzer enable" name="NTF_BUZZ_ENABLE" documentation="Enable or disable the buzzer. Only for Linux and PX4 based boards." user="Advanced">
<values>
<value code="0">Disable</value>
<value code="1">Enable</value>
</values>
</param>
<param humanName="Setup for MAVLink LED override" name="NTF_LED_OVERRIDE" documentation="This sets up the board RGB LED for override by MAVLink. Normal notify LED control is disabled" user="Advanced">
<values>
<value code="0">Disable</value>
<value code="1">Enable</value>
</values>
</param>
<param humanName="Type of on-board I2C display" name="NTF_DISPLAY_TYPE" documentation="This sets up the type of on-board I2C display. Disabled by default." user="Advanced">
<values>
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<value code="0">Disable</value>
<value code="1">ssd1306</value>
<value code="2">sh1106</value>
</values>
</param>
<param humanName="OreoLED Theme" name="NTF_OREO_THEME" documentation="Enable/Disable Solo Oreo LED driver, 0 to disable, 1 for Aircraft theme, 2 for Rover theme" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="1">Aircraft</value>
<value code="2">Rover</value>
</values>
</param>
</parameters>
<parameters name="PTCH2SRV_">
<param humanName="Pitch Time Constant" name="PTCH2SRV_TCONST" documentation="This controls the time constant in seconds from demanded to achieved pitch angle. A value of 0.5 is a good default and will work with nearly all models. Advanced users may want to reduce this time to obtain a faster response but there is no point setting a time less than the aircraft can achieve." user="Advanced">
<field name="Range">0.4 1.0</field>
<field name="Increment">0.1</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Proportional Gain" name="PTCH2SRV_P" documentation="This is the gain from pitch angle to elevator. This gain works the same way as PTCH2SRV_P in the old PID controller and can be set to the same value." user="User">
<field name="Range">0.1 3.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Damping Gain" name="PTCH2SRV_D" documentation="This is the gain from pitch rate to elevator. This adjusts the damping of the pitch control loop. It has the same effect as PTCH2SRV_D in the old PID controller and can be set to the same value, but without the spikes in servo demands. This gain helps to reduce pitching in turbulence. Some airframes such as flying wings that have poor pitch damping can benefit from increasing this gain term. This should be increased in 0.01 increments as too high a value can lead to a high frequency pitch oscillation that could overstress the airframe." user="User">
<field name="Range">0 0.1</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Integrator Gain" name="PTCH2SRV_I" documentation="This is the gain applied to the integral of pitch angle. It has the same effect as PTCH2SRV_I in the old PID controller and can be set to the same value. Increasing this gain causes the controller to trim out constant offsets between demanded and measured pitch angle." user="User">
<field name="Range">0 0.5</field>
<field name="Increment">0.05</field>
</param>
<param humanName="Pitch up max rate" name="PTCH2SRV_RMAX_UP" documentation="This sets the maximum nose up pitch rate that the controller will demand (degrees/sec). Setting it to zero disables the limit." user="Advanced">
<field name="Range">0 100</field>
<field name="Increment">1</field>
<field name="Units">deg/s</field>
<field name="UnitText">degrees per second</field>
</param>
<param humanName="Pitch down max rate" name="PTCH2SRV_RMAX_DN" documentation="This sets the maximum nose down pitch rate that the controller will demand (degrees/sec). Setting it to zero disables the limit." user="Advanced">
<field name="Range">0 100</field>
<field name="Increment">1</field>
<field name="Units">deg/s</field>
<field name="UnitText">degrees per second</field>
</param>
<param humanName="Roll compensation" name="PTCH2SRV_RLL" documentation="This is the gain term that is applied to the pitch rate offset calculated as required to keep the nose level during turns. The default value is 1 which will work for all models. Advanced users can use it to correct for height variation in turns. If height is lost initially in turns this can be increased in small increments of 0.05 to compensate. If height is gained initially in turns then it can be decreased." user="User">
<field name="Range">0.7 1.5</field>
<field name="Increment">0.05</field>
</param>
<param humanName="Integrator limit" name="PTCH2SRV_IMAX" documentation="This limits the number of centi-degrees of elevator over which the integrator will operate. At the default setting of 3000 centi-degrees, the integrator will be limited to +- 30 degrees of servo travel. The maximum servo deflection is +- 45 degrees, so the default value represents a 2/3rd of the total control throw which is adequate for most aircraft unless they are severely out of trim or have very limited elevator control effectiveness." user="Advanced">
<field name="Range">0 4500</field>
<field name="Increment">1</field>
</param>
<param humanName="Feed forward Gain" name="PTCH2SRV_FF" documentation="This is the gain from demanded rate to elevator output. " user="User">
<field name="Range">0.1 4.0</field>
<field name="Increment">0.1</field>
</param>
</parameters>
<parameters name="Q_">
<param humanName="Enable QuadPlane" name="Q_ENABLE" documentation="This enables QuadPlane functionality, assuming multicopter motors start on output 5. If this is set to 2 then when starting AUTO mode it will initially be in VTOL AUTO mode." user="Standard">
<values>
<value code="0">Disable</value>
<value code="1">Enable</value>
<value code="2">Enable VTOL AUTO</value>
</values>
</param>
<param humanName="Angle Max" name="Q_ANGLE_MAX" documentation="Maximum lean angle in all VTOL flight modes" user="Advanced">
<field name="Range">1000 8000</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
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<param humanName="Transition time" name="Q_TRANSITION_MS" documentation="Transition time in milliseconds after minimum airspeed is reached" user="Advanced">
<field name="Range">0 30000</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
</param>
<param humanName="Position (vertical) controller P gain" name="Q_PZ_P" documentation="Position (vertical) controller P gain. Converts the difference between the desired altitude and actual altitude into a climb or descent rate which is passed to the throttle rate controller" user="Standard">
<field name="Range">1.000 3.000</field>
</param>
<param humanName="Position (horizonal) controller P gain" name="Q_PXY_P" documentation="Loiter position controller P gain. Converts the distance (in the latitude direction) to the target location into a desired speed which is then passed to the loiter latitude rate controller" user="Standard">
<field name="Range">0.500 2.000</field>
</param>
<param humanName="Velocity (horizontal) P gain" name="Q_VXY_P" documentation="Velocity (horizontal) P gain. Converts the difference between desired velocity to a target acceleration" user="Advanced">
<field name="Range">0.1 6.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Velocity (horizontal) I gain" name="Q_VXY_I" documentation="Velocity (horizontal) I gain. Corrects long-term difference in desired velocity to a target acceleration" user="Advanced">
<field name="Range">0.02 1.00</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Velocity (horizontal) integrator maximum" name="Q_VXY_IMAX" documentation="Velocity (horizontal) integrator maximum. Constrains the target acceleration that the I gain will output" user="Advanced">
<field name="Range">0 4500</field>
<field name="Increment">10</field>
<field name="Units">cm/s/s</field>
<field name="UnitText">centimeters per square second</field>
</param>
<param humanName="Velocity (vertical) P gain" name="Q_VZ_P" documentation="Velocity (vertical) P gain. Converts the difference between desired vertical speed and actual speed into a desired acceleration that is passed to the throttle acceleration controller" user="Standard">
<field name="Range">1.000 8.000</field>
</param>
<param humanName="Throttle acceleration controller P gain" name="Q_AZ_P" documentation="Throttle acceleration controller P gain. Converts the difference between desired vertical acceleration and actual acceleration into a motor output" user="Standard">
<field name="Range">0.500 1.500</field>
</param>
<param humanName="Throttle acceleration controller I gain" name="Q_AZ_I" documentation="Throttle acceleration controller I gain. Corrects long-term difference in desired vertical acceleration and actual acceleration" user="Standard">
<field name="Range">0.000 3.000</field>
</param>
<param humanName="Throttle acceleration controller I gain maximum" name="Q_AZ_IMAX" documentation="Throttle acceleration controller I gain maximum. Constrains the maximum pwm that the I term will generate" user="Standard">
<field name="Range">0 1000</field>
<field name="Units">d%</field>
<field name="UnitText">decipercent</field>
</param>
<param humanName="Throttle acceleration controller D gain" name="Q_AZ_D" documentation="Throttle acceleration controller D gain. Compensates for short-term change in desired vertical acceleration vs actual acceleration" user="Standard">
<field name="Range">0.000 0.400</field>
</param>
<param humanName="Throttle acceleration filter" name="Q_AZ_FILT_HZ" documentation="Filter applied to acceleration to reduce noise. Lower values reduce noise but add delay." user="Standard">
<field name="Range">1.000 100.000</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Pilot maximum vertical speed" name="Q_VELZ_MAX" documentation="The maximum vertical velocity the pilot may request in cm/s" user="Standard">
<field name="Range">50 500</field>
<field name="Increment">10</field>
<field name="Units">cm/s</field>
<field name="UnitText">centimeters per second</field>
</param>
<param humanName="Pilot vertical acceleration" name="Q_ACCEL_Z" documentation="The vertical acceleration used when pilot is controlling the altitude" user="Standard">
<field name="Range">50 500</field>
<field name="Increment">10</field>
<field name="Units">cm/s/s</field>
<field name="UnitText">centimeters per square second</field>
</param>
<param humanName="RC output speed in Hz" name="Q_RC_SPEED" documentation="This is the PWM refresh rate in Hz for QuadPlane quad motors" user="Standard">
<field name="Range">50 500</field>
<field name="Increment">10</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Minimum PWM output" name="Q_THR_MIN_PWM" documentation="This is the minimum PWM output for the quad motors" user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
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</param>
<param humanName="Maximum PWM output" name="Q_THR_MAX_PWM" documentation="This is the maximum PWM output for the quad motors" user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Quadplane assistance speed" name="Q_ASSIST_SPEED" documentation="This is the speed below which the quad motors will provide stability and lift assistance in fixed wing modes. Zero means no assistance except during transition" user="Standard">
<field name="Range">0 100</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Maximum yaw rate" name="Q_YAW_RATE_MAX" documentation="This is the maximum yaw rate for pilot input on rudder stick in degrees/second" user="Standard">
<field name="Range">50 500</field>
<field name="Increment">1</field>
<field name="Units">deg/s</field>
<field name="UnitText">degrees per second</field>
</param>
<param humanName="Land speed" name="Q_LAND_SPEED" documentation="The descent speed for the final stage of landing in cm/s" user="Standard">
<field name="Range">30 200</field>
<field name="Increment">10</field>
<field name="Units">cm/s</field>
<field name="UnitText">centimeters per second</field>
</param>
<param humanName="Land final altitude" name="Q_LAND_FINAL_ALT" documentation="The altitude at which we should switch to Q_LAND_SPEED descent rate" user="Standard">
<field name="Range">0.5 50</field>
<field name="Increment">0.1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Transition max pitch" name="Q_TRAN_PIT_MAX" documentation="Maximum pitch during transition to auto fixed wing flight" user="Standard">
<field name="Range">0 30</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Frame Class" name="Q_FRAME_CLASS" documentation="Controls major frame class for multicopter component" user="Standard">
<values>
<value code="0">Undefined</value>
<value code=" 1">Quad</value>
<value code=" 2">Hexa</value>
<value code=" 3">Octa</value>
<value code=" 4">OctaQuad</value>
<value code=" 5">Y6</value>
<value code=" 7">Tri</value>
<value code=" 10"> TailSitter</value>
</values>
</param>
<param humanName="Frame Type (+, X or V)" name="Q_FRAME_TYPE" documentation="Controls motor mixing for multicopter component" user="Standard">
<values>
<value code="0">Plus</value>
<value code=" 1">X</value>
<value code=" 2">V</value>
<value code=" 3">H</value>
<value code=" 4">V-Tail</value>
<value code=" 5">A-Tail</value>
<value code=" 10">Y6B</value>
<value code=" 11">Y6F</value>
</values>
</param>
<param humanName="Forward velocity hold gain" name="Q_VFWD_GAIN" documentation="Controls use of forward motor in vtol modes. If this is zero then the forward motor will not be used for position control in VTOL modes. A value of 0.05 is a good place to start if you want to use the forward motor for position control. No forward motor will be used in QSTABILIZE or QHOVER modes. Use QLOITER for position hold with the forward motor." user="Standard">
<field name="Range">0 0.5</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Weathervaning gain" name="Q_WVANE_GAIN" documentation="This controls the tendency to yaw to face into the wind. A value of 0.1 is to start with and will give a slow turn into the wind. Use a value of 0.4 for more rapid response. The weathervaning works by turning into the direction of roll." user="Standard">
<field name="Range">0 1</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Weathervaning min roll" name="Q_WVANE_MINROLL" documentation="This set the minimum roll in degrees before active weathervaning will start. This may need to be larger if your aircraft has bad roll trim." user="Standard">
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<field name="Range">0 10</field>
<field name="Increment">0.1</field>
</param>
<param humanName="QRTL return altitude" name="Q_RTL_ALT" documentation="The altitude which QRTL mode heads to initially" user="Standard">
<field name="Range">1 200</field>
<field name="Increment">1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="VTOL RTL mode" name="Q_RTL_MODE" documentation="If this is set to 1 then an RTL will change to QRTL when within RTL_RADIUS meters of the RTL destination" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Tiltrotor mask" name="Q_TILT_MASK" documentation="This is a bitmask of motors that are tiltable in a tiltrotor (or tiltwing). The mask is in terms of the standard motor order for the frame type." user="Standard">
</param>
<param humanName="Tiltrotor upwards tilt rate" name="Q_TILT_RATE_UP" documentation="This is the maximum speed at which the motor angle will change for a tiltrotor when moving from forward flight to hover" user="Standard">
<field name="Range">10 300</field>
<field name="Increment">1</field>
<field name="Units">deg/s</field>
<field name="UnitText">degrees per second</field>
</param>
<param humanName="Tiltrotor maximum VTOL angle" name="Q_TILT_MAX" documentation="This is the maximum angle of the tiltable motors at which multicopter control will be enabled. Beyond this angle the plane will fly solely as a fixed wing aircraft and the motors will tilt to their maximum angle at the TILT_RATE" user="Standard">
<field name="Range">20 80</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Enable VTOL in GUIDED mode" name="Q_GUIDED_MODE" documentation="This enables use of VTOL in guided mode. When enabled the aircraft will switch to VTOL flight when the guided destination is reached and hover at the destination." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="ESC Calibration" name="Q_ESC_CAL" documentation="This is used to calibrate the throttle range of the VTOL motors. Please read http://ardupilot.org/plane/docs/quadplane-esc-calibration.html before using. This parameter is automatically set back to 0 on every boot. This parameter only takes effect in QSTABILIZE mode. When set to 1 the output of all motors will come directly from the throttle stick when armed, and will be zero when disarmed. When set to 2 the output of all motors will be maximum when armed and zero when disarmed. Make sure you remove all properllers before using." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">ThrottleInput</value>
<value code="2">FullInput</value>
</values>
</param>
<param humanName="Forward velocity alt cutoff" name="Q_VFWD_ALT" documentation="Controls altitude to disable forward velocity assist when below this relative altitude. This is useful to keep the forward velocity propeller from hitting the ground. Rangefinder height data is incorporated when available." user="Standard">
<field name="Range">0 10</field>
<field name="Increment">0.25</field>
</param>
<param humanName="Cut IC engine on landing" name="Q_LAND_ICE_CUT" documentation="This controls stopping an internal combustion engine in the final landing stage of a VTOL. This is important for aircraft where the forward thrust engine may experience prop-strike if left running during landing. This requires the engine controls are enabled using the ICE_* parameters." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">Enabled</value>
</values>
</param>
<param humanName="Quadplane assistance angle" name="Q_ASSIST_ANGLE" documentation="This is the angular error in attitude beyond which the quadplane VTOL motors will provide stability assistance. This will only be used if Q_ASSIST_SPEED is also non-zero. Assistance will be given if the attitude is outside the normal attitude limits by at least 5 degrees and the angular error in roll or pitch is greater than this angle for at least 1 second. Set to zero to disable angle assistance." user="Standard">
<field name="Range">0 90</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Tiltrotor type" name="Q_TILT_TYPE" documentation="This is the type of tiltrotor when TILT_MASK is non-zero. A continuous tiltrotor can tilt the rotors to any angle on demand. A binary tiltrotor assumes a retract style servo where the servo is either fully forward or fully up. In both cases the servo can't move faster than Q_TILT_RATE. A vectored yaw tiltrotor will use the tilt of the motors to control yaw in hover">
<values>
<value code="0">Continuous</value>
<value code="1">Binary</value>
<value code="2">VectoredYaw</value>
</values>
</param>
<param humanName="Tailsitter transition angle" name="Q_TAILSIT_ANGLE" documentation="This is the angle at which tailsitter aircraft will change from VTOL control to fixed wing control.">
<field name="Range">5 80</field>
</param>
<param humanName="Tiltrotor downwards tilt rate" name="Q_TILT_RATE_DN" documentation="This is the maximum speed at which the motor angle will change for a tiltrotor when moving from hover to forward flight. When this is zero the Q_TILT_RATE_UP value is used." user="Standard">
<field name="Range">10 300</field>
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<field name="Increment">1</field>
<field name="Units">deg/s</field>
<field name="UnitText">degrees per second</field>
</param>
<param humanName="Tailsitter input type" name="Q_TAILSIT_INPUT" documentation="This controls whether stick input when hovering as a tailsitter follows the conventions for fixed wing hovering or multicopter hovering. When multicopter input is selected the roll stick will roll the aircraft in earth frame and yaw stick will yaw in earth frame. When using fixed wing input the roll and yaw sticks will control the aircraft in body frame.">
<values>
<value code="0">MultiCopterInput</value>
<value code="1">FixedWingInput</value>
</values>
</param>
<param humanName="Tailsitter input mask" name="Q_TAILSIT_MASK" documentation="This controls what channels have full manual control when hovering as a tailsitter and the Q_TAILSIT_MASKCH channel in high. This can be used to teach yourself to prop-hang a 3D plane by learning one or more channels at a time.">
<field name="Bitmask">0:Aileron,1:Elevator,2:Throttle,3:Rudder</field>
</param>
<param humanName="Tailsitter input mask channel" name="Q_TAILSIT_MASKCH" documentation="This controls what input channel will activate the Q_TAILSIT_MASK mask. When this channel goes above 1700 then the pilot will have direct manual control of the output channels specified in Q_TAILSIT_MASK. Set to zero to disable.">
<values>
<value code="0">Disabled</value>
<value code="1">Channel1</value>
<value code="2">Channel2</value>
<value code="3">Channel3</value>
<value code="4">Channel4</value>
<value code="5">Channel5</value>
<value code="6">Channel6</value>
<value code="7">Channel7</value>
<value code="8">Channel8</value>
</values>
</param>
<param humanName="Tailsitter vector thrust gain in forward flight" name="Q_TAILSIT_VFGAIN" documentation="This controls the amount of vectored thrust control used in forward flight for a vectored tailsitter">
<field name="Range">0 1</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Tailsitter vector thrust gain in hover" name="Q_TAILSIT_VHGAIN" documentation="This controls the amount of vectored thrust control used in hover for a vectored tailsitter">
<field name="Range">0 1</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Tilt minimum angle for vectored yaw" name="Q_TILT_YAW_ANGLE" documentation="This is the angle of the tilt servos when in VTOL mode and at minimum output. This needs to be set for Q_TILT_TYPE=3 to enable vectored control for yaw of tricopter tilt quadplanes.">
<field name="Range">0 30</field>
</param>
<param humanName="Tailsitter vector thrust gain power" name="Q_TAILSIT_VHPOW" documentation="This controls the amount of extra pitch given to the vectored control when at high pitch errors">
<field name="Range">0 4</field>
<field name="Increment">0.1</field>
</param>
<param humanName="MAVLink type identifier" name="Q_MAV_TYPE" documentation="This controls the mavlink type given in HEARTBEAT messages. For some GCS types a particular setting will be needed for correct operation.">
<values>
<value code="0">AUTO</value>
<value code="1">FIXED_WING</value>
<value code="2">QUADROTOR</value>
<value code="3">COAXIAL</value>
<value code="4">HELICOPTER</value>
<value code="7">AIRSHIP</value>
<value code="8">FREE_BALLOON</value>
<value code="9">ROCKET</value>
<value code="10">GROUND_ROVER</value>
<value code="11">SURFACE_BOAT</value>
<value code="12">SUBMARINE</value>
<value code="16">FLAPPING_WING</value>
<value code="17">KITE</value>
<value code="19">VTOL_DUOROTOR</value>
<value code="20">VTOL_QUADROTOR</value>
<value code="21">VTOL_TILTROTOR</value>
</values>
</param>
<param humanName="quadplane options" name="Q_OPTIONS" documentation="This provides a set of additional control options for quadplanes. LevelTransition means that the wings should be held level to within LEVEL_ROLL_LIMIT degrees during transition to fixed wing flight. If AllowFWTakeoff is disabled then fixed wing takeoff on quadplanes will instead perform a VTOL takeoff. If AllowFWLand is disabled then fixed wing land on quadplanes will instead perform a VTOL land.">
<field name="Bitmask">0:LevelTransition,1:AllowFWTakeoff,2:AllowFWLand</field>
</param>
<param humanName="Transition deceleration" name="Q_TRANS_DECEL" documentation="This is deceleration rate that will be used in calculating the stopping distance when transitioning from fixed wing flight to multicopter flight." user="Standard">
<field name="Range">0.2 5</field>
<field name="Increment">0.1</field>
<field name="Units">m/s/s</field>
<field name="UnitText">meters per square second</field>
</param>
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</parameters>
<parameters name="Q_A_">
<param humanName="Roll axis rate controller P gain" name="Q_A_RAT_RLL_P" documentation="Roll axis rate controller P gain. Converts the difference between desired roll rate and actual roll rate into a motor speed output" user="Standard">
<field name="Range">0.08 0.30</field>
<field name="Increment">0.005</field>
</param>
<param humanName="Roll axis rate controller I gain" name="Q_A_RAT_RLL_I" documentation="Roll axis rate controller I gain. Corrects long-term difference in desired roll rate vs actual roll rate" user="Standard">
<field name="Range">0.01 0.5</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Roll axis rate controller I gain maximum" name="Q_A_RAT_RLL_IMAX" documentation="Roll axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output" user="Standard">
<field name="Range">0 1</field>
<field name="Increment">0.01</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Roll axis rate controller D gain" name="Q_A_RAT_RLL_D" documentation="Roll axis rate controller D gain. Compensates for short-term change in desired roll rate vs actual roll rate" user="Standard">
<field name="Range">0.0 0.02</field>
<field name="Increment">0.001</field>
</param>
<param humanName="Roll axis rate controller feed forward" name="Q_A_RAT_RLL_FF" documentation="Roll axis rate controller feed forward" user="Standard">
<field name="Range">0 0.5</field>
<field name="Increment">0.001</field>
</param>
<param humanName="Roll axis rate controller input frequency in Hz" name="Q_A_RAT_RLL_FILT" documentation="Roll axis rate controller input frequency in Hz" user="Standard">
<field name="Range">1 100</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Pitch axis rate controller P gain" name="Q_A_RAT_PIT_P" documentation="Pitch axis rate controller P gain. Converts the difference between desired pitch rate and actual pitch rate into a motor speed output" user="Standard">
<field name="Range">0.08 0.30</field>
<field name="Increment">0.005</field>
</param>
<param humanName="Pitch axis rate controller I gain" name="Q_A_RAT_PIT_I" documentation="Pitch axis rate controller I gain. Corrects long-term difference in desired pitch rate vs actual pitch rate" user="Standard">
<field name="Range">0.01 0.5</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Pitch axis rate controller I gain maximum" name="Q_A_RAT_PIT_IMAX" documentation="Pitch axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output" user="Standard">
<field name="Range">0 1</field>
<field name="Increment">0.01</field>
<field name="Units">%</field>
<field name="UnitText">percent</field>
</param>
<param humanName="Pitch axis rate controller D gain" name="Q_A_RAT_PIT_D" documentation="Pitch axis rate controller D gain. Compensates for short-term change in desired pitch rate vs actual pitch rate" user="Standard">
<field name="Range">0.0 0.02</field>
<field name="Increment">0.001</field>
</param>
<param humanName="Pitch axis rate controller feed forward" name="Q_A_RAT_PIT_FF" documentation="Pitch axis rate controller feed forward" user="Standard">
<field name="Range">0 0.5</field>
<field name="Increment">0.001</field>
</param>
<param humanName="Pitch axis rate controller input frequency in Hz" name="Q_A_RAT_PIT_FILT" documentation="Pitch axis rate controller input frequency in Hz" user="Standard">
<field name="Range">1 100</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Yaw axis rate controller P gain" name="Q_A_RAT_YAW_P" documentation="Yaw axis rate controller P gain. Converts the difference between desired yaw rate and actual yaw rate into a motor speed output" user="Standard">
<field name="Range">0.10 0.50</field>
<field name="Increment">0.005</field>
</param>
<param humanName="Yaw axis rate controller I gain" name="Q_A_RAT_YAW_I" documentation="Yaw axis rate controller I gain. Corrects long-term difference in desired yaw rate vs actual yaw rate" user="Standard">
<field name="Range">0.010 0.05</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Yaw axis rate controller I gain maximum" name="Q_A_RAT_YAW_IMAX" documentation="Yaw axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output" user="Standard">
<field name="Range">0 1</field>
<field name="Increment">0.01</field>
<field name="Units">%</field>
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4280
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4299
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4340
<field name="UnitText">percent</field>
</param>
<param humanName="Yaw axis rate controller D gain" name="Q_A_RAT_YAW_D" documentation="Yaw axis rate controller D gain. Compensates for short-term change in desired yaw rate vs actual yaw rate" user="Standard">
<field name="Range">0.000 0.02</field>
<field name="Increment">0.001</field>
</param>
<param humanName="Yaw axis rate controller feed forward" name="Q_A_RAT_YAW_FF" documentation="Yaw axis rate controller feed forward" user="Standard">
<field name="Range">0 0.5</field>
<field name="Increment">0.001</field>
</param>
<param humanName="Yaw axis rate controller input frequency in Hz" name="Q_A_RAT_YAW_FILT" documentation="Yaw axis rate controller input frequency in Hz" user="Standard">
<field name="Range">1 100</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Throttle Mix Minimum" name="Q_A_THR_MIX_MIN" documentation="Throttle vs attitude control prioritisation used when landing (higher values mean we prioritise attitude control over throttle)" user="Advanced">
<field name="Range">0.1 0.25</field>
</param>
<param humanName="Throttle Mix Maximum" name="Q_A_THR_MIX_MAX" documentation="Throttle vs attitude control prioritisation used during active flight (higher values mean we prioritise attitude control over throttle)" user="Advanced">
<field name="Range">0.5 0.9</field>
</param>
<param humanName="Throttle Mix Manual" name="Q_A_THR_MIX_MAN" documentation="Throttle vs attitude control prioritisation used during manual flight (higher values mean we prioritise attitude control over throttle)" user="Advanced">
<field name="Range">0.5 0.9</field>
</param>
</parameters>
<parameters name="Q_M_">
<param humanName="Matrix Yaw Min" name="Q_M_YAW_HEADROOM" documentation="Yaw control is given at least this pwm in microseconds range" user="Advanced">
<field name="Range">0 500</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Thrust Curve Expo" name="Q_M_THST_EXPO" documentation="Motor thrust curve exponent (from 0 for linear to 1.0 for second order curve)" user="Advanced">
<field name="Range">0.25 0.8</field>
</param>
<param humanName="Motor Spin maximum" name="Q_M_SPIN_MAX" documentation="Point at which the thrust saturates expressed as a number from 0 to 1 in the entire output range" user="Advanced">
<field name="Values">0.9:Low, 0.95:Default, 1.0:High</field>
</param>
<param humanName="Battery voltage compensation maximum voltage" name="Q_M_BAT_VOLT_MAX" documentation="Battery voltage compensation maximum voltage (voltage above this will have no additional scaling effect on thrust). Recommend 4.4 * cell count, 0 = Disabled" user="Advanced">
<field name="Range">6 35</field>
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
<param humanName="Battery voltage compensation minimum voltage" name="Q_M_BAT_VOLT_MIN" documentation="Battery voltage compensation minimum voltage (voltage below this will have no additional scaling effect on thrust). Recommend 3.5 * cell count, 0 = Disabled" user="Advanced">
<field name="Range">6 35</field>
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
<param humanName="Motor Current Max" name="Q_M_BAT_CURR_MAX" documentation="Maximum current over which maximum throttle is limited (0 = Disabled)" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">A</field>
<field name="UnitText">ampere</field>
</param>
<param humanName="Output PWM type" name="Q_M_PWM_TYPE" documentation="This selects the output PWM type, allowing for normal PWM continuous output, OneShot or brushed motor output" user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">OneShot</value>
<value code="2">OneShot125</value>
<value code="3">Brushed</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="PWM output miniumum" name="Q_M_PWM_MIN" documentation="This sets the min PWM output value in microseconds that will ever be output to the motors, 0 = use input RC3_MIN" user="Advanced">
<field name="Range">0 2000</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="PWM output maximum" name="Q_M_PWM_MAX" documentation="This sets the max PWM value in microseconds that will ever be output to the motors, 0 = use input RC3_MAX" user="Advanced">
<field name="Range">0 2000</field>
<field name="Units">PWM</field>
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4380
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<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Motor Spin minimum" name="Q_M_SPIN_MIN" documentation="Point at which the thrust starts expressed as a number from 0 to 1 in the entire output range. Should be higher than MOT_SPIN_ARM." user="Advanced">
<field name="Values">0.0:Low, 0.15:Default, 0.3:High</field>
</param>
<param humanName="Motor Spin armed" name="Q_M_SPIN_ARM" documentation="Point at which the motors start to spin expressed as a number from 0 to 1 in the entire output range. Should be lower than MOT_SPIN_MIN." user="Advanced">
<field name="Values">0.0:Low, 0.1:Default, 0.2:High</field>
</param>
<param humanName="Motor Current Max Time Constant" name="Q_M_BAT_CURR_TC" documentation="Time constant used to limit the maximum current" user="Advanced">
<field name="Range">0 10</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Thrust Hover Value" name="Q_M_THST_HOVER" documentation="Motor thrust needed to hover expressed as a number from 0 to 1" user="Advanced">
<field name="Range">0.2 0.8</field>
</param>
<param humanName="Hover Value Learning" name="Q_M_HOVER_LEARN" documentation="Enable/Disable automatic learning of hover throttle" user="Advanced">
<values>
<value code="0">Disabled</value>
<value code=" 1">Learn</value>
<value code=" 2">LearnAndSave</value>
</values>
</param>
<param humanName="Motor PWM output disabled when disarmed" name="Q_M_SAFE_DISARM" documentation="Disables motor PWM output when disarmed" user="Advanced">
<values>
<value code="0">PWM enabled while disarmed</value>
<value code=" 1">PWM disabled while disarmed</value>
</values>
</param>
<param humanName="Yaw Servo Max Lean Angle" name="Q_M_YAW_SV_ANGLE" documentation="Yaw servo's maximum lean angle" user="Standard">
<field name="Range">5 80</field>
<field name="Increment">1</field>
<field name="Units">deg</field>
<field name="UnitText">degrees</field>
</param>
<param humanName="Spool up time" name="Q_M_SPOOL_TIME" documentation="Time in seconds to spool up the motors from zero to min throttle. " user="Advanced">
<field name="Range">0 2</field>
<field name="Increment">0.1</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Motor boost scale" name="Q_M_BOOST_SCALE" documentation="This is a scaling factor for vehicles with a vertical booster motor used for extra lift. It is used with electric multicopters that have an internal combusion booster motor for longer endurance. The output to the BoostThrottle servo function is set to the current motor thottle times this scaling factor. A higher scaling factor will put more of the load on the booster motor. A value of 1 will set the BoostThrottle equal to the main throttle." user="Advanced">
<field name="Range">0 5</field>
<field name="Increment">0.1</field>
</param>
</parameters>
<parameters name="Q_P_">
<param humanName="XY Acceleration filter cutoff frequency" name="Q_P__ACC_XY_FILT" documentation="Lower values will slow the response of the navigation controller and reduce twitchiness" user="Advanced">
<field name="Range">0.5 5</field>
<field name="Increment">0.1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
</parameters>
<parameters name="Q_WP_">
<param humanName="Waypoint Horizontal Speed Target" name="Q_WP_SPEED" documentation="Defines the speed in cm/s which the aircraft will attempt to maintain horizontally during a WP mission" user="Standard">
<field name="Range">20 2000</field>
<field name="Increment">50</field>
<field name="Units">cm/s</field>
<field name="UnitText">centimeters per second</field>
</param>
<param humanName="Waypoint Radius" name="Q_WP_RADIUS" documentation="Defines the distance from a waypoint, that when crossed indicates the wp has been hit." user="Standard">
<field name="Range">10 1000</field>
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Waypoint Climb Speed Target" name="Q_WP_SPEED_UP" documentation="Defines the speed in cm/s which the aircraft will attempt to maintain while climbing during a WP mission" user="Standard">
<field name="Range">10 1000</field>
<field name="Increment">50</field>
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4480
<field name="Units">cm/s</field>
<field name="UnitText">centimeters per second</field>
</param>
<param humanName="Waypoint Descent Speed Target" name="Q_WP_SPEED_DN" documentation="Defines the speed in cm/s which the aircraft will attempt to maintain while descending during a WP mission" user="Standard">
<field name="Range">10 500</field>
<field name="Increment">10</field>
<field name="Units">cm/s</field>
<field name="UnitText">centimeters per second</field>
</param>
<param humanName="Loiter Horizontal Maximum Speed" name="Q_WP_LOIT_SPEED" documentation="Defines the maximum speed in cm/s which the aircraft will travel horizontally while in loiter mode" user="Standard">
<field name="Range">20 2000</field>
<field name="Increment">50</field>
<field name="Units">cm/s</field>
<field name="UnitText">centimeters per second</field>
</param>
<param humanName="Waypoint Acceleration " name="Q_WP_ACCEL" documentation="Defines the horizontal acceleration in cm/s/s used during missions" user="Standard">
<field name="Range">50 500</field>
<field name="Increment">10</field>
<field name="Units">cm/s/s</field>
<field name="UnitText">centimeters per square second</field>
</param>
<param humanName="Waypoint Vertical Acceleration" name="Q_WP_ACCEL_Z" documentation="Defines the vertical acceleration in cm/s/s used during missions" user="Standard">
<field name="Range">50 500</field>
<field name="Increment">10</field>
<field name="Units">cm/s/s</field>
<field name="UnitText">centimeters per square second</field>
</param>
<param humanName="Loiter maximum jerk" name="Q_WP_LOIT_JERK" documentation="Loiter maximum jerk in cm/s/s/s" user="Advanced">
<field name="Range">500 5000</field>
<field name="Increment">1</field>
<field name="Units">cm/s/s/s</field>
<field name="UnitText">centimeters per cubic second</field>
</param>
<param humanName="Loiter maximum acceleration" name="Q_WP_LOIT_MAXA" documentation="Loiter maximum acceleration in cm/s/s. Higher values cause the copter to accelerate and stop more quickly." user="Advanced">
<field name="Range">100 981</field>
<field name="Increment">1</field>
<field name="Units">cm/s/s</field>
<field name="UnitText">centimeters per square second</field>
</param>
<param humanName="Loiter minimum acceleration" name="Q_WP_LOIT_MINA" documentation="Loiter minimum acceleration in cm/s/s. Higher values stop the copter more quickly when the stick is centered, but cause a larger jerk when the copter stops." user="Advanced">
<field name="Range">25 250</field>
<field name="Increment">1</field>
<field name="Units">cm/s/s</field>
<field name="UnitText">centimeters per square second</field>
</param>
<param humanName="Use rangefinder for terrain following" name="Q_WP_RFND_USE" documentation="This controls the use of a rangefinder for terrain following" user="Advanced">
<values>
<value code="0">Disable</value>
<value code="1">Enable</value>
</values>
</param>
</parameters>
<parameters name="RALLY_">
<param humanName="Rally Total" name="RALLY_TOTAL" documentation="Number of rally points currently loaded" user="Advanced">
</param>
<param humanName="Rally Limit" name="RALLY_LIMIT_KM" documentation="Maximum distance to rally point. If the closest rally point is more than this number of kilometers from the current position and the home location is closer than any of the rally points from the current position then do RTL to home rather than to the closest rally point. This prevents a leftover rally point from a different airfield being used accidentally. If this is set to 0 then the closest rally point is always used." user="Advanced">
<field name="Increment">0.1</field>
<field name="Units">km</field>
<field name="UnitText">kilometers</field>
</param>
<param humanName="Rally Include Home" name="RALLY_INCL_HOME" documentation="Controls if Home is included as a Rally point (i.e. as a safe landing place) for RTL" user="Standard">
<values>
<value code="0">DoNotIncludeHome</value>
<value code="1">IncludeHome</value>
</values>
</param>
</parameters>
<parameters name="RC10_">
<param humanName="RC min PWM" name="RC10_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
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4487
4488
4489
4490
4491
4492
4493
4494
4495
4496
4497
4498
4499
4500
4501
4502
4503
4504
4505
4506
4507
4508
4509
4510
4511
4512
4513
4514
4515
4516
4517
4518
4519
4520
4521
4522
4523
4524
4525
4526
4527
4528
4529
4530
4531
4532
4533
4534
4535
4536
4537
4538
4539
4540
4541
4542
4543
4544
4545
4546
4547
4548
4549
4550
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC10_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC10_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC10_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC10_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC11_">
<param humanName="RC min PWM" name="RC11_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC11_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC11_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC11_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC11_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC12_">
<param humanName="RC min PWM" name="RC12_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC12_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
4551
4552
4553
4554
4555
4556
4557
4558
4559
4560
4561
4562
4563
4564
4565
4566
4567
4568
4569
4570
4571
4572
4573
4574
4575
4576
4577
4578
4579
4580
4581
4582
4583
4584
4585
4586
4587
4588
4589
4590
4591
4592
4593
4594
4595
4596
4597
4598
4599
4600
4601
4602
4603
4604
4605
4606
4607
4608
4609
4610
4611
4612
4613
4614
4615
4616
4617
4618
4619
4620
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC12_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC12_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC12_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC13_">
<param humanName="RC min PWM" name="RC13_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC13_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC13_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC13_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC13_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC14_">
<param humanName="RC min PWM" name="RC14_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC14_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC14_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
4621
4622
4623
4624
4625
4626
4627
4628
4629
4630
4631
4632
4633
4634
4635
4636
4637
4638
4639
4640
4641
4642
4643
4644
4645
4646
4647
4648
4649
4650
4651
4652
4653
4654
4655
4656
4657
4658
4659
4660
4661
4662
4663
4664
4665
4666
4667
4668
4669
4670
4671
4672
4673
4674
4675
4676
4677
4678
4679
4680
4681
4682
4683
4684
4685
4686
4687
4688
4689
4690
<param humanName="RC reversed" name="RC14_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC14_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC15_">
<param humanName="RC min PWM" name="RC15_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC15_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC15_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC15_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC15_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC16_">
<param humanName="RC min PWM" name="RC16_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC16_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC16_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC16_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC16_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
4691
4692
4693
4694
4695
4696
4697
4698
4699
4700
4701
4702
4703
4704
4705
4706
4707
4708
4709
4710
4711
4712
4713
4714
4715
4716
4717
4718
4719
4720
4721
4722
4723
4724
4725
4726
4727
4728
4729
4730
4731
4732
4733
4734
4735
4736
4737
4738
4739
4740
4741
4742
4743
4744
4745
4746
4747
4748
4749
4750
4751
4752
4753
4754
4755
4756
4757
4758
4759
4760
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC1_">
<param humanName="RC min PWM" name="RC1_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC1_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC1_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC1_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC1_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC2_">
<param humanName="RC min PWM" name="RC2_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC2_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC2_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC2_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC2_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC3_">
<param humanName="RC min PWM" name="RC3_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
4761
4762
4763
4764
4765
4766
4767
4768
4769
4770
4771
4772
4773
4774
4775
4776
4777
4778
4779
4780
4781
4782
4783
4784
4785
4786
4787
4788
4789
4790
4791
4792
4793
4794
4795
4796
4797
4798
4799
4800
4801
4802
4803
4804
4805
4806
4807
4808
4809
4810
4811
4812
4813
4814
4815
4816
4817
4818
4819
4820
4821
4822
4823
4824
4825
4826
4827
4828
4829
4830
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC3_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC3_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC3_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC3_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC4_">
<param humanName="RC min PWM" name="RC4_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC4_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC4_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC4_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC4_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC5_">
<param humanName="RC min PWM" name="RC5_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC5_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
4831
4832
4833
4834
4835
4836
4837
4838
4839
4840
4841
4842
4843
4844
4845
4846
4847
4848
4849
4850
4851
4852
4853
4854
4855
4856
4857
4858
4859
4860
4861
4862
4863
4864
4865
4866
4867
4868
4869
4870
4871
4872
4873
4874
4875
4876
4877
4878
4879
4880
4881
4882
4883
4884
4885
4886
4887
4888
4889
4890
4891
4892
4893
4894
4895
4896
4897
4898
4899
4900
</param>
<param humanName="RC max PWM" name="RC5_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC5_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC5_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC6_">
<param humanName="RC min PWM" name="RC6_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC6_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC6_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC6_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC6_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC7_">
<param humanName="RC min PWM" name="RC7_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC7_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC7_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC7_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
4901
4902
4903
4904
4905
4906
4907
4908
4909
4910
4911
4912
4913
4914
4915
4916
4917
4918
4919
4920
4921
4922
4923
4924
4925
4926
4927
4928
4929
4930
4931
4932
4933
4934
4935
4936
4937
4938
4939
4940
4941
4942
4943
4944
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4955
4956
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4958
4959
4960
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4964
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4970
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC7_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC8_">
<param humanName="RC min PWM" name="RC8_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC8_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC8_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC8_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC8_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RC9_">
<param humanName="RC min PWM" name="RC9_MIN" documentation="RC minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC trim PWM" name="RC9_TRIM" documentation="RC trim (neutral) PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC max PWM" name="RC9_MAX" documentation="RC maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Advanced">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="RC reversed" name="RC9_REVERSED" documentation="Reverse channel input. Set to 0 for normal operation. Set to 1 to reverse this input channel." user="Advanced">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="RC dead-zone" name="RC9_DZ" documentation="PWM dead zone in microseconds around trim or bottom" user="Advanced">
<field name="Range">0 200</field>
<field name="Units">PWM</field>
4971
4972
4973
4974
4975
4976
4977
4978
4979
4980
4981
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4984
4985
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5010
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5028
5029
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5033
5034
5035
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5040
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="RCMAP_">
<param humanName="Roll channel" name="RCMAP_ROLL" documentation="Roll channel number. This is useful when you have a RC transmitter that can't change the channel order easily. Roll is normally on channel 1, but you can move it to any channel with this parameter. Reboot is required for changes to take effect." user="Advanced">
<field name="Range">1 8</field>
<field name="Increment">1</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Pitch channel" name="RCMAP_PITCH" documentation="Pitch channel number. This is useful when you have a RC transmitter that can't change the channel order easily. Pitch is normally on channel 2, but you can move it to any channel with this parameter. Reboot is required for changes to take effect." user="Advanced">
<field name="Range">1 8</field>
<field name="Increment">1</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Throttle channel" name="RCMAP_THROTTLE" documentation="Throttle channel number. This is useful when you have a RC transmitter that can't change the channel order easily. Throttle is normally on channel 3, but you can move it to any channel with this parameter. Warning APM 2.X: Changing the throttle channel could produce unexpected fail-safe results if connection between receiver and on-board PPM Encoder is lost. Disabling on-board PPM Encoder is recommended. Reboot is required for changes to take effect." user="Advanced">
<field name="Range">1 8</field>
<field name="Increment">1</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Yaw channel" name="RCMAP_YAW" documentation="Yaw channel number. This is useful when you have a RC transmitter that can't change the channel order easily. Yaw (also known as rudder) is normally on channel 4, but you can move it to any channel with this parameter. Reboot is required for changes to take effect." user="Advanced">
<field name="Range">1 8</field>
<field name="Increment">1</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Forward channel" name="RCMAP_FORWARD" documentation="Forward channel number. This is useful when you have a RC transmitter that can't change the channel order easily. Forward is normally on channel 5, but you can move it to any channel with this parameter. Reboot is required for changes to take effect." user="Advanced">
<field name="Range">1 8</field>
<field name="Increment">1</field>
<field name="RebootRequired">True</field>
</param>
<param humanName="Lateral channel" name="RCMAP_LATERAL" documentation="Lateral channel number. This is useful when you have a RC transmitter that can't change the channel order easily. Lateral is normally on channel 6, but you can move it to any channel with this parameter. Reboot is required for changes to take effect." user="Advanced">
<field name="Range">1 8</field>
<field name="Increment">1</field>
<field name="RebootRequired">True</field>
</param>
</parameters>
<parameters name="RELAY_">
<param humanName="First Relay Pin" name="RELAY_PIN" documentation="Digital pin number for first relay control. This is the pin used for camera control." user="Standard">
<values>
<value code="-1">Disabled</value>
<value code="13">APM2 A9 pin</value>
<value code="47">APM1 relay</value>
<value code="50">Pixhawk AUXOUT1</value>
<value code="51">Pixhawk AUXOUT2</value>
<value code="52">Pixhawk AUXOUT3</value>
<value code="53">Pixhawk AUXOUT4</value>
<value code="54">Pixhawk AUXOUT5</value>
<value code="55">Pixhawk AUXOUT6</value>
<value code="111">PX4 FMU Relay1</value>
<value code="112">PX4 FMU Relay2</value>
<value code="113">PX4IO Relay1</value>
<value code="114">PX4IO Relay2</value>
<value code="115">PX4IO ACC1</value>
<value code="116">PX4IO ACC2</value>
</values>
</param>
<param humanName="Second Relay Pin" name="RELAY_PIN2" documentation="Digital pin number for 2nd relay control." user="Standard">
<values>
<value code="-1">Disabled</value>
<value code="13">APM2 A9 pin</value>
<value code="47">APM1 relay</value>
<value code="50">Pixhawk AUXOUT1</value>
<value code="51">Pixhawk AUXOUT2</value>
<value code="52">Pixhawk AUXOUT3</value>
<value code="53">Pixhawk AUXOUT4</value>
<value code="54">Pixhawk AUXOUT5</value>
<value code="55">Pixhawk AUXOUT6</value>
<value code="111">PX4 FMU Relay1</value>
<value code="112">PX4 FMU Relay2</value>
<value code="113">PX4IO Relay1</value>
<value code="114">PX4IO Relay2</value>
5041
5042
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5044
5045
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5049
5050
5051
5052
5053
5054
5055
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5068
5069
5070
5071
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5077
5078
5079
5080
5081
5082
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5084
5085
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5088
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5090
5091
5092
5093
5094
5095
5096
5097
5098
5099
5100
5101
5102
5103
5104
5105
5106
5107
5108
5109
5110
<value code="115">PX4IO ACC1</value>
<value code="116">PX4IO ACC2</value>
</values>
</param>
<param humanName="Third Relay Pin" name="RELAY_PIN3" documentation="Digital pin number for 3rd relay control." user="Standard">
<values>
<value code="-1">Disabled</value>
<value code="13">APM2 A9 pin</value>
<value code="47">APM1 relay</value>
<value code="50">Pixhawk AUXOUT1</value>
<value code="51">Pixhawk AUXOUT2</value>
<value code="52">Pixhawk AUXOUT3</value>
<value code="53">Pixhawk AUXOUT4</value>
<value code="54">Pixhawk AUXOUT5</value>
<value code="55">Pixhawk AUXOUT6</value>
<value code="111">PX4 FMU Relay1</value>
<value code="112">PX4 FMU Relay2</value>
<value code="113">PX4IO Relay1</value>
<value code="114">PX4IO Relay2</value>
<value code="115">PX4IO ACC1</value>
<value code="116">PX4IO ACC2</value>
</values>
</param>
<param humanName="Fourth Relay Pin" name="RELAY_PIN4" documentation="Digital pin number for 4th relay control." user="Standard">
<values>
<value code="-1">Disabled</value>
<value code="13">APM2 A9 pin</value>
<value code="47">APM1 relay</value>
<value code="50">Pixhawk AUXOUT1</value>
<value code="51">Pixhawk AUXOUT2</value>
<value code="52">Pixhawk AUXOUT3</value>
<value code="53">Pixhawk AUXOUT4</value>
<value code="54">Pixhawk AUXOUT5</value>
<value code="55">Pixhawk AUXOUT6</value>
<value code="111">PX4 FMU Relay1</value>
<value code="112">PX4 FMU Relay2</value>
<value code="113">PX4IO Relay1</value>
<value code="114">PX4IO Relay2</value>
<value code="115">PX4IO ACC1</value>
<value code="116">PX4IO ACC2</value>
</values>
</param>
<param humanName="Default relay state" name="RELAY_DEFAULT" documentation="The state of the relay on boot. " user="Standard">
<values>
<value code="0">Off</value>
<value code="1">On</value>
<value code="2">NoChange</value>
</values>
</param>
</parameters>
<parameters name="RLL2SRV_">
<param humanName="Roll Time Constant" name="RLL2SRV_TCONST" documentation="This controls the time constant in seconds from demanded to achieved bank angle. A value of 0.5 is a good default and will work with nearly all models. Advanced users may want to reduce this time to obtain a faster response but there is no point setting a time less than the aircraft can achieve." user="Advanced">
<field name="Range">0.4 1.0</field>
<field name="Increment">0.1</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Proportional Gain" name="RLL2SRV_P" documentation="This is the gain from bank angle error to aileron." user="User">
<field name="Range">0.1 4.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Damping Gain" name="RLL2SRV_D" documentation="This is the gain from roll rate to aileron. This adjusts the damping of the roll control loop. It has the same effect as RLL2SRV_D in the old PID controller but without the spikes in servo demands. This gain helps to reduce rolling in turbulence. It should be increased in 0.01 increments as too high a value can lead to a high frequency roll oscillation that could overstress the airframe." user="User">
<field name="Range">0 0.1</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Integrator Gain" name="RLL2SRV_I" documentation="This is the gain from the integral of bank angle to aileron. It has the same effect as RLL2SRV_I in the old PID controller. Increasing this gain causes the controller to trim out steady offsets due to an out of trim aircraft." user="User">
<field name="Range">0 1.0</field>
<field name="Increment">0.05</field>
</param>
<param humanName="Maximum Roll Rate" name="RLL2SRV_RMAX" documentation="This sets the maximum roll rate that the controller will demand (degrees/sec). Setting it to zero disables the limit. If this value is set too low, then the roll can't keep up with the navigation demands and the plane will start weaving. If it is set too high (or disabled by setting to zero) then ailerons will get large inputs at the start of turns. A limit of 60 degrees/sec is a good default." user="Advanced">
5111
5112
5113
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5118
5119
5120
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5168
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5172
5173
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5175
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5180
<field name="Range">0 180</field>
<field name="Increment">1</field>
<field name="Units">deg/s</field>
<field name="UnitText">degrees per second</field>
</param>
<param humanName="Integrator limit" name="RLL2SRV_IMAX" documentation="This limits the number of degrees of aileron in centi-degrees over which the integrator will operate. At the default setting of 3000 centi-degrees, the integrator will be limited to +- 30 degrees of servo travel. The maximum servo deflection is +- 45 centi-degrees, so the default value represents a 2/3rd of the total control throw which is adequate unless the aircraft is severely out of trim." user="Advanced">
<field name="Range">0 4500</field>
<field name="Increment">1</field>
</param>
<param humanName="Feed forward Gain" name="RLL2SRV_FF" documentation="This is the gain from demanded rate to aileron output. " user="User">
<field name="Range">0.1 4.0</field>
<field name="Increment">0.1</field>
</param>
</parameters>
<parameters name="RNGFND">
<param humanName="Rangefinder type" name="RNGFND_TYPE" documentation="What type of rangefinder device that is connected" user="Standard">
<values>
<value code="0">None</value>
<value code="1">Analog</value>
<value code="2">MaxbotixI2C</value>
<value code="3">LidarLiteV2-I2C</value>
<value code="5">PX4-PWM</value>
<value code="6">BBB-PRU</value>
<value code="7">LightWareI2C</value>
<value code="8">LightWareSerial</value>
<value code="9">Bebop</value>
<value code="10">MAVLink</value>
<value code="11">uLanding</value>
<value code="12">LeddarOne</value>
<value code="13">MaxbotixSerial</value>
<value code="14">TrOneI2C</value>
<value code="15">LidarLiteV3-I2C</value>
<value code="16">VL53L0X</value>
</values>
</param>
<param humanName="Rangefinder pin" name="RNGFND_PIN" documentation="Analog pin that rangefinder is connected to. Set this to 0..9 for the APM2 analog pins. Set to 64 on an APM1 for the dedicated 'airspeed' port on the end of the board. Set to 11 on PX4 for the analog 'airspeed' port. Set to 15 on the Pixhawk for the analog 'airspeed' port." user="Standard">
<values>
<value code="-1">Not Used</value>
<value code=" 0">APM2-A0</value>
<value code=" 1">APM2-A1</value>
<value code=" 2">APM2-A2</value>
<value code=" 3">APM2-A3</value>
<value code=" 4">APM2-A4</value>
<value code=" 5">APM2-A5</value>
<value code=" 6">APM2-A6</value>
<value code=" 7">APM2-A7</value>
<value code=" 8">APM2-A8</value>
<value code=" 9">APM2-A9</value>
<value code=" 11">PX4-airspeed port</value>
<value code=" 15">Pixhawk-airspeed port</value>
<value code=" 64">APM1-airspeed port</value>
</values>
</param>
<param humanName="Rangefinder scaling" name="RNGFND_SCALING" documentation="Scaling factor between rangefinder reading and distance. For the linear and inverted functions this is in meters per volt. For the hyperbolic function the units are meterVolts." user="Standard">
<field name="Increment">0.001</field>
<field name="Units">m/V</field>
<field name="UnitText">meters per volt</field>
</param>
<param humanName="rangefinder offset" name="RNGFND_OFFSET" documentation="Offset in volts for zero distance for analog rangefinders. Offset added to distance in centimeters for PWM and I2C Lidars" user="Standard">
<field name="Increment">0.001</field>
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
<param humanName="Rangefinder function" name="RNGFND_FUNCTION" documentation="Control over what function is used to calculate distance. For a linear function, the distance is (voltage-offset)*scaling. For a inverted function the distance is (offset-voltage)*scaling. For a hyperbolic function the distance is scaling/(voltage-offset). The functions return the distance in meters." user="Standard">
<values>
<value code="0">Linear</value>
<value code="1">Inverted</value>
<value code="2">Hyperbolic</value>
</values>
</param>
5181
5182
5183
5184
5185
5186
5187
5188
5189
5190
5191
5192
5193
5194
5195
5196
5197
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5199
5200
5201
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5203
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5205
5206
5207
5208
5209
5210
5211
5212
5213
5214
5215
5216
5217
5218
5219
5220
5221
5222
5223
5224
5225
5226
5227
5228
5229
5230
5231
5232
5233
5234
5235
5236
5237
5238
5239
5240
5241
5242
5243
5244
5245
5246
5247
5248
5249
5250
<param humanName="Rangefinder minimum distance" name="RNGFND_MIN_CM" documentation="Minimum distance in centimeters that rangefinder can reliably read" user="Standard">
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Rangefinder maximum distance" name="RNGFND_MAX_CM" documentation="Maximum distance in centimeters that rangefinder can reliably read" user="Standard">
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Rangefinder stop pin" name="RNGFND_STOP_PIN" documentation="Digital pin that enables/disables rangefinder measurement for an analog rangefinder. A value of -1 means no pin. If this is set, then the pin is set to 1 to enable the rangefinder and set to 0 to disable it. This can be used to ensure that multiple sonar rangefinders don't interfere with each other." user="Standard">
<values>
<value code="-1">Not Used</value>
<value code="50">Pixhawk AUXOUT1</value>
<value code="51">Pixhawk AUXOUT2</value>
<value code="52">Pixhawk AUXOUT3</value>
<value code="53">Pixhawk AUXOUT4</value>
<value code="54">Pixhawk AUXOUT5</value>
<value code="55">Pixhawk AUXOUT6</value>
<value code="111">PX4 FMU Relay1</value>
<value code="112">PX4 FMU Relay2</value>
<value code="113">PX4IO Relay1</value>
<value code="114">PX4IO Relay2</value>
<value code="115">PX4IO ACC1</value>
<value code="116">PX4IO ACC2</value>
</values>
</param>
<param humanName="Rangefinder settle time" name="RNGFND_SETTLE" documentation="The time in milliseconds that the rangefinder reading takes to settle. This is only used when a STOP_PIN is specified. It determines how long we have to wait for the rangefinder to give a reading after we set the STOP_PIN high. For a sonar rangefinder with a range of around 7m this would need to be around 50 milliseconds to allow for the sonar pulse to travel to the target and back again." user="Standard">
<field name="Increment">1</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
</param>
<param humanName="Ratiometric" name="RNGFND_RMETRIC" documentation="This parameter sets whether an analog rangefinder is ratiometric. Most analog rangefinders are ratiometric, meaning that their output voltage is influenced by the supply voltage. Some analog rangefinders (such as the SF/02) have their own internal voltage regulators so they are not ratiometric." user="Standard">
<values>
<value code="0">No</value>
<value code="1">Yes</value>
</values>
</param>
<param humanName="Powersave range" name="RNGFND_PWRRNG" documentation="This parameter sets the estimated terrain distance in meters above which the sensor will be put into a power saving mode (if available). A value of zero means power saving is not enabled" user="Standard">
<field name="Range">0 32767</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Distance (in cm) from the range finder to the ground" name="RNGFND_GNDCLEAR" documentation="This parameter sets the expected range measurement(in cm) that the range finder should return when the vehicle is on the ground." user="Standard">
<field name="Range">5 127</field>
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Bus address of sensor" name="RNGFND_ADDR" documentation="This sets the bus address of the sensor, where applicable. Used for the LightWare I2C sensor to allow for multiple sensors on different addresses. A value of 0 disables the sensor." user="Standard">
<field name="Range">0 127</field>
<field name="Increment">1</field>
</param>
<param humanName=" X position offset" name="RNGFND_POS_X" documentation="X position of the first rangefinder in body frame. Positive X is forward of the origin. Use the zero range datum point if supplied." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Y position offset" name="RNGFND_POS_Y" documentation="Y position of the first rangefinder in body frame. Positive Y is to the right of the origin. Use the zero range datum point if supplied." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Z position offset" name="RNGFND_POS_Z" documentation="Z position of the first rangefinder in body frame. Positive Z is down from the origin. Use the zero range datum point if supplied." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Rangefinder orientation" name="RNGFND_ORIENT" documentation="Orientation of rangefinder" user="Advanced">
<values>
<value code="0">Forward</value>
<value code=" 1">Forward-Right</value>
<value code=" 2">Right</value>
5251
5252
5253
5254
5255
5256
5257
5258
5259
5260
5261
5262
5263
5264
5265
5266
5267
5268
5269
5270
5271
5272
5273
5274
5275
5276
5277
5278
5279
5280
5281
5282
5283
5284
5285
5286
5287
5288
5289
5290
5291
5292
5293
5294
5295
5296
5297
5298
5299
5300
5301
5302
5303
5304
5305
5306
5307
5308
5309
5310
5311
5312
5313
5314
5315
5316
5317
5318
5319
5320
<value code=" 3">Back-Right</value>
<value code=" 4">Back</value>
<value code=" 5">Back-Left</value>
<value code=" 6">Left</value>
<value code=" 7">Forward-Left</value>
<value code=" 24">Up</value>
<value code=" 25">Down</value>
</values>
</param>
<param humanName="Second Rangefinder type" name="RNGFND2_TYPE" documentation="What type of rangefinder device that is connected" user="Advanced">
<values>
<value code="0">None</value>
<value code="1">Analog</value>
<value code="2">MaxbotixI2C</value>
<value code="3">LidarLiteV2-I2C</value>
<value code="5">PX4-PWM</value>
<value code="6">BBB-PRU</value>
<value code="7">LightWareI2C</value>
<value code="8">LightWareSerial</value>
<value code="9">Bebop</value>
<value code="10">MAVLink</value>
<value code="11">uLanding</value>
<value code="12">LeddarOne</value>
<value code="13">MaxbotixSerial</value>
<value code="14">TrOneI2C</value>
<value code="15">LidarLiteV3-I2C</value>
<value code="16">VL53L0X</value>
</values>
</param>
<param humanName="Rangefinder pin" name="RNGFND2_PIN" documentation="Analog pin that rangefinder is connected to. Set this to 0..9 for the APM2 analog pins. Set to 64 on an APM1 for the dedicated 'airspeed' port on the end of the board. Set to 11 on PX4 for the analog 'airspeed' port. Set to 15 on the Pixhawk for the analog 'airspeed' port." user="Advanced">
<values>
<value code="-1">Not Used</value>
<value code=" 0">APM2-A0</value>
<value code=" 1">APM2-A1</value>
<value code=" 2">APM2-A2</value>
<value code=" 3">APM2-A3</value>
<value code=" 4">APM2-A4</value>
<value code=" 5">APM2-A5</value>
<value code=" 6">APM2-A6</value>
<value code=" 7">APM2-A7</value>
<value code=" 8">APM2-A8</value>
<value code=" 9">APM2-A9</value>
<value code=" 11">PX4-airspeed port</value>
<value code=" 15">Pixhawk-airspeed port</value>
<value code=" 64">APM1-airspeed port</value>
</values>
</param>
<param humanName="Rangefinder scaling" name="RNGFND2_SCALING" documentation="Scaling factor between rangefinder reading and distance. For the linear and inverted functions this is in meters per volt. For the hyperbolic function the units are meterVolts." user="Advanced">
<field name="Increment">0.001</field>
<field name="Units">m/V</field>
<field name="UnitText">meters per volt</field>
</param>
<param humanName="rangefinder offset" name="RNGFND2_OFFSET" documentation="Offset in volts for zero distance" user="Advanced">
<field name="Increment">0.001</field>
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
<param humanName="Rangefinder function" name="RNGFND2_FUNCTION" documentation="Control over what function is used to calculate distance. For a linear function, the distance is (voltage-offset)*scaling. For a inverted function the distance is (offset-voltage)*scaling. For a hyperbolic function the distance is scaling/(voltage-offset). The functions return the distance in meters." user="Advanced">
<values>
<value code="0">Linear</value>
<value code="1">Inverted</value>
<value code="2">Hyperbolic</value>
</values>
</param>
<param humanName="Rangefinder minimum distance" name="RNGFND2_MIN_CM" documentation="Minimum distance in centimeters that rangefinder can reliably read" user="Advanced">
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Rangefinder maximum distance" name="RNGFND2_MAX_CM" documentation="Maximum distance in centimeters that rangefinder can reliably read" user="Advanced">
5321
5322
5323
5324
5325
5326
5327
5328
5329
5330
5331
5332
5333
5334
5335
5336
5337
5338
5339
5340
5341
5342
5343
5344
5345
5346
5347
5348
5349
5350
5351
5352
5353
5354
5355
5356
5357
5358
5359
5360
5361
5362
5363
5364
5365
5366
5367
5368
5369
5370
5371
5372
5373
5374
5375
5376
5377
5378
5379
5380
5381
5382
5383
5384
5385
5386
5387
5388
5389
5390
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Rangefinder stop pin" name="RNGFND2_STOP_PIN" documentation="Digital pin that enables/disables rangefinder measurement for an analog rangefinder. A value of -1 means no pin. If this is set, then the pin is set to 1 to enable the rangefinder and set to 0 to disable it. This can be used to ensure that multiple sonar rangefinders don't interfere with each other." user="Advanced">
<values>
<value code="-1">Not Used</value>
<value code="50">Pixhawk AUXOUT1</value>
<value code="51">Pixhawk AUXOUT2</value>
<value code="52">Pixhawk AUXOUT3</value>
<value code="53">Pixhawk AUXOUT4</value>
<value code="54">Pixhawk AUXOUT5</value>
<value code="55">Pixhawk AUXOUT6</value>
<value code="111">PX4 FMU Relay1</value>
<value code="112">PX4 FMU Relay2</value>
<value code="113">PX4IO Relay1</value>
<value code="114">PX4IO Relay2</value>
<value code="115">PX4IO ACC1</value>
<value code="116">PX4IO ACC2</value>
</values>
</param>
<param humanName="Sonar settle time" name="RNGFND2_SETTLE" documentation="The time in milliseconds that the rangefinder reading takes to settle. This is only used when a STOP_PIN is specified. It determines how long we have to wait for the rangefinder to give a reading after we set the STOP_PIN high. For a sonar rangefinder with a range of around 7m this would need to be around 50 milliseconds to allow for the sonar pulse to travel to the target and back again." user="Advanced">
<field name="Increment">1</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
</param>
<param humanName="Ratiometric" name="RNGFND2_RMETRIC" documentation="This parameter sets whether an analog rangefinder is ratiometric. Most analog rangefinders are ratiometric, meaning that their output voltage is influenced by the supply voltage. Some analog rangefinders (such as the SF/02) have their own internal voltage regulators so they are not ratiometric." user="Advanced">
<values>
<value code="0">No</value>
<value code="1">Yes</value>
</values>
</param>
<param humanName="Distance (in cm) from the second range finder to the ground" name="RNGFND2_GNDCLEAR" documentation="This parameter sets the expected range measurement(in cm) that the second range finder should return when the vehicle is on the ground." user="Advanced">
<field name="Range">0 127</field>
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Bus address of second rangefinder" name="RNGFND2_ADDR" documentation="This sets the bus address of the sensor, where applicable. Used for the LightWare I2C sensor to allow for multiple sensors on different addresses. A value of 0 disables the sensor." user="Advanced">
<field name="Range">0 127</field>
<field name="Increment">1</field>
</param>
<param humanName=" X position offset" name="RNGFND2_POS_X" documentation="X position of the second rangefinder in body frame. Positive X is forward of the origin. Use the zero range datum point if supplied." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Y position offset" name="RNGFND2_POS_Y" documentation="Y position of the second rangefinder in body frame. Positive Y is to the right of the origin. Use the zero range datum point if supplied." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Z position offset" name="RNGFND2_POS_Z" documentation="Z position of the second rangefinder in body frame. Positive Z is down from the origin. Use the zero range datum point if supplied." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Rangefinder 2 orientation" name="RNGFND2_ORIENT" documentation="Orientation of 2nd rangefinder" user="Advanced">
<values>
<value code="0">Forward</value>
<value code=" 1">Forward-Right</value>
<value code=" 2">Right</value>
<value code=" 3">Back-Right</value>
<value code=" 4">Back</value>
<value code=" 5">Back-Left</value>
<value code=" 6">Left</value>
<value code=" 7">Forward-Left</value>
<value code=" 24">Up</value>
<value code=" 25">Down</value>
</values>
</param>
<param humanName="Third Rangefinder type" name="RNGFND3_TYPE" documentation="What type of rangefinder device that is connected" user="Advanced">
<values>
5391
5392
5393
5394
5395
5396
5397
5398
5399
5400
5401
5402
5403
5404
5405
5406
5407
5408
5409
5410
5411
5412
5413
5414
5415
5416
5417
5418
5419
5420
5421
5422
5423
5424
5425
5426
5427
5428
5429
5430
5431
5432
5433
5434
5435
5436
5437
5438
5439
5440
5441
5442
5443
5444
5445
5446
5447
5448
5449
5450
5451
5452
5453
5454
5455
5456
5457
5458
5459
5460
<value code="0">None</value>
<value code="1">Analog</value>
<value code="2">MaxbotixI2C</value>
<value code="3">LidarLiteV2-I2C</value>
<value code="5">PX4-PWM</value>
<value code="6">BBB-PRU</value>
<value code="7">LightWareI2C</value>
<value code="8">LightWareSerial</value>
<value code="9">Bebop</value>
<value code="10">MAVLink</value>
<value code="11">uLanding</value>
<value code="12">LeddarOne</value>
<value code="13">MaxbotixSerial</value>
<value code="14">TrOneI2C</value>
<value code="15">LidarLiteV3-I2C</value>
<value code="16">VL53L0X</value>
</values>
</param>
<param humanName="Rangefinder pin" name="RNGFND3_PIN" documentation="Analog pin that rangefinder is connected to. Set this to 0..9 for the APM2 analog pins. Set to 64 on an APM1 for the dedicated 'airspeed' port on the end of the board. Set to 11 on PX4 for the analog 'airspeed' port. Set to 15 on the Pixhawk for the analog 'airspeed' port." user="Advanced">
<values>
<value code="-1">Not Used</value>
<value code=" 0">APM2-A0</value>
<value code=" 1">APM2-A1</value>
<value code=" 2">APM2-A2</value>
<value code=" 3">APM2-A3</value>
<value code=" 4">APM2-A4</value>
<value code=" 5">APM2-A5</value>
<value code=" 6">APM2-A6</value>
<value code=" 7">APM2-A7</value>
<value code=" 8">APM2-A8</value>
<value code=" 9">APM2-A9</value>
<value code=" 11">PX4-airspeed port</value>
<value code=" 15">Pixhawk-airspeed port</value>
<value code=" 64">APM1-airspeed port</value>
</values>
</param>
<param humanName="Rangefinder scaling" name="RNGFND3_SCALING" documentation="Scaling factor between rangefinder reading and distance. For the linear and inverted functions this is in meters per volt. For the hyperbolic function the units are meterVolts." user="Advanced">
<field name="Increment">0.001</field>
<field name="Units">m/V</field>
<field name="UnitText">meters per volt</field>
</param>
<param humanName="rangefinder offset" name="RNGFND3_OFFSET" documentation="Offset in volts for zero distance" user="Advanced">
<field name="Increment">0.001</field>
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
<param humanName="Rangefinder function" name="RNGFND3_FUNCTION" documentation="Control over what function is used to calculate distance. For a linear function, the distance is (voltage-offset)*scaling. For a inverted function the distance is (offset-voltage)*scaling. For a hyperbolic function the distance is scaling/(voltage-offset). The functions return the distance in meters." user="Advanced">
<values>
<value code="0">Linear</value>
<value code="1">Inverted</value>
<value code="2">Hyperbolic</value>
</values>
</param>
<param humanName="Rangefinder minimum distance" name="RNGFND3_MIN_CM" documentation="Minimum distance in centimeters that rangefinder can reliably read" user="Advanced">
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Rangefinder maximum distance" name="RNGFND3_MAX_CM" documentation="Maximum distance in centimeters that rangefinder can reliably read" user="Advanced">
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Rangefinder stop pin" name="RNGFND3_STOP_PIN" documentation="Digital pin that enables/disables rangefinder measurement for an analog rangefinder. A value of -1 means no pin. If this is set, then the pin is set to 1 to enable the rangefinder and set to 0 to disable it. This can be used to ensure that multiple sonar rangefinders don't interfere with each other." user="Advanced">
<values>
<value code="-1">Not Used</value>
<value code="50">Pixhawk AUXOUT1</value>
<value code="51">Pixhawk AUXOUT2</value>
<value code="52">Pixhawk AUXOUT3</value>
<value code="53">Pixhawk AUXOUT4</value>
5461
5462
5463
5464
5465
5466
5467
5468
5469
5470
5471
5472
5473
5474
5475
5476
5477
5478
5479
5480
5481
5482
5483
5484
5485
5486
5487
5488
5489
5490
5491
5492
5493
5494
5495
5496
5497
5498
5499
5500
5501
5502
5503
5504
5505
5506
5507
5508
5509
5510
5511
5512
5513
5514
5515
5516
5517
5518
5519
5520
5521
5522
5523
5524
5525
5526
5527
5528
5529
5530
<value code="54">Pixhawk AUXOUT5</value>
<value code="55">Pixhawk AUXOUT6</value>
<value code="111">PX4 FMU Relay1</value>
<value code="112">PX4 FMU Relay2</value>
<value code="113">PX4IO Relay1</value>
<value code="114">PX4IO Relay2</value>
<value code="115">PX4IO ACC1</value>
<value code="116">PX4IO ACC2</value>
</values>
</param>
<param humanName="Sonar settle time" name="RNGFND3_SETTLE" documentation="The time in milliseconds that the rangefinder reading takes to settle. This is only used when a STOP_PIN is specified. It determines how long we have to wait for the rangefinder to give a reading after we set the STOP_PIN high. For a sonar rangefinder with a range of around 7m this would need to be around 50 milliseconds to allow for the sonar pulse to travel to the target and back again." user="Advanced">
<field name="Increment">1</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
</param>
<param humanName="Ratiometric" name="RNGFND3_RMETRIC" documentation="This parameter sets whether an analog rangefinder is ratiometric. Most analog rangefinders are ratiometric, meaning that their output voltage is influenced by the supply voltage. Some analog rangefinders (such as the SF/02) have their own internal voltage regulators so they are not ratiometric." user="Advanced">
<values>
<value code="0">No</value>
<value code="1">Yes</value>
</values>
</param>
<param humanName="Distance (in cm) from the third range finder to the ground" name="RNGFND3_GNDCLEAR" documentation="This parameter sets the expected range measurement(in cm) that the third range finder should return when the vehicle is on the ground." user="Advanced">
<field name="Range">0 127</field>
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Bus address of third rangefinder" name="RNGFND3_ADDR" documentation="This sets the bus address of the sensor, where applicable. Used for the LightWare I2C sensor to allow for multiple sensors on different addresses. A value of 0 disables the sensor." user="Advanced">
<field name="Range">0 127</field>
<field name="Increment">1</field>
</param>
<param humanName=" X position offset" name="RNGFND3_POS_X" documentation="X position of the third rangefinder in body frame. Positive X is forward of the origin. Use the zero range datum point if supplied." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Y position offset" name="RNGFND3_POS_Y" documentation="Y position of the third rangefinder in body frame. Positive Y is to the right of the origin. Use the zero range datum point if supplied." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Z position offset" name="RNGFND3_POS_Z" documentation="Z position of the third rangefinder in body frame. Positive Z is down from the origin. Use the zero range datum point if supplied." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Rangefinder 3 orientation" name="RNGFND3_ORIENT" documentation="Orientation of 3rd rangefinder" user="Advanced">
<values>
<value code="0">Forward</value>
<value code=" 1">Forward-Right</value>
<value code=" 2">Right</value>
<value code=" 3">Back-Right</value>
<value code=" 4">Back</value>
<value code=" 5">Back-Left</value>
<value code=" 6">Left</value>
<value code=" 7">Forward-Left</value>
<value code=" 24">Up</value>
<value code=" 25">Down</value>
</values>
</param>
<param humanName="Fourth Rangefinder type" name="RNGFND4_TYPE" documentation="What type of rangefinder device that is connected" user="Advanced">
<values>
<value code="0">None</value>
<value code="1">Analog</value>
<value code="2">MaxbotixI2C</value>
<value code="3">LidarLiteV2-I2C</value>
<value code="5">PX4-PWM</value>
<value code="6">BBB-PRU</value>
<value code="7">LightWareI2C</value>
<value code="8">LightWareSerial</value>
<value code="9">Bebop</value>
<value code="10">MAVLink</value>
<value code="11">uLanding</value>
5531
5532
5533
5534
5535
5536
5537
5538
5539
5540
5541
5542
5543
5544
5545
5546
5547
5548
5549
5550
5551
5552
5553
5554
5555
5556
5557
5558
5559
5560
5561
5562
5563
5564
5565
5566
5567
5568
5569
5570
5571
5572
5573
5574
5575
5576
5577
5578
5579
5580
5581
5582
5583
5584
5585
5586
5587
5588
5589
5590
5591
5592
5593
5594
5595
5596
5597
5598
5599
5600
<value code="12">LeddarOne</value>
<value code="13">MaxbotixSerial</value>
<value code="14">TrOneI2C</value>
<value code="15">LidarLiteV3-I2C</value>
<value code="16">VL53L0X</value>
</values>
</param>
<param humanName="Rangefinder pin" name="RNGFND4_PIN" documentation="Analog pin that rangefinder is connected to. Set this to 0..9 for the APM2 analog pins. Set to 64 on an APM1 for the dedicated 'airspeed' port on the end of the board. Set to 11 on PX4 for the analog 'airspeed' port. Set to 15 on the Pixhawk for the analog 'airspeed' port." user="Advanced">
<values>
<value code="-1">Not Used</value>
<value code=" 0">APM2-A0</value>
<value code=" 1">APM2-A1</value>
<value code=" 2">APM2-A2</value>
<value code=" 3">APM2-A3</value>
<value code=" 4">APM2-A4</value>
<value code=" 5">APM2-A5</value>
<value code=" 6">APM2-A6</value>
<value code=" 7">APM2-A7</value>
<value code=" 8">APM2-A8</value>
<value code=" 9">APM2-A9</value>
<value code=" 11">PX4-airspeed port</value>
<value code=" 15">Pixhawk-airspeed port</value>
<value code=" 64">APM1-airspeed port</value>
</values>
</param>
<param humanName="Rangefinder scaling" name="RNGFND4_SCALING" documentation="Scaling factor between rangefinder reading and distance. For the linear and inverted functions this is in meters per volt. For the hyperbolic function the units are meterVolts." user="Advanced">
<field name="Increment">0.001</field>
<field name="Units">m/V</field>
<field name="UnitText">meters per volt</field>
</param>
<param humanName="rangefinder offset" name="RNGFND4_OFFSET" documentation="Offset in volts for zero distance" user="Advanced">
<field name="Increment">0.001</field>
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
<param humanName="Rangefinder function" name="RNGFND4_FUNCTION" documentation="Control over what function is used to calculate distance. For a linear function, the distance is (voltage-offset)*scaling. For a inverted function the distance is (offset-voltage)*scaling. For a hyperbolic function the distance is scaling/(voltage-offset). The functions return the distance in meters." user="Advanced">
<values>
<value code="0">Linear</value>
<value code="1">Inverted</value>
<value code="2">Hyperbolic</value>
</values>
</param>
<param humanName="Rangefinder minimum distance" name="RNGFND4_MIN_CM" documentation="Minimum distance in centimeters that rangefinder can reliably read" user="Advanced">
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Rangefinder maximum distance" name="RNGFND4_MAX_CM" documentation="Maximum distance in centimeters that rangefinder can reliably read" user="Advanced">
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Rangefinder stop pin" name="RNGFND4_STOP_PIN" documentation="Digital pin that enables/disables rangefinder measurement for an analog rangefinder. A value of -1 means no pin. If this is set, then the pin is set to 1 to enable the rangefinder and set to 0 to disable it. This can be used to ensure that multiple sonar rangefinders don't interfere with each other." user="Advanced">
<values>
<value code="-1">Not Used</value>
<value code="50">Pixhawk AUXOUT1</value>
<value code="51">Pixhawk AUXOUT2</value>
<value code="52">Pixhawk AUXOUT3</value>
<value code="53">Pixhawk AUXOUT4</value>
<value code="54">Pixhawk AUXOUT5</value>
<value code="55">Pixhawk AUXOUT6</value>
<value code="111">PX4 FMU Relay1</value>
<value code="112">PX4 FMU Relay2</value>
<value code="113">PX4IO Relay1</value>
<value code="114">PX4IO Relay2</value>
<value code="115">PX4IO ACC1</value>
<value code="116">PX4IO ACC2</value>
</values>
</param>
<param humanName="Sonar settle time" name="RNGFND4_SETTLE" documentation="The time in milliseconds that the rangefinder reading takes to settle. This is only used when a STOP_PIN is specified. It determines how long we have to wait for the rangefinder to give a reading after we set the STOP_PIN high. For a sonar rangefinder with a range of around 7m this would need to be around 50 milliseconds to allow for the sonar pulse to travel to the target and back again." user="Advanced">
5601
5602
5603
5604
5605
5606
5607
5608
5609
5610
5611
5612
5613
5614
5615
5616
5617
5618
5619
5620
5621
5622
5623
5624
5625
5626
5627
5628
5629
5630
5631
5632
5633
5634
5635
5636
5637
5638
5639
5640
5641
5642
5643
5644
5645
5646
5647
5648
5649
5650
5651
5652
5653
5654
5655
5656
5657
5658
5659
5660
5661
5662
5663
5664
5665
5666
5667
5668
5669
5670
<field name="Increment">1</field>
<field name="Units">ms</field>
<field name="UnitText">milliseconds</field>
</param>
<param humanName="Ratiometric" name="RNGFND4_RMETRIC" documentation="This parameter sets whether an analog rangefinder is ratiometric. Most analog rangefinders are ratiometric, meaning that their output voltage is influenced by the supply voltage. Some analog rangefinders (such as the SF/02) have their own internal voltage regulators so they are not ratiometric." user="Advanced">
<values>
<value code="0">No</value>
<value code="1">Yes</value>
</values>
</param>
<param humanName="Distance (in cm) from the fourth range finder to the ground" name="RNGFND4_GNDCLEAR" documentation="This parameter sets the expected range measurement(in cm) that the fourth range finder should return when the vehicle is on the ground." user="Advanced">
<field name="Range">0 127</field>
<field name="Increment">1</field>
<field name="Units">cm</field>
<field name="UnitText">centimeters</field>
</param>
<param humanName="Bus address of fourth rangefinder" name="RNGFND4_ADDR" documentation="This sets the bus address of the sensor, where applicable. Used for the LightWare I2C sensor to allow for multiple sensors on different addresses. A value of 0 disables the sensor." user="Advanced">
<field name="Range">0 127</field>
<field name="Increment">1</field>
</param>
<param humanName=" X position offset" name="RNGFND4_POS_X" documentation="X position of the fourth rangefinder in body frame. Use the zero range datum point if supplied." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Y position offset" name="RNGFND4_POS_Y" documentation="Y position of the fourth rangefinder in body frame. Use the zero range datum point if supplied." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Z position offset" name="RNGFND4_POS_Z" documentation="Z position of the fourth rangefinder in body frame. Use the zero range datum point if supplied." user="Advanced">
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Rangefinder 4 orientation" name="RNGFND4_ORIENT" documentation="Orientation of 4th range finder" user="Advanced">
<values>
<value code="0">Forward</value>
<value code=" 1">Forward-Right</value>
<value code=" 2">Right</value>
<value code=" 3">Back-Right</value>
<value code=" 4">Back</value>
<value code=" 5">Back-Left</value>
<value code=" 6">Left</value>
<value code=" 7">Forward-Left</value>
<value code=" 24">Up</value>
<value code=" 25">Down</value>
</values>
</param>
</parameters>
<parameters name="RPM">
<param humanName="RPM type" name="RPM_TYPE" documentation="What type of RPM sensor is connected" user="Standard">
<values>
<value code="0">None</value>
<value code="1">PX4-PWM</value>
<value code="2">AUXPIN</value>
</values>
</param>
<param humanName="RPM scaling" name="RPM_SCALING" documentation="Scaling factor between sensor reading and RPM." user="Standard">
<field name="Increment">0.001</field>
</param>
<param humanName="Maximum RPM" name="RPM_MAX" documentation="Maximum RPM to report" user="Standard">
<field name="Increment">1</field>
</param>
<param humanName="Minimum RPM" name="RPM_MIN" documentation="Minimum RPM to report" user="Standard">
<field name="Increment">1</field>
</param>
<param humanName="Minimum Quality" name="RPM_MIN_QUAL" documentation="Minimum data quality to be used" user="Advanced">
<field name="Increment">0.1</field>
</param>
<param humanName="Input pin number" name="RPM_PIN" documentation="Which pin to use" user="Standard">
<values>
<value code="-1">Disabled</value>
5671
5672
5673
5674
5675
5676
5677
5678
5679
5680
5681
5682
5683
5684
5685
5686
5687
5688
5689
5690
5691
5692
5693
5694
5695
5696
5697
5698
5699
5700
5701
5702
5703
5704
5705
5706
5707
5708
5709
5710
5711
5712
5713
5714
5715
5716
5717
5718
5719
5720
5721
5722
5723
5724
5725
5726
5727
5728
5729
5730
5731
5732
5733
5734
5735
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5737
5738
5739
5740
<value code="50">PixhawkAUX1</value>
<value code="51">PixhawkAUX2</value>
<value code="52">PixhawkAUX3</value>
<value code="53">PixhawkAUX4</value>
<value code="54">PixhawkAUX5</value>
<value code="55">PixhawkAUX6</value>
</values>
</param>
<param humanName="Second RPM type" name="RPM2_TYPE" documentation="What type of RPM sensor is connected" user="Advanced">
<values>
<value code="0">None</value>
<value code="1">PX4-PWM</value>
<value code="2">AUXPIN</value>
</values>
</param>
<param humanName="RPM scaling" name="RPM2_SCALING" documentation="Scaling factor between sensor reading and RPM." user="Advanced">
<field name="Increment">0.001</field>
</param>
<param humanName="RPM2 input pin number" name="RPM2_PIN" documentation="Which pin to use" user="Standard">
<values>
<value code="-1">Disabled</value>
<value code="50">PixhawkAUX1</value>
<value code="51">PixhawkAUX2</value>
<value code="52">PixhawkAUX3</value>
<value code="53">PixhawkAUX4</value>
<value code="54">PixhawkAUX5</value>
<value code="55">PixhawkAUX6</value>
</values>
</param>
</parameters>
<parameters name="RSSI_">
<param humanName="RSSI Type" name="RSSI_TYPE" documentation="Radio Receiver RSSI type. If your radio receiver supports RSSI of some kind, set it here, then set its associated RSSI_XXXXX parameters, if any." user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">AnalogPin</value>
<value code="2">RCChannelPwmValue</value>
<value code="3">ReceiverProtocol</value>
</values>
</param>
<param humanName="Receiver RSSI analog sensing pin" name="RSSI_ANA_PIN" documentation="This selects an analog pin where the receiver RSSI voltage will be read." user="Standard">
<values>
<value code="0">APM2 A0</value>
<value code="1">APM2 A1</value>
<value code="13">APM2 A13</value>
<value code="11">Pixracer</value>
<value code="13">Pixhawk ADC4</value>
<value code="14">Pixhawk ADC3</value>
<value code="15"> Pixhawk ADC6</value>
<value code="103">Pixhawk SBUS</value>
</values>
</param>
<param humanName="Receiver RSSI voltage low" name="RSSI_PIN_LOW" documentation="This is the voltage value that the radio receiver will put on the RSSI_ANA_PIN when the signal strength is the weakest. Since some radio receivers put out inverted values from what you might otherwise expect, this isn't necessarily a lower value than RSSI_PIN_HIGH. " user="Standard">
<field name="Range">0 5.0</field>
<field name="Increment">0.01</field>
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
<param humanName="Receiver RSSI voltage high" name="RSSI_PIN_HIGH" documentation="This is the voltage value that the radio receiver will put on the RSSI_ANA_PIN when the signal strength is the strongest. Since some radio receivers put out inverted values from what you might otherwise expect, this isn't necessarily a higher value than RSSI_PIN_LOW. " user="Standard">
<field name="Range">0 5.0</field>
<field name="Increment">0.01</field>
<field name="Units">V</field>
<field name="UnitText">volt</field>
</param>
<param humanName="Receiver RSSI channel number" name="RSSI_CHANNEL" documentation="The channel number where RSSI will be output by the radio receiver (5 and above)." user="Standard">
</param>
<param humanName="Receiver RSSI PWM low value" name="RSSI_CHAN_LOW" documentation="This is the PWM value in microseconds that the radio receiver will put on the RSSI_CHANNEL when the signal strength is the weakest. Since some radio receivers put out inverted values from what you might otherwise expect, this isn't necessarily a lower value than RSSI_CHAN_HIGH." user="Standard">
<field name="Range">0 2000</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
5741
5742
5743
5744
5745
5746
5747
5748
5749
5750
5751
5752
5753
5754
5755
5756
5757
5758
5759
5760
5761
5762
5763
5764
5765
5766
5767
5768
5769
5770
5771
5772
5773
5774
5775
5776
5777
5778
5779
5780
5781
5782
5783
5784
5785
5786
5787
5788
5789
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5791
5792
5793
5794
5795
5796
5797
5798
5799
5800
5801
5802
5803
5804
5805
5806
5807
5808
5809
5810
<param humanName="Receiver RSSI PWM high value" name="RSSI_CHAN_HIGH" documentation="This is the PWM value in microseconds that the radio receiver will put on the RSSI_CHANNEL when the signal strength is the strongest. Since some radio receivers put out inverted values from what you might otherwise expect, this isn't necessarily a higher value than RSSI_CHAN_LOW." user="Standard">
<field name="Range">0 2000</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
</parameters>
<parameters name="SCHED_">
<param humanName="Scheduler debug level" name="SCHED_DEBUG" documentation='Set to non-zero to enable scheduler debug messages. When set to show "Slips" the scheduler will display a message whenever a scheduled task is delayed due to too much CPU load. When set to ShowOverruns the scheduled will display a message whenever a task takes longer than the limit promised in the task table.' user="Advanced">
<values>
<value code="0">Disabled</value>
<value code="2">ShowSlips</value>
<value code="3">ShowOverruns</value>
</values>
</param>
<param humanName="Scheduling main loop rate" name="SCHED_LOOP_RATE" documentation="This controls the rate of the main control loop in Hz. This should only be changed by developers. This only takes effect on restart" user="Advanced">
<values>
<value code="50">50Hz</value>
<value code="100">100Hz</value>
<value code="200">200Hz</value>
<value code="250">250Hz</value>
<value code="300">300Hz</value>
<value code="400">400Hz</value>
</values>
<field name="RebootRequired">True</field>
</param>
</parameters>
<parameters name="SERIAL">
<param humanName="Serial0 baud rate" name="SERIAL0_BAUD" documentation="The baud rate used on the USB console. The APM2 can support all baudrates up to 115, and also can support 500. The PX4 can support rates of up to 1500. If you setup a rate you cannot support on APM2 and then can't connect to your board you should load a firmware from a different vehicle type. That will reset all your parameters to defaults." user="Standard">
<values>
<value code="1">1200</value>
<value code="2">2400</value>
<value code="4">4800</value>
<value code="9">9600</value>
<value code="19">19200</value>
<value code="38">38400</value>
<value code="57">57600</value>
<value code="111">111100</value>
<value code="115">115200</value>
<value code="460">460800</value>
<value code="500">500000</value>
<value code="921">921600</value>
<value code="1500">1500000</value>
</values>
</param>
<param humanName="Console protocol selection" name="SERIAL0_PROTOCOL" documentation="Control what protocol to use on the console. " user="Standard">
<values>
<value code="1">MAVlink1</value>
<value code=" 2">MAVLink2</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Telem1 protocol selection" name="SERIAL1_PROTOCOL" documentation="Control what protocol to use on the Telem1 port. Note that the Frsky options require external converter hardware. See the wiki for details." user="Standard">
<values>
<value code="-1">None</value>
<value code=" 1">MAVLink1</value>
<value code=" 2">MAVLink2</value>
<value code=" 3">Frsky D</value>
<value code=" 4">Frsky SPort</value>
<value code=" 5">GPS</value>
<value code=" 7">Alexmos Gimbal Serial</value>
<value code=" 8">SToRM32 Gimbal Serial</value>
<value code=" 9">Lidar</value>
<value code=" 10">FrSky SPort Passthrough (OpenTX)</value>
<value code=" 11">Lidar360</value>
<value code=" 12">Aerotenna uLanding</value>
<value code=" 13">Beacon</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Telem1 Baud Rate" name="SERIAL1_BAUD" documentation="The baud rate used on the Telem1 port. The APM2 can support all baudrates up to 115, and also can support 500. The PX4 can support rates of up to 1500. If you setup a rate you cannot support on APM2 and then can't connect to your board you should load a firmware from a different vehicle type. That will reset all your parameters to defaults." user="Standard">
5811
5812
5813
5814
5815
5816
5817
5818
5819
5820
5821
5822
5823
5824
5825
5826
5827
5828
5829
5830
5831
5832
5833
5834
5835
5836
5837
5838
5839
5840
5841
5842
5843
5844
5845
5846
5847
5848
5849
5850
5851
5852
5853
5854
5855
5856
5857
5858
5859
5860
5861
5862
5863
5864
5865
5866
5867
5868
5869
5870
5871
5872
5873
5874
5875
5876
5877
5878
5879
5880
<values>
<value code="1">1200</value>
<value code="2">2400</value>
<value code="4">4800</value>
<value code="9">9600</value>
<value code="19">19200</value>
<value code="38">38400</value>
<value code="57">57600</value>
<value code="111">111100</value>
<value code="115">115200</value>
<value code="500">500000</value>
<value code="921">921600</value>
<value code="1500">1500000</value>
</values>
</param>
<param humanName="Telemetry 2 protocol selection" name="SERIAL2_PROTOCOL" documentation="Control what protocol to use on the Telem2 port. Note that the Frsky options require external converter hardware. See the wiki for details." user="Standard">
<values>
<value code="-1">None</value>
<value code=" 1">MAVLink1</value>
<value code=" 2">MAVLink2</value>
<value code=" 3">Frsky D</value>
<value code=" 4">Frsky SPort</value>
<value code=" 5">GPS</value>
<value code=" 7">Alexmos Gimbal Serial</value>
<value code=" 8">SToRM32 Gimbal Serial</value>
<value code=" 9">Lidar</value>
<value code=" 10">FrSky SPort Passthrough (OpenTX)</value>
<value code=" 11">Lidar360</value>
<value code=" 12">Aerotenna uLanding</value>
<value code=" 13">Beacon</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Telemetry 2 Baud Rate" name="SERIAL2_BAUD" documentation="The baud rate of the Telem2 port. The APM2 can support all baudrates up to 115, and also can support 500. The PX4 can support rates of up to 1500. If you setup a rate you cannot support on APM2 and then can't connect to your board you should load a firmware from a different vehicle type. That will reset all your parameters to defaults." user="Standard">
<values>
<value code="1">1200</value>
<value code="2">2400</value>
<value code="4">4800</value>
<value code="9">9600</value>
<value code="19">19200</value>
<value code="38">38400</value>
<value code="57">57600</value>
<value code="111">111100</value>
<value code="115">115200</value>
<value code="500">500000</value>
<value code="921">921600</value>
<value code="1500">1500000</value>
</values>
</param>
<param humanName="Serial 3 (GPS) protocol selection" name="SERIAL3_PROTOCOL" documentation="Control what protocol Serial 3 (GPS) should be used for. Note that the Frsky options require external converter hardware. See the wiki for details." user="Standard">
<values>
<value code="-1">None</value>
<value code=" 1">MAVLink1</value>
<value code=" 2">MAVLink2</value>
<value code=" 3">Frsky D</value>
<value code=" 4">Frsky SPort</value>
<value code=" 5">GPS</value>
<value code=" 7">Alexmos Gimbal Serial</value>
<value code=" 8">SToRM32 Gimbal Serial</value>
<value code=" 9">Lidar</value>
<value code=" 10">FrSky SPort Passthrough (OpenTX)</value>
<value code=" 11">Lidar360</value>
<value code=" 12">Aerotenna uLanding</value>
<value code=" 13">Beacon</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Serial 3 (GPS) Baud Rate" name="SERIAL3_BAUD" documentation="The baud rate used for the Serial 3 (GPS). The APM2 can support all baudrates up to 115, and also can support 500. The PX4 can support rates of up to 1500. If you setup a rate you cannot support on APM2 and then can't connect to your board you should load a firmware from a different vehicle type. That will reset all your parameters to defaults." user="Standard">
<values>
<value code="1">1200</value>
5881
5882
5883
5884
5885
5886
5887
5888
5889
5890
5891
5892
5893
5894
5895
5896
5897
5898
5899
5900
5901
5902
5903
5904
5905
5906
5907
5908
5909
5910
5911
5912
5913
5914
5915
5916
5917
5918
5919
5920
5921
5922
5923
5924
5925
5926
5927
5928
5929
5930
5931
5932
5933
5934
5935
5936
5937
5938
5939
5940
5941
5942
5943
5944
5945
5946
5947
5948
5949
5950
<value code="2">2400</value>
<value code="4">4800</value>
<value code="9">9600</value>
<value code="19">19200</value>
<value code="38">38400</value>
<value code="57">57600</value>
<value code="111">111100</value>
<value code="115">115200</value>
<value code="500">500000</value>
<value code="921">921600</value>
<value code="1500">1500000</value>
</values>
</param>
<param humanName="Serial4 protocol selection" name="SERIAL4_PROTOCOL" documentation="Control what protocol Serial4 port should be used for. Note that the Frsky options require external converter hardware. See the wiki for details." user="Standard">
<values>
<value code="-1">None</value>
<value code=" 1">MAVLink1</value>
<value code=" 2">MAVLink2</value>
<value code=" 3">Frsky D</value>
<value code=" 4">Frsky SPort</value>
<value code=" 5">GPS</value>
<value code=" 7">Alexmos Gimbal Serial</value>
<value code=" 8">SToRM32 Gimbal Serial</value>
<value code=" 9">Lidar</value>
<value code=" 10">FrSky SPort Passthrough (OpenTX)</value>
<value code=" 11">Lidar360</value>
<value code=" 12">Aerotenna uLanding</value>
<value code=" 13">Beacon</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Serial 4 Baud Rate" name="SERIAL4_BAUD" documentation="The baud rate used for Serial4. The APM2 can support all baudrates up to 115, and also can support 500. The PX4 can support rates of up to 1500. If you setup a rate you cannot support on APM2 and then can't connect to your board you should load a firmware from a different vehicle type. That will reset all your parameters to defaults." user="Standard">
<values>
<value code="1">1200</value>
<value code="2">2400</value>
<value code="4">4800</value>
<value code="9">9600</value>
<value code="19">19200</value>
<value code="38">38400</value>
<value code="57">57600</value>
<value code="111">111100</value>
<value code="115">115200</value>
<value code="500">500000</value>
<value code="921">921600</value>
<value code="1500">1500000</value>
</values>
</param>
<param humanName="Serial5 protocol selection" name="SERIAL5_PROTOCOL" documentation="Control what protocol Serial5 port should be used for. Note that the Frsky options require external converter hardware. See the wiki for details." user="Standard">
<values>
<value code="-1">None</value>
<value code=" 1">MAVLink1</value>
<value code=" 2">MAVLink2</value>
<value code=" 3">Frsky D</value>
<value code=" 4">Frsky SPort</value>
<value code=" 5">GPS</value>
<value code=" 7">Alexmos Gimbal Serial</value>
<value code=" 8">SToRM32 Gimbal Serial</value>
<value code=" 9">Lidar</value>
<value code=" 10">FrSky SPort Passthrough (OpenTX)</value>
<value code=" 11">Lidar360</value>
<value code=" 12">Aerotenna uLanding</value>
<value code=" 13">Beacon</value>
</values>
<field name="RebootRequired">True</field>
</param>
<param humanName="Serial 5 Baud Rate" name="SERIAL5_BAUD" documentation="The baud rate used for Serial5. The APM2 can support all baudrates up to 115, and also can support 500. The PX4 can support rates of up to 1500. If you setup a rate you cannot support on APM2 and then can't connect to your board you should load a firmware from a different vehicle type. That will reset all your parameters to defaults." user="Standard">
<values>
<value code="1">1200</value>
<value code="2">2400</value>
<value code="4">4800</value>
5951
5952
5953
5954
5955
5956
5957
5958
5959
5960
5961
5962
5963
5964
5965
5966
5967
5968
5969
5970
5971
5972
5973
5974
5975
5976
5977
5978
5979
5980
5981
5982
5983
5984
5985
5986
5987
5988
5989
5990
5991
5992
5993
5994
5995
5996
5997
5998
5999
6000
6001
6002
6003
6004
6005
6006
6007
6008
6009
6010
6011
6012
6013
6014
6015
6016
6017
6018
6019
6020
<value code="9">9600</value>
<value code="19">19200</value>
<value code="38">38400</value>
<value code="57">57600</value>
<value code="111">111100</value>
<value code="115">115200</value>
<value code="500">500000</value>
<value code="921">921600</value>
<value code="1500">1500000</value>
</values>
</param>
</parameters>
<parameters name="SERVO">
<param humanName="Automatic servo trim" name="SERVO_AUTO_TRIM" documentation="This enables automatic servo trim in flight. Servos will be trimed in stabilized flight modes when the aircraft is close to level. Changes to servo trim will be saved every 10 seconds and will persist between flights." user="Advanced">
<values>
<value code="0">Disable</value>
<value code="1">Enable</value>
</values>
</param>
<param humanName="Servo default output rate" name="SERVO_RATE" documentation="This sets the default output rate in Hz for all outputs." user="Advanced">
<field name="Range">25 400</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
</parameters>
<parameters name="SERVO10_">
<param humanName="Minimum PWM" name="SERVO10_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO10_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO10_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO10_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO10_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
6021
6022
6023
6024
6025
6026
6027
6028
6029
6030
6031
6032
6033
6034
6035
6036
6037
6038
6039
6040
6041
6042
6043
6044
6045
6046
6047
6048
6049
6050
6051
6052
6053
6054
6055
6056
6057
6058
6059
6060
6061
6062
6063
6064
6065
6066
6067
6068
6069
6070
6071
6072
6073
6074
6075
6076
6077
6078
6079
6080
6081
6082
6083
6084
6085
6086
6087
6088
6089
6090
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO11_">
<param humanName="Minimum PWM" name="SERVO11_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO11_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
6091
6092
6093
6094
6095
6096
6097
6098
6099
6100
6101
6102
6103
6104
6105
6106
6107
6108
6109
6110
6111
6112
6113
6114
6115
6116
6117
6118
6119
6120
6121
6122
6123
6124
6125
6126
6127
6128
6129
6130
6131
6132
6133
6134
6135
6136
6137
6138
6139
6140
6141
6142
6143
6144
6145
6146
6147
6148
6149
6150
6151
6152
6153
6154
6155
6156
6157
6158
6159
6160
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO11_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO11_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO11_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
6161
6162
6163
6164
6165
6166
6167
6168
6169
6170
6171
6172
6173
6174
6175
6176
6177
6178
6179
6180
6181
6182
6183
6184
6185
6186
6187
6188
6189
6190
6191
6192
6193
6194
6195
6196
6197
6198
6199
6200
6201
6202
6203
6204
6205
6206
6207
6208
6209
6210
6211
6212
6213
6214
6215
6216
6217
6218
6219
6220
6221
6222
6223
6224
6225
6226
6227
6228
6229
6230
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO12_">
<param humanName="Minimum PWM" name="SERVO12_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO12_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO12_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO12_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO12_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
6231
6232
6233
6234
6235
6236
6237
6238
6239
6240
6241
6242
6243
6244
6245
6246
6247
6248
6249
6250
6251
6252
6253
6254
6255
6256
6257
6258
6259
6260
6261
6262
6263
6264
6265
6266
6267
6268
6269
6270
6271
6272
6273
6274
6275
6276
6277
6278
6279
6280
6281
6282
6283
6284
6285
6286
6287
6288
6289
6290
6291
6292
6293
6294
6295
6296
6297
6298
6299
6300
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO13_">
<param humanName="Minimum PWM" name="SERVO13_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO13_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
6301
6302
6303
6304
6305
6306
6307
6308
6309
6310
6311
6312
6313
6314
6315
6316
6317
6318
6319
6320
6321
6322
6323
6324
6325
6326
6327
6328
6329
6330
6331
6332
6333
6334
6335
6336
6337
6338
6339
6340
6341
6342
6343
6344
6345
6346
6347
6348
6349
6350
6351
6352
6353
6354
6355
6356
6357
6358
6359
6360
6361
6362
6363
6364
6365
6366
6367
6368
6369
6370
<param humanName="Trim PWM" name="SERVO13_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO13_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO13_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
6371
6372
6373
6374
6375
6376
6377
6378
6379
6380
6381
6382
6383
6384
6385
6386
6387
6388
6389
6390
6391
6392
6393
6394
6395
6396
6397
6398
6399
6400
6401
6402
6403
6404
6405
6406
6407
6408
6409
6410
6411
6412
6413
6414
6415
6416
6417
6418
6419
6420
6421
6422
6423
6424
6425
6426
6427
6428
6429
6430
6431
6432
6433
6434
6435
6436
6437
6438
6439
6440
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO14_">
<param humanName="Minimum PWM" name="SERVO14_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO14_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO14_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO14_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO14_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
6441
6442
6443
6444
6445
6446
6447
6448
6449
6450
6451
6452
6453
6454
6455
6456
6457
6458
6459
6460
6461
6462
6463
6464
6465
6466
6467
6468
6469
6470
6471
6472
6473
6474
6475
6476
6477
6478
6479
6480
6481
6482
6483
6484
6485
6486
6487
6488
6489
6490
6491
6492
6493
6494
6495
6496
6497
6498
6499
6500
6501
6502
6503
6504
6505
6506
6507
6508
6509
6510
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO15_">
<param humanName="Minimum PWM" name="SERVO15_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO15_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO15_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
6511
6512
6513
6514
6515
6516
6517
6518
6519
6520
6521
6522
6523
6524
6525
6526
6527
6528
6529
6530
6531
6532
6533
6534
6535
6536
6537
6538
6539
6540
6541
6542
6543
6544
6545
6546
6547
6548
6549
6550
6551
6552
6553
6554
6555
6556
6557
6558
6559
6560
6561
6562
6563
6564
6565
6566
6567
6568
6569
6570
6571
6572
6573
6574
6575
6576
6577
6578
6579
6580
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO15_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO15_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
6581
6582
6583
6584
6585
6586
6587
6588
6589
6590
6591
6592
6593
6594
6595
6596
6597
6598
6599
6600
6601
6602
6603
6604
6605
6606
6607
6608
6609
6610
6611
6612
6613
6614
6615
6616
6617
6618
6619
6620
6621
6622
6623
6624
6625
6626
6627
6628
6629
6630
6631
6632
6633
6634
6635
6636
6637
6638
6639
6640
6641
6642
6643
6644
6645
6646
6647
6648
6649
6650
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO16_">
<param humanName="Minimum PWM" name="SERVO16_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO16_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO16_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO16_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO16_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
6651
6652
6653
6654
6655
6656
6657
6658
6659
6660
6661
6662
6663
6664
6665
6666
6667
6668
6669
6670
6671
6672
6673
6674
6675
6676
6677
6678
6679
6680
6681
6682
6683
6684
6685
6686
6687
6688
6689
6690
6691
6692
6693
6694
6695
6696
6697
6698
6699
6700
6701
6702
6703
6704
6705
6706
6707
6708
6709
6710
6711
6712
6713
6714
6715
6716
6717
6718
6719
6720
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO1_">
<param humanName="Minimum PWM" name="SERVO1_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO1_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO1_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
6721
6722
6723
6724
6725
6726
6727
6728
6729
6730
6731
6732
6733
6734
6735
6736
6737
6738
6739
6740
6741
6742
6743
6744
6745
6746
6747
6748
6749
6750
6751
6752
6753
6754
6755
6756
6757
6758
6759
6760
6761
6762
6763
6764
6765
6766
6767
6768
6769
6770
6771
6772
6773
6774
6775
6776
6777
6778
6779
6780
6781
6782
6783
6784
6785
6786
6787
6788
6789
6790
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO1_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO1_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
6791
6792
6793
6794
6795
6796
6797
6798
6799
6800
6801
6802
6803
6804
6805
6806
6807
6808
6809
6810
6811
6812
6813
6814
6815
6816
6817
6818
6819
6820
6821
6822
6823
6824
6825
6826
6827
6828
6829
6830
6831
6832
6833
6834
6835
6836
6837
6838
6839
6840
6841
6842
6843
6844
6845
6846
6847
6848
6849
6850
6851
6852
6853
6854
6855
6856
6857
6858
6859
6860
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO2_">
<param humanName="Minimum PWM" name="SERVO2_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO2_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO2_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO2_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO2_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
6861
6862
6863
6864
6865
6866
6867
6868
6869
6870
6871
6872
6873
6874
6875
6876
6877
6878
6879
6880
6881
6882
6883
6884
6885
6886
6887
6888
6889
6890
6891
6892
6893
6894
6895
6896
6897
6898
6899
6900
6901
6902
6903
6904
6905
6906
6907
6908
6909
6910
6911
6912
6913
6914
6915
6916
6917
6918
6919
6920
6921
6922
6923
6924
6925
6926
6927
6928
6929
6930
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO3_">
<param humanName="Minimum PWM" name="SERVO3_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO3_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO3_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
6931
6932
6933
6934
6935
6936
6937
6938
6939
6940
6941
6942
6943
6944
6945
6946
6947
6948
6949
6950
6951
6952
6953
6954
6955
6956
6957
6958
6959
6960
6961
6962
6963
6964
6965
6966
6967
6968
6969
6970
6971
6972
6973
6974
6975
6976
6977
6978
6979
6980
6981
6982
6983
6984
6985
6986
6987
6988
6989
6990
6991
6992
6993
6994
6995
6996
6997
6998
6999
7000
<param humanName="Servo reverse" name="SERVO3_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO3_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
7001
7002
7003
7004
7005
7006
7007
7008
7009
7010
7011
7012
7013
7014
7015
7016
7017
7018
7019
7020
7021
7022
7023
7024
7025
7026
7027
7028
7029
7030
7031
7032
7033
7034
7035
7036
7037
7038
7039
7040
7041
7042
7043
7044
7045
7046
7047
7048
7049
7050
7051
7052
7053
7054
7055
7056
7057
7058
7059
7060
7061
7062
7063
7064
7065
7066
7067
7068
7069
7070
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO4_">
<param humanName="Minimum PWM" name="SERVO4_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO4_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO4_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO4_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO4_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
7071
7072
7073
7074
7075
7076
7077
7078
7079
7080
7081
7082
7083
7084
7085
7086
7087
7088
7089
7090
7091
7092
7093
7094
7095
7096
7097
7098
7099
7100
7101
7102
7103
7104
7105
7106
7107
7108
7109
7110
7111
7112
7113
7114
7115
7116
7117
7118
7119
7120
7121
7122
7123
7124
7125
7126
7127
7128
7129
7130
7131
7132
7133
7134
7135
7136
7137
7138
7139
7140
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO5_">
<param humanName="Minimum PWM" name="SERVO5_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO5_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO5_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO5_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
7141
7142
7143
7144
7145
7146
7147
7148
7149
7150
7151
7152
7153
7154
7155
7156
7157
7158
7159
7160
7161
7162
7163
7164
7165
7166
7167
7168
7169
7170
7171
7172
7173
7174
7175
7176
7177
7178
7179
7180
7181
7182
7183
7184
7185
7186
7187
7188
7189
7190
7191
7192
7193
7194
7195
7196
7197
7198
7199
7200
7201
7202
7203
7204
7205
7206
7207
7208
7209
7210
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO5_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
7211
7212
7213
7214
7215
7216
7217
7218
7219
7220
7221
7222
7223
7224
7225
7226
7227
7228
7229
7230
7231
7232
7233
7234
7235
7236
7237
7238
7239
7240
7241
7242
7243
7244
7245
7246
7247
7248
7249
7250
7251
7252
7253
7254
7255
7256
7257
7258
7259
7260
7261
7262
7263
7264
7265
7266
7267
7268
7269
7270
7271
7272
7273
7274
7275
7276
7277
7278
7279
7280
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO6_">
<param humanName="Minimum PWM" name="SERVO6_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO6_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO6_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO6_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO6_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
7281
7282
7283
7284
7285
7286
7287
7288
7289
7290
7291
7292
7293
7294
7295
7296
7297
7298
7299
7300
7301
7302
7303
7304
7305
7306
7307
7308
7309
7310
7311
7312
7313
7314
7315
7316
7317
7318
7319
7320
7321
7322
7323
7324
7325
7326
7327
7328
7329
7330
7331
7332
7333
7334
7335
7336
7337
7338
7339
7340
7341
7342
7343
7344
7345
7346
7347
7348
7349
7350
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO7_">
<param humanName="Minimum PWM" name="SERVO7_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO7_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO7_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO7_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
7351
7352
7353
7354
7355
7356
7357
7358
7359
7360
7361
7362
7363
7364
7365
7366
7367
7368
7369
7370
7371
7372
7373
7374
7375
7376
7377
7378
7379
7380
7381
7382
7383
7384
7385
7386
7387
7388
7389
7390
7391
7392
7393
7394
7395
7396
7397
7398
7399
7400
7401
7402
7403
7404
7405
7406
7407
7408
7409
7410
7411
7412
7413
7414
7415
7416
7417
7418
7419
7420
</values>
</param>
<param humanName="Servo output function" name="SERVO7_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
7421
7422
7423
7424
7425
7426
7427
7428
7429
7430
7431
7432
7433
7434
7435
7436
7437
7438
7439
7440
7441
7442
7443
7444
7445
7446
7447
7448
7449
7450
7451
7452
7453
7454
7455
7456
7457
7458
7459
7460
7461
7462
7463
7464
7465
7466
7467
7468
7469
7470
7471
7472
7473
7474
7475
7476
7477
7478
7479
7480
7481
7482
7483
7484
7485
7486
7487
7488
7489
7490
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO8_">
<param humanName="Minimum PWM" name="SERVO8_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO8_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO8_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO8_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
<param humanName="Servo output function" name="SERVO8_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
7491
7492
7493
7494
7495
7496
7497
7498
7499
7500
7501
7502
7503
7504
7505
7506
7507
7508
7509
7510
7511
7512
7513
7514
7515
7516
7517
7518
7519
7520
7521
7522
7523
7524
7525
7526
7527
7528
7529
7530
7531
7532
7533
7534
7535
7536
7537
7538
7539
7540
7541
7542
7543
7544
7545
7546
7547
7548
7549
7550
7551
7552
7553
7554
7555
7556
7557
7558
7559
7560
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SERVO9_">
<param humanName="Minimum PWM" name="SERVO9_MIN" documentation="minimum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Maximum PWM" name="SERVO9_MAX" documentation="maximum PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Trim PWM" name="SERVO9_TRIM" documentation="Trim PWM pulse width in microseconds. Typically 1000 is lower limit, 1500 is neutral and 2000 is upper limit." user="Standard">
<field name="Range">800 2200</field>
<field name="Increment">1</field>
<field name="Units">PWM</field>
<field name="UnitText">PWM in microseconds</field>
</param>
<param humanName="Servo reverse" name="SERVO9_REVERSED" documentation="Reverse servo operation. Set to 0 for normal operation. Set to 1 to reverse this output channel." user="Standard">
<values>
<value code="0">Normal</value>
<value code="1">Reversed</value>
</values>
</param>
7561
7562
7563
7564
7565
7566
7567
7568
7569
7570
7571
7572
7573
7574
7575
7576
7577
7578
7579
7580
7581
7582
7583
7584
7585
7586
7587
7588
7589
7590
7591
7592
7593
7594
7595
7596
7597
7598
7599
7600
7601
7602
7603
7604
7605
7606
7607
7608
7609
7610
7611
7612
7613
7614
7615
7616
7617
7618
7619
7620
7621
7622
7623
7624
7625
7626
7627
7628
7629
7630
<param humanName="Servo output function" name="SERVO9_FUNCTION" documentation="Function assigned to this servo. Seeing this to Disabled(0) will setup this output for control by auto missions or MAVLink servo set commands. any other value will enable the corresponding function" user="Standard">
<values>
<value code="0">Disabled</value>
<value code="1">RCPassThru</value>
<value code="2">Flap</value>
<value code="3">Flap_auto</value>
<value code="4">Aileron</value>
<value code="6">mount_pan</value>
<value code="7">mount_tilt</value>
<value code="8">mount_roll</value>
<value code="9">mount_open</value>
<value code="10">camera_trigger</value>
<value code="11">release</value>
<value code="12">mount2_pan</value>
<value code="13">mount2_tilt</value>
<value code="14">mount2_roll</value>
<value code="15">mount2_open</value>
<value code="16">DifferentialSpoilerLeft1</value>
<value code="17">DifferentialSpoilerRight1</value>
<value code="86">DifferentialSpoilerLeft2</value>
<value code="87">DifferentialSpoilerRight2</value>
<value code="19">Elevator</value>
<value code="21">Rudder</value>
<value code="24">FlaperonLeft</value>
<value code="25">FlaperonRight</value>
<value code="26">GroundSteering</value>
<value code="27">Parachute</value>
<value code="28">EPM</value>
<value code="29">LandingGear</value>
<value code="30">EngineRunEnable</value>
<value code="31">HeliRSC</value>
<value code="32">HeliTailRSC</value>
<value code="33">Motor1</value>
<value code="34">Motor2</value>
<value code="35">Motor3</value>
<value code="36">Motor4</value>
<value code="37">Motor5</value>
<value code="38">Motor6</value>
<value code="39">Motor7</value>
<value code="40">Motor8</value>
<value code="41">MotorTilt</value>
<value code="51">RCIN1</value>
<value code="52">RCIN2</value>
<value code="53">RCIN3</value>
<value code="54">RCIN4</value>
<value code="55">RCIN5</value>
<value code="56">RCIN6</value>
<value code="57">RCIN7</value>
<value code="58">RCIN8</value>
<value code="59">RCIN9</value>
<value code="60">RCIN10</value>
<value code="61">RCIN11</value>
<value code="62">RCIN12</value>
<value code="63">RCIN13</value>
<value code="64">RCIN14</value>
<value code="65">RCIN15</value>
<value code="66">RCIN16</value>
<value code="67">Ignition</value>
<value code="68">Choke</value>
<value code="69">Starter</value>
<value code="70">Throttle</value>
<value code="71">TrackerYaw</value>
<value code="72">TrackerPitch</value>
<value code="73">ThrottleLeft</value>
<value code="74">ThrottleRight</value>
<value code="75">tiltMotorLeft</value>
<value code="76">tiltMotorRight</value>
<value code="77">ElevonLeft</value>
<value code="78">ElevonRight</value>
<value code="79">VTailLeft</value>
7631
7632
7633
7634
7635
7636
7637
7638
7639
7640
7641
7642
7643
7644
7645
7646
7647
7648
7649
7650
7651
7652
7653
7654
7655
7656
7657
7658
7659
7660
7661
7662
7663
7664
7665
7666
7667
7668
7669
7670
7671
7672
7673
7674
7675
7676
7677
7678
7679
7680
7681
7682
7683
7684
7685
7686
7687
7688
7689
7690
7691
7692
7693
7694
7695
7696
7697
7698
7699
7700
<value code="80">VTailRight</value>
<value code="81">BoostThrottle</value>
<value code="82">Motor9</value>
<value code="83">Motor10</value>
<value code="84">Motor11</value>
<value code="85">Motor12</value>
</values>
</param>
</parameters>
<parameters name="SOAR_">
<param humanName="Is the soaring mode enabled or not" name="SOAR_ENABLE" documentation="Toggles the soaring mode on and off" user="Advanced">
<values>
<value code="0">Disable</value>
<value code="1">Enable</value>
</values>
</param>
<param humanName="Vertical v-speed" name="SOAR_VSPEED" documentation="Rate of climb to trigger themalling speed" user="Advanced">
<field name="Range">0 10</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Distance to thermal center" name="SOAR_DIST_AHEAD" documentation="Initial guess of the distance to the thermal center" user="Advanced">
<field name="Range">0 100</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Minimum thermalling time" name="SOAR_MIN_THML_S" documentation="Minimum number of seconds to spend thermalling" user="Advanced">
<field name="Range">0 32768</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Minimum cruising time" name="SOAR_MIN_CRSE_S" documentation="Minimum number of seconds to spend cruising" user="Advanced">
<field name="Range">0 32768</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Cl factor" name="SOAR_POLAR_K" documentation="Cl factor 2*m*g/(rho*S)" user="Advanced">
<field name="Range">0 0.5</field>
<field name="Units">m.m/s/s</field>
<field name="UnitText">square meter per square second</field>
</param>
<param humanName="Maximum soaring altitude, relative to the home location" name="SOAR_ALT_MAX" documentation="Don't thermal any higher than this." user="Advanced">
<field name="Range">0 1000.0</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Minimum soaring altitude, relative to the home location" name="SOAR_ALT_MIN" documentation="Don't get any lower than this." user="Advanced">
<field name="Range">0 1000.0</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="Maximum power altitude, relative to the home location" name="SOAR_ALT_CUTOFF" documentation="Cut off throttle at this alt." user="Advanced">
<field name="Range">0 1000.0</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
<param humanName="(Optional) RC channel that toggles the soaring controller on and off" name="SOAR_ENABLE_CH" documentation="Toggles the soaring controller on and off. This parameter has any effect only if SOAR_ENABLE is set to 1 and this parameter is set to a valid non-zero channel number. When set, soaring will be activated when RC input to the specified channel is greater than or equal to 1700." user="Advanced">
<field name="Range">0 16</field>
</param>
</parameters>
<parameters name="SR0_">
<param humanName="Raw sensor stream rate" name="SR0_RAW_SENS" documentation="Raw sensor stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extended status stream rate to ground station" name="SR0_EXT_STAT" documentation="Extended status stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
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<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="RC Channel stream rate to ground station" name="SR0_RC_CHAN" documentation="RC Channel stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Raw Control stream rate to ground station" name="SR0_RAW_CTRL" documentation="Raw Control stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Position stream rate to ground station" name="SR0_POSITION" documentation="Position stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extra data type 1 stream rate to ground station" name="SR0_EXTRA1" documentation="Extra data type 1 stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extra data type 2 stream rate to ground station" name="SR0_EXTRA2" documentation="Extra data type 2 stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extra data type 3 stream rate to ground station" name="SR0_EXTRA3" documentation="Extra data type 3 stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Parameter stream rate to ground station" name="SR0_PARAMS" documentation="Parameter stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="ADSB stream rate to ground station" name="SR0_ADSB" documentation="ADSB stream rate to ground station" user="Advanced">
<field name="Range">0 50</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
</parameters>
<parameters name="SR1_">
<param humanName="Raw sensor stream rate" name="SR1_RAW_SENS" documentation="Raw sensor stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extended status stream rate to ground station" name="SR1_EXT_STAT" documentation="Extended status stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="RC Channel stream rate to ground station" name="SR1_RC_CHAN" documentation="RC Channel stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
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7840
</param>
<param humanName="Raw Control stream rate to ground station" name="SR1_RAW_CTRL" documentation="Raw Control stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Position stream rate to ground station" name="SR1_POSITION" documentation="Position stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extra data type 1 stream rate to ground station" name="SR1_EXTRA1" documentation="Extra data type 1 stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extra data type 2 stream rate to ground station" name="SR1_EXTRA2" documentation="Extra data type 2 stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extra data type 3 stream rate to ground station" name="SR1_EXTRA3" documentation="Extra data type 3 stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Parameter stream rate to ground station" name="SR1_PARAMS" documentation="Parameter stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="ADSB stream rate to ground station" name="SR1_ADSB" documentation="ADSB stream rate to ground station" user="Advanced">
<field name="Range">0 50</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
</parameters>
<parameters name="SR2_">
<param humanName="Raw sensor stream rate" name="SR2_RAW_SENS" documentation="Raw sensor stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extended status stream rate to ground station" name="SR2_EXT_STAT" documentation="Extended status stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="RC Channel stream rate to ground station" name="SR2_RC_CHAN" documentation="RC Channel stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Raw Control stream rate to ground station" name="SR2_RAW_CTRL" documentation="Raw Control stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Position stream rate to ground station" name="SR2_POSITION" documentation="Position stream rate to ground station" user="Advanced">
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<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extra data type 1 stream rate to ground station" name="SR2_EXTRA1" documentation="Extra data type 1 stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extra data type 2 stream rate to ground station" name="SR2_EXTRA2" documentation="Extra data type 2 stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extra data type 3 stream rate to ground station" name="SR2_EXTRA3" documentation="Extra data type 3 stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Parameter stream rate to ground station" name="SR2_PARAMS" documentation="Parameter stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="ADSB stream rate to ground station" name="SR2_ADSB" documentation="ADSB stream rate to ground station" user="Advanced">
<field name="Range">0 50</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
</parameters>
<parameters name="SR3_">
<param humanName="Raw sensor stream rate" name="SR3_RAW_SENS" documentation="Raw sensor stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extended status stream rate to ground station" name="SR3_EXT_STAT" documentation="Extended status stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="RC Channel stream rate to ground station" name="SR3_RC_CHAN" documentation="RC Channel stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Raw Control stream rate to ground station" name="SR3_RAW_CTRL" documentation="Raw Control stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Position stream rate to ground station" name="SR3_POSITION" documentation="Position stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extra data type 1 stream rate to ground station" name="SR3_EXTRA1" documentation="Extra data type 1 stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
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<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extra data type 2 stream rate to ground station" name="SR3_EXTRA2" documentation="Extra data type 2 stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Extra data type 3 stream rate to ground station" name="SR3_EXTRA3" documentation="Extra data type 3 stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="Parameter stream rate to ground station" name="SR3_PARAMS" documentation="Parameter stream rate to ground station" user="Advanced">
<field name="Range">0 10</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
<param humanName="ADSB stream rate to ground station" name="SR3_ADSB" documentation="ADSB stream rate to ground station" user="Advanced">
<field name="Range">0 50</field>
<field name="Increment">1</field>
<field name="Units">Hz</field>
<field name="UnitText">hertz</field>
</param>
</parameters>
<parameters name="STAT">
<param humanName="Boot Count" name="STAT_BOOTCNT" documentation="Number of times board has been booted" user="Standard">
<field name="ReadOnly">True</field>
</param>
<param humanName="Total FlightTime" name="STAT_FLTTIME" documentation="Total FlightTime (seconds)" user="Standard">
<field name="ReadOnly">True</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Total RunTime" name="STAT_RUNTIME" documentation="Total time autopilot has run" user="Standard">
<field name="ReadOnly">True</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Reset time" name="STAT_RESET" documentation="Seconds since January 1st 2016 (Unix epoch+1451606400) since reset (set to 0 to reset statistics)" user="Standard">
<field name="ReadOnly">True</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
</parameters>
<parameters name="STEER2SRV_">
<param humanName="Steering Time Constant" name="STEER2SRV_TCONST" documentation="This controls the time constant in seconds from demanded to achieved steering angle. A value of 0.75 is a good default and will work with nearly all rovers. Ground steering in aircraft needs a bit smaller time constant, and a value of 0.5 is recommended for best ground handling in fixed wing aircraft. A value of 0.75 means that the controller will try to correct any deviation between the desired and actual steering angle in 0.75 seconds. Advanced users may want to reduce this time to obtain a faster response but there is no point setting a time less than the vehicle can achieve." user="Advanced">
<field name="Range">0.4 1.0</field>
<field name="Increment">0.1</field>
<field name="Units">s</field>
<field name="UnitText">seconds</field>
</param>
<param humanName="Steering turning gain" name="STEER2SRV_P" documentation="The proportional gain for steering. This should be approximately equal to the diameter of the turning circle of the vehicle at low speed and maximum steering angle" user="User">
<field name="Range">0.1 10.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Integrator Gain" name="STEER2SRV_I" documentation="This is the gain from the integral of steering angle. Increasing this gain causes the controller to trim out steady offsets due to an out of trim vehicle." user="User">
<field name="Range">0 1.0</field>
<field name="Increment">0.05</field>
</param>
<param humanName="Damping Gain" name="STEER2SRV_D" documentation="This adjusts the damping of the steering control loop. This gain helps to reduce steering jitter with vibration. It should be increased in 0.01 increments as too high a value can lead to a high frequency steering oscillation that could overstress the vehicle." user="User">
<field name="Range">0 0.1</field>
<field name="Increment">0.01</field>
</param>
<param humanName="Integrator limit" name="STEER2SRV_IMAX" documentation="This limits the number of degrees of steering in centi-degrees over which the integrator will operate. At the default setting of 1500 centi-degrees, the integrator will be limited to +- 15 degrees of servo travel. The maximum servo deflection is +- 45 centi-degrees, so the default value represents a 1/3rd of the total control throw which is adequate unless the vehicle is severely out of trim." user="Advanced">
<field name="Range">0 4500</field>
<field name="Increment">1</field>
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<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
<param humanName="Minimum speed" name="STEER2SRV_MINSPD" documentation="This is the minimum assumed ground speed in meters/second for steering. Having a minimum speed prevents oscillations when the vehicle first starts moving. The vehicle can still drive slower than this limit, but the steering calculations will be done based on this minimum speed." user="User">
<field name="Range">0 5</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Steering feed forward" name="STEER2SRV_FF" documentation="The feed forward gain for steering this is the ratio of the achieved turn rate to applied steering. A value of 1 means that the vehicle would yaw at a rate of 45 degrees per second with full steering deflection at 1m/s ground speed." user="User">
<field name="Range">0.0 10.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Derating speed" name="STEER2SRV_DRTSPD" documentation="Speed after that the maximum degree of steering will start to derate. Set this speed to a maximum speed that a plane can do controlled turn at maximum angle of steering wheel without rolling to wing. If 0 then no derating is used." user="Advanced">
<field name="Range">0.0 30.0</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Derating factor" name="STEER2SRV_DRTFCT" documentation='Degrees of steering wheel to derate at each additional m/s of speed above "Derating speed". Should be set so that at higher speeds the plane does not roll to the wing in turns.' user="Advanced">
<field name="Range">0.0 50.0</field>
<field name="Increment">0.1</field>
<field name="Units">deg/m/s</field>
<field name="UnitText">degrees per meter per second</field>
</param>
<param humanName="Minimum angle of wheel" name="STEER2SRV_DRTMIN" documentation="The angle that limits smallest angle of steering wheel at maximum speed. Even if it should derate below, it will stop derating at this angle." user="Advanced">
<field name="Range">0.0 4500.0</field>
<field name="Increment">0.1</field>
<field name="Units">cdeg</field>
<field name="UnitText">centidegrees</field>
</param>
</parameters>
<parameters name="TECS_">
<param humanName="Maximum Climb Rate (metres/sec)" name="TECS_CLMB_MAX" documentation="This is the best climb rate that the aircraft can achieve with the throttle set to THR_MAX and the airspeed set to the default value. For electric aircraft make sure this number can be achieved towards the end of flight when the battery voltage has reduced. The setting of this parameter can be checked by commanding a positive altitude change of 100m in loiter, RTL or guided mode. If the throttle required to climb is close to THR_MAX and the aircraft is maintaining airspeed, then this parameter is set correctly. If the airspeed starts to reduce, then the parameter is set to high, and if the throttle demand require to climb and maintain speed is noticeably less than THR_MAX, then either CLMB_MAX should be increased or THR_MAX reduced." user="Standard">
<field name="Range">0.1 20.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Minimum Sink Rate (metres/sec)" name="TECS_SINK_MIN" documentation="This is the sink rate of the aircraft with the throttle set to THR_MIN and the same airspeed as used to measure CLMB_MAX." user="Standard">
<field name="Range">0.1 10.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Controller time constant (sec)" name="TECS_TIME_CONST" documentation="This is the time constant of the TECS control algorithm. Smaller values make it faster to respond, large values make it slower to respond." user="Advanced">
<field name="Range">3.0 10.0</field>
<field name="Increment">0.2</field>
</param>
<param humanName="Controller throttle damping" name="TECS_THR_DAMP" documentation="This is the damping gain for the throttle demand loop. Increase to add damping to correct for oscillations in speed and height." user="Advanced">
<field name="Range">0.1 1.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Controller integrator" name="TECS_INTEG_GAIN" documentation="This is the integrator gain on the control loop. Increase to increase the rate at which speed and height offsets are trimmed out" user="Advanced">
<field name="Range">0.0 0.5</field>
<field name="Increment">0.02</field>
</param>
<param humanName="Vertical Acceleration Limit (metres/sec^2)" name="TECS_VERT_ACC" documentation="This is the maximum vertical acceleration either up or down that the controller will use to correct speed or height errors." user="Advanced">
<field name="Range">1.0 10.0</field>
<field name="Increment">0.5</field>
</param>
<param humanName="Height complementary filter frequency (radians/sec)" name="TECS_HGT_OMEGA" documentation="This is the cross-over frequency of the complementary filter used to fuse vertical acceleration and baro alt to obtain an estimate of height rate and height." user="Advanced">
<field name="Range">1.0 5.0</field>
<field name="Increment">0.05</field>
</param>
<param humanName="Speed complementary filter frequency (radians/sec)" name="TECS_SPD_OMEGA" documentation="This is the cross-over frequency of the complementary filter used to fuse longitudinal acceleration and airspeed to obtain a lower noise and lag estimate of airspeed." user="Advanced">
<field name="Range">0.5 2.0</field>
<field name="Increment">0.05</field>
</param>
<param humanName="Bank angle compensation gain" name="TECS_RLL2THR" documentation="Increasing this gain turn increases the amount of throttle that will be used to compensate for the additional drag created by turning. Ideally this should be set to approximately 10 x the extra sink rate in m/s created by a 45 degree bank turn. Increase this gain if the aircraft initially loses energy in turns and reduce if the aircraft initially gains energy in turns. Efficient high aspect-ratio aircraft (eg powered sailplanes) can use a lower value, whereas inefficient low aspect-ratio models (eg delta wings) can use a higher value." user="Advanced">
<field name="Range">5.0 30.0</field>
<field name="Increment">1.0</field>
</param>
<param humanName="Weighting applied to speed control" name="TECS_SPDWEIGHT" documentation="This parameter adjusts the amount of weighting that the pitch control applies to speed vs height errors. Setting it to 0.0 will cause the pitch control to control height and ignore speed errors. This will normally improve height accuracy but give larger airspeed errors. Setting it to 2.0 will cause the pitch control loop to control speed and ignore height errors. This will normally reduce airsped errors, but give larger height errors.	A value of 1.0 gives a balanced response and is the default." user="Advanced">
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<field name="Range">0.0 2.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Controller pitch damping" name="TECS_PTCH_DAMP" documentation="This is the damping gain for the pitch demand loop. Increase to add damping to correct for oscillations in speed and height." user="Advanced">
<field name="Range">0.1 1.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Maximum Descent Rate (metres/sec)" name="TECS_SINK_MAX" documentation="This sets the maximum descent rate that the controller will use. If this value is too large, the aircraft will reach the pitch angle limit first and be unable to achieve the descent rate. This should be set to a value that can be achieved at the lower pitch angle limit." user="User">
<field name="Range">0.0 20.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Airspeed during landing approach (m/s)" name="TECS_LAND_ARSPD" documentation="When performing an autonomus landing, this value is used as the goal airspeed during approach. Note that this parameter is not useful if your platform does not have an airspeed sensor (use TECS_LAND_THR instead). If negative then this value is not used during landing." user="User">
<field name="Range">-1 127</field>
<field name="Increment">1</field>
</param>
<param humanName="Cruise throttle during landing approach (percentage)" name="TECS_LAND_THR" documentation="Use this parameter instead of LAND_ARSPD if your platform does not have an airspeed sensor. It is the cruise throttle during landing approach. If this value is negative then it is disabled and TECS_LAND_ARSPD is used instead." user="User">
<field name="Range">-1 100</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Weighting applied to speed control during landing." name="TECS_LAND_SPDWGT" documentation="Same as SPDWEIGHT parameter, with the exception that this parameter is applied during landing flight stages. A value closer to 2 will result in the plane ignoring height error during landing and our experience has been that the plane will therefore keep the nose up -- sometimes good for a glider landing (with the side effect that you will likely glide a ways past the landing point). A value closer to 0 results in the plane ignoring speed error -- use caution when lowering the value below 1 -- ignoring speed could result in a stall. Values between 0 and 2 are valid values for a fixed landing weight. When using -1 the weight will be scaled during the landing. At the start of the landing approach it starts with TECS_SPDWEIGHT and scales down to 0 by the time you reach the land point. Example: Halfway down the landing approach you'll effectively have a weight of TECS_SPDWEIGHT/2." user="Advanced">
<field name="Range">-1.0 2.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Maximum pitch in auto flight" name="TECS_PITCH_MAX" documentation="This controls maximum pitch up in automatic throttle modes. If this is set to zero then LIM_PITCH_MAX is used instead. The purpose of this parameter is to allow the use of a smaller pitch range when in automatic flight than what is used in FBWA mode." user="Advanced">
<field name="Range">0 45</field>
<field name="Increment">1</field>
</param>
<param humanName="Minimum pitch in auto flight" name="TECS_PITCH_MIN" documentation="This controls minimum pitch in automatic throttle modes. If this is set to zero then LIM_PITCH_MIN is used instead. The purpose of this parameter is to allow the use of a smaller pitch range when in automatic flight than what is used in FBWA mode. Note that TECS_PITCH_MIN should be a negative number." user="Advanced">
<field name="Range">-45 0</field>
<field name="Increment">1</field>
</param>
<param humanName="Sink rate for final landing stage" name="TECS_LAND_SINK" documentation="The sink rate in meters/second for the final stage of landing." user="Advanced">
<field name="Range">0.0 2.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Land controller time constant (sec)" name="TECS_LAND_TCONST" documentation="This is the time constant of the TECS control algorithm when in final landing stage of flight. It should be smaller than TECS_TIME_CONST to allow for faster flare" user="Advanced">
<field name="Range">1.0 5.0</field>
<field name="Increment">0.2</field>
</param>
<param humanName="Controller sink rate to pitch gain during flare" name="TECS_LAND_DAMP" documentation="This is the sink rate gain for the pitch demand loop when in final landing stage of flight. It should be larger than TECS_PTCH_DAMP to allow for better sink rate control during flare." user="Advanced">
<field name="Range">0.1 1.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Maximum pitch during final stage of landing" name="TECS_LAND_PMAX" documentation="This limits the pitch used during the final stage of automatic landing. During the final landing stage most planes need to keep their pitch small to avoid stalling. A maximum of 10 degrees is usually good. A value of zero means to use the normal pitch limits." user="Advanced">
<field name="Range">-5 40</field>
<field name="Increment">1</field>
</param>
<param humanName="Sink rate max for landing approach stage" name="TECS_APPR_SMAX" documentation="The sink rate max for the landing approach stage of landing. This will need to be large for steep landing approaches especially when using reverse thrust. If 0, then use TECS_SINK_MAX." user="Advanced">
<field name="Range">0.0 20.0</field>
<field name="Increment">0.1</field>
<field name="Units">m/s</field>
<field name="UnitText">meters per second</field>
</param>
<param humanName="Land sink rate change" name="TECS_LAND_SRC" documentation="When zero, the flare sink rate (TECS_LAND_SINK) is a fixed sink demand. With this enabled the flare sinkrate will increase/decrease the flare sink demand as you get further beyond the LAND waypoint. Has no effect before the waypoint. This value is added to TECS_LAND_SINK proportional to distance traveled after wp. With an increasing sink rate you can still land in a given distance if you're traveling too fast and cruise passed the land point. A positive value will force the plane to land sooner proportional to distance passed land point. A negative number will tell the plane to slowly climb allowing for a pitched-up stall landing. Recommend 0.2 as initial value." user="Advanced">
<field name="Range">-2.0 2.0</field>
<field name="Increment">0.1</field>
<field name="Units">m/s/m</field>
<field name="UnitText">meters per second per meter</field>
</param>
<param humanName="Controller throttle damping when landing" name="TECS_LAND_TDAMP" documentation="This is the damping gain for the throttle demand loop during and auto-landing. Same as TECS_THR_DAMP but only in effect during an auto-land. Increase to add damping to correct for oscillations in speed and height. When set to 0 landing throttle damp is controlled by TECS_THR_DAMP." user="Advanced">
<field name="Range">0.1 1.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Controller integrator during landing" name="TECS_LAND_IGAIN" documentation="This is the integrator gain on the control loop during landing. When set to 0 then TECS_INTEG_GAIN is used. Increase to increase the rate at which speed and height offsets are trimmed out. Typically values lower than TECS_INTEG_GAIN work best" user="Advanced">
<field name="Range">0.0 0.5</field>
<field name="Increment">0.02</field>
</param>
<param humanName="Controller integrator during takeoff" name="TECS_TKOFF_IGAIN" documentation="This is the integrator gain on the control loop during takeoff. When set to 0 then TECS_INTEG_GAIN is used. Increase to increase the rate at which speed and height offsets are trimmed out. Typically values higher than TECS_INTEG_GAIN work best" user="Advanced">
<field name="Range">0.0 0.5</field>
<field name="Increment">0.02</field>
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</param>
<param humanName="Pitch damping gain when landing" name="TECS_LAND_PDAMP" documentation="This is the damping gain for the pitch demand loop during landing. Increase to add damping to correct for oscillations in speed and height. If set to 0 then TECS_PTCH_DAMP will be used instead." user="Advanced">
<field name="Range">0.1 1.0</field>
<field name="Increment">0.1</field>
</param>
<param humanName="Enable the use of synthetic airspeed" name="TECS_SYNAIRSPEED" documentation="This enable the use of synthetic airspeed for aircraft that don't have a real airspeed sensor. This is useful for development testing where the user is aware of the considerable limitations of the synthetic airspeed system, such as very poor estimates when a wind estimate is not accurate. Do not enable this option unless you fully understand the limitations of a synthetic airspeed estimate." user="Advanced">
<values>
<value code="0">Disable</value>
<value code="1">Enable</value>
</values>
</param>
</parameters>
<parameters name="TERRAIN_">
<param humanName="Terrain data enable" name="TERRAIN_ENABLE" documentation="enable terrain data. This enables the vehicle storing a database of terrain data on the SD card. The terrain data is requested from the ground station as needed, and stored for later use on the SD card. To be useful the ground station must support TERRAIN_REQUEST messages and have access to a terrain database, such as the SRTM database." user="Advanced">
<values>
<value code="0">Disable</value>
<value code="1">Enable</value>
</values>
</param>
<param humanName="Terrain grid spacing" name="TERRAIN_SPACING" documentation="Distance between terrain grid points in meters. This controls the horizontal resolution of the terrain data that is stored on te SD card and requested from the ground station. If your GCS is using the worldwide SRTM database then a resolution of 100 meters is appropriate. Some parts of the world may have higher resolution data available, such as 30 meter data available in the SRTM database in the USA. The grid spacing also controls how much data is kept in memory during flight. A larger grid spacing will allow for a larger amount of data in memory. A grid spacing of 100 meters results in the vehicle keeping 12 grid squares in memory with each grid square having a size of 2.7 kilometers by 3.2 kilometers. Any additional grid squares are stored on the SD once they are fetched from the GCS and will be demand loaded as needed." user="Advanced">
<field name="Increment">1</field>
<field name="Units">m</field>
<field name="UnitText">meters</field>
</param>
</parameters>
<parameters name="TUNE_">
<param humanName="Transmitter tuning parameter or set of parameters" name="TUNE_PARAM" documentation="This sets which parameter or set of parameters will be tuned. Values greater than 100 indicate a set of parameters rather than a single parameter. Parameters less than 50 are for QuadPlane vertical lift motors only." user="Standard">
<values>
<value code="0">None</value>
<value code="1">RateRollPI</value>
<value code="2">RateRollP</value>
<value code="3">RateRollI</value>
<value code="4">RateRollD</value>
<value code="5">RatePitchPI</value>
<value code="6">RatePitchP</value>
<value code="7">RatePitchI</value>
<value code="8">RatePitchD</value>
<value code="9">RateYawPI</value>
<value code="10">RateYawP</value>
<value code="11">RateYawI</value>
<value code="12">RateYawD</value>
<value code="13">AngleRollP</value>
<value code="14">AnglePitchP</value>
<value code="15">AngleYawP</value>
<value code="16">PosXYP</value>
<value code="17">PosZP</value>
<value code="18">VelXYP</value>
<value code="19">VelXYI</value>
<value code="20">VelZP</value>
<value code="21">AccelZP</value>
<value code="22">AccelZI</value>
<value code="23">AccelZD</value>
<value code="50">FixedWingRollP</value>
<value code="51">FixedWingRollI</value>
<value code="52">FixedWingRollD</value>
<value code="53">FixedWingRollFF</value>
<value code="54">FixedWingPitchP</value>
<value code="55">FixedWingPitchI</value>
<value code="56">FixedWingPitchD</value>
<value code="57">FixedWingPitchFF</value>
<value code="101">Set_RateRollPitch</value>
<value code="102">Set_RateRoll</value>
<value code="103">Set_RatePitch</value>
<value code="104">Set_RateYaw</value>
<value code="105">Set_AngleRollPitch</value>
<value code="106">Set_VelXY</value>
<value code="107">Set_AccelZ</value>
</values>
</param>
<param humanName="Transmitter tuning channel" name="TUNE_CHAN" documentation="This sets the channel for transmitter tuning. This should be connected to a knob or slider on your transmitter. It needs to be setup to use the PWM range given by TUNE_CHAN_MIN to TUNE_CHAN_MAX" user="Standard">
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<values>
<value code="0">Disable</value>
<value code="5">Chan5</value>
<value code="6">Chan6</value>
<value code="7">Chan7</value>
<value code="8">Chan8</value>
<value code="9">Chan9</value>
<value code="10">Chan10</value>
<value code="11">Chan11</value>
<value code="12">Chan12</value>
<value code="13">Chan13</value>
<value code="14">Chan14</value>
<value code="15">Chan15</value>
<value code="16">Chan16</value>
</values>
</param>
<param humanName="Transmitter tuning channel minimum pwm" name="TUNE_CHAN_MIN" documentation="This sets the PWM lower limit for the tuning channel" user="Standard">
<field name="Range">900 2100</field>
</param>
<param humanName="Transmitter tuning channel maximum pwm" name="TUNE_CHAN_MAX" documentation="This sets the PWM upper limit for the tuning channel" user="Standard">
<field name="Range">900 2100</field>
</param>
<param humanName="Transmitter tuning selector channel" name="TUNE_SELECTOR" documentation="This sets the channel for the transmitter tuning selector switch. This should be a 2 position switch, preferably spring loaded. A PWM above 1700 means high, below 1300 means low. If no selector is set then you won't be able to switch between parameters during flight or re-center the tuning knob" user="Standard">
<values>
<value code="0">Disable</value>
<value code="1">Chan1</value>
<value code="2">Chan3</value>
<value code="3">Chan3</value>
<value code="4">Chan4</value>
<value code="5">Chan5</value>
<value code="6">Chan6</value>
<value code="7">Chan7</value>
<value code="8">Chan8</value>
<value code="9">Chan9</value>
<value code="10">Chan10</value>
<value code="11">Chan11</value>
<value code="12">Chan12</value>
<value code="13">Chan13</value>
<value code="14">Chan14</value>
<value code="15">Chan15</value>
<value code="16">Chan16</value>
</values>
</param>
<param humanName="Transmitter tuning range" name="TUNE_RANGE" documentation="This sets the range over which tuning will change a parameter. A value of 2 means the tuning parameter will go from 0.5 times the start value to 2x the start value over the range of the tuning channel" user="Standard">
</param>
<param humanName="Revert on mode change" name="TUNE_MODE_REVERT" documentation="This controls whether tuning values will revert on a flight mode change." user="Standard">
<values>
<value code="0">Disable</value>
<value code="1">Enable</value>
</values>
</param>
<param humanName="Controller error threshold" name="TUNE_ERR_THRESH" documentation="This sets the controller error threshold above which an alarm will sound and a message will be sent to the GCS to warn of controller instability" user="Standard">
<field name="Range">0 1</field>
</param>
</parameters>
<parameters name="YAW2SRV_">
<param humanName="Sideslip control gain" name="YAW2SRV_SLIP" documentation="This is the gain from measured lateral acceleration to demanded yaw rate. It should be set to zero unless active control of sideslip is desired. This will only work effectively if there is enough fuselage side area to generate a measureable lateral acceleration when the model sideslips. Flying wings and most gliders cannot use this term. This term should only be adjusted after the basic yaw damper gain YAW2SRV_DAMP is tuned and the YAW2SRV_INT integrator gain has been set. Set this gain to zero if only yaw damping is required." user="Advanced">
<field name="Range">0 4</field>
<field name="Increment">0.25</field>
</param>
<param humanName="Sideslip control integrator" name="YAW2SRV_INT" documentation="This is the integral gain from lateral acceleration error. This gain should only be non-zero if active control over sideslip is desired. If active control over sideslip is required then this can be set to 1.0 as a first try." user="Advanced">
<field name="Range">0 2</field>
<field name="Increment">0.25</field>
</param>
<param humanName="Yaw damping" name="YAW2SRV_DAMP" documentation="This is the gain from yaw rate to rudder. It acts as a damper on yaw motion. If a basic yaw damper is required, this gain term can be incremented, whilst leaving the YAW2SRV_SLIP and YAW2SRV_INT gains at zero. Note that unlike with a standard PID controller, if this damping term is zero then the integrator will also be disabled." user="Advanced">
<field name="Range">0 2</field>
<field name="Increment">0.25</field>
</param>
<param humanName="Yaw coordination gain" name="YAW2SRV_RLL" documentation="This is the gain term that is applied to the yaw rate offset calculated as required to keep the yaw rate consistent with the turn rate for a coordinated turn. The default value is 1 which will work for all models. Advanced users can use it to correct for any tendency to yaw away from or into the turn once the turn is established. Increase to make the model yaw more initially and decrease to make the model yaw less initially. If values greater than 1.1 or less than 0.9 are required then it normally indicates a problem with the airspeed calibration." user="Advanced">
<field name="Range">0.8 1.2</field>
<field name="Increment">0.05</field>
</param>
<param humanName="Integrator limit" name="YAW2SRV_IMAX" documentation="This limits the number of centi-degrees of rudder over which the integrator will operate. At the default setting of 1500 centi-degrees, the integrator will be limited to +- 15 degrees of servo travel. The maximum servo deflection is +- 45 degrees, so the default value represents a 1/3rd of the total control throw which is adequate for most aircraft unless they are severely out of trim or have very limited rudder control effectiveness." user="Advanced">
<field name="Range">0 4500</field>
<field name="Increment">1</field>
</param>
</parameters>
</libraries></paramfile>