<airframeid="20000"maintainer="Julian Oes <julian@oes.ch> This startup can be used on Pixhawk/Pixfalcon/Pixracer for the passthrough of RC input and PWM output."name="Passthrough mode for Snapdragon">
<long_desc>Selects which pin is used, ranges from 1 to 6 (AUX1-AUX6 on px4fmu-v2 and the rail pins on px4fmu-v4). The PWM interface takes two pins per camera, while relay triggers on every pin individually. Example: Value 34 would trigger on pins 3 and 4.</long_desc>
<long_desc>Selects which pin is used, ranges from 1 to 6 (AUX1-AUX6 on px4fmu-v2 and the rail pins on px4fmu-v4). The PWM interface takes two pins per camera, while relay triggers on every pin individually. Example: Value 56 would trigger on pins 5 and 6.</long_desc>
<short_desc>Time-out for auto disarm after landing</short_desc>
<long_desc>A non-zero, positive value specifies the time-out period in seconds after which the vehicle will be automatically disarmed in case a landing situation has been detected during this period. A value of zero means that automatic disarming is disabled.</long_desc>
<long_desc>A non-zero, positive value specifies the time-out period in seconds after which the vehicle will be automatically disarmed in case a landing situation has been detected during this period. The vehicle will also auto-disarm right after arming if it has not even flown, however the time will be longer by a factor of 5. A value of zero means that automatic disarming is disabled.</long_desc>
<min>0</min>
<max>20</max>
<unit>s</unit>
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@@ -689,6 +689,31 @@ See COM_OBL_ACT and COM_OBL_RC_ACT to configure action</short_desc>
<short_desc>Auxiliary switch to set mount operation mode</short_desc>
<long_desc>Set to 0 to disable manual mode control. If set to an auxiliary switch: Switch off means the gimbal is put into safe/locked position. Switch on means the gimbal can move freely, and landing gear will be retracted if applicable.</long_desc>
<short_desc>Slope for Throttle PID Attenuation (TPA)</short_desc>
<long_desc>Rate at which to attenuate roll/pitch P gain Attenuation factor is 1.0 when throttle magnitude is below the setpoint Above the setpoint, the attenuation factor is (1 - slope*(abs(throttle)-breakpoint))</long_desc>
<long_desc>Feed forward weight for altitude control in stabilized modes (ALTCTRL). 0 will give slow responce and no overshot, 1 - fast responce and big overshot.</long_desc>
<short_desc>Differential gain for horizontal velocity error. Small values help reduce fast oscillations. If value is too big oscillations will appear again</short_desc>
<long_desc>Feed forward weight for position control in position control mode (POSCTRL). 0 will give slow responce and no overshot, 1 - fast responce and big overshot.</long_desc>
<long_desc>Feed forward weight for altitude control in stabilized modes (ALTCTRL). 0 will give slow responce and no overshot, 1 - fast responce and big overshot.</long_desc>
<short_desc>Differential gain for horizontal velocity error. Small values help reduce fast oscillations. If value is too big oscillations will appear again</short_desc>
<long_desc>Feed forward weight for position control in position control mode (POSCTRL). 0 will give slow responce and no overshot, 1 - fast responce and big overshot.</long_desc>
<short_desc>Set the minimum PWM for the MAIN outputs</short_desc>
<long_desc>IMPORTANT: CHANGING THIS PARAMETER REQUIRES A COMPLETE SYSTEM REBOOT IN ORDER TO APPLY THE CHANGES. COMPLETELY POWER-CYCLE THE SYSTEM TO PUT CHANGES INTO EFFECT. Set to 1000 for industry default or 900 to increase servo travel.</long_desc>
<short_desc>Set the maximum PWM for the MAIN outputs</short_desc>
<long_desc>IMPORTANT: CHANGING THIS PARAMETER REQUIRES A COMPLETE SYSTEM REBOOT IN ORDER TO APPLY THE CHANGES. COMPLETELY POWER-CYCLE THE SYSTEM TO PUT CHANGES INTO EFFECT. Set to 2000 for industry default or 2100 to increase servo travel.</long_desc>
<short_desc>Set the disarmed PWM for MAIN outputs</short_desc>
<long_desc>IMPORTANT: CHANGING THIS PARAMETER REQUIRES A COMPLETE SYSTEM REBOOT IN ORDER TO APPLY THE CHANGES. COMPLETELY POWER-CYCLE THE SYSTEM TO PUT CHANGES INTO EFFECT. This is the PWM pulse the autopilot is outputting if not armed. The main use of this parameter is to silence ESCs when they are disarmed.</long_desc>
<short_desc>Set the minimum PWM for the MAIN outputs</short_desc>
<long_desc>IMPORTANT: CHANGING THIS PARAMETER REQUIRES A COMPLETE SYSTEM REBOOT IN ORDER TO APPLY THE CHANGES. COMPLETELY POWER-CYCLE THE SYSTEM TO PUT CHANGES INTO EFFECT. Set to 1000 for default or 900 to increase servo travel</long_desc>
<short_desc>Set the maximum PWM for the MAIN outputs</short_desc>
<long_desc>IMPORTANT: CHANGING THIS PARAMETER REQUIRES A COMPLETE SYSTEM REBOOT IN ORDER TO APPLY THE CHANGES. COMPLETELY POWER-CYCLE THE SYSTEM TO PUT CHANGES INTO EFFECT. Set to 2000 for default or 2100 to increase servo travel</long_desc>
<short_desc>Set the disarmed PWM for AUX outputs</short_desc>
<long_desc>IMPORTANT: CHANGING THIS PARAMETER REQUIRES A COMPLETE SYSTEM REBOOT IN ORDER TO APPLY THE CHANGES. COMPLETELY POWER-CYCLE THE SYSTEM TO PUT CHANGES INTO EFFECT. This is the PWM pulse the autopilot is outputting if not armed. The main use of this parameter is to silence ESCs when they are disarmed.</long_desc>
<short_desc>Minimum motor rise time (slew rate limit)</short_desc>
<long_desc>Minimum time allowed for the motor input signal to pass through a range of 1000 PWM units. A value x means that the motor signal can only go from 1000 to 2000 PWM in maximum x seconds. Zero means that slew rate limiting is disabled.</long_desc>
<short_desc>Set the minimum PWM for the MAIN outputs</short_desc>
<long_desc>IMPORTANT: CHANGING THIS PARAMETER REQUIRES A COMPLETE SYSTEM REBOOT IN ORDER TO APPLY THE CHANGES. COMPLETELY POWER-CYCLE THE SYSTEM TO PUT CHANGES INTO EFFECT. Set to 1000 for industry default or 900 to increase servo travel.</long_desc>
<short_desc>Set the maximum PWM for the MAIN outputs</short_desc>
<long_desc>IMPORTANT: CHANGING THIS PARAMETER REQUIRES A COMPLETE SYSTEM REBOOT IN ORDER TO APPLY THE CHANGES. COMPLETELY POWER-CYCLE THE SYSTEM TO PUT CHANGES INTO EFFECT. Set to 2000 for industry default or 2100 to increase servo travel.</long_desc>
<short_desc>Set the disarmed PWM for MAIN outputs</short_desc>
<long_desc>IMPORTANT: CHANGING THIS PARAMETER REQUIRES A COMPLETE SYSTEM REBOOT IN ORDER TO APPLY THE CHANGES. COMPLETELY POWER-CYCLE THE SYSTEM TO PUT CHANGES INTO EFFECT. This is the PWM pulse the autopilot is outputting if not armed. The main use of this parameter is to silence ESCs when they are disarmed.</long_desc>
<short_desc>Set the minimum PWM for the MAIN outputs</short_desc>
<long_desc>IMPORTANT: CHANGING THIS PARAMETER REQUIRES A COMPLETE SYSTEM REBOOT IN ORDER TO APPLY THE CHANGES. COMPLETELY POWER-CYCLE THE SYSTEM TO PUT CHANGES INTO EFFECT. Set to 1000 for default or 900 to increase servo travel</long_desc>
<short_desc>Set the maximum PWM for the MAIN outputs</short_desc>
<long_desc>IMPORTANT: CHANGING THIS PARAMETER REQUIRES A COMPLETE SYSTEM REBOOT IN ORDER TO APPLY THE CHANGES. COMPLETELY POWER-CYCLE THE SYSTEM TO PUT CHANGES INTO EFFECT. Set to 2000 for default or 2100 to increase servo travel</long_desc>
<short_desc>Set the disarmed PWM for AUX outputs</short_desc>
<long_desc>IMPORTANT: CHANGING THIS PARAMETER REQUIRES A COMPLETE SYSTEM REBOOT IN ORDER TO APPLY THE CHANGES. COMPLETELY POWER-CYCLE THE SYSTEM TO PUT CHANGES INTO EFFECT. This is the PWM pulse the autopilot is outputting if not armed. The main use of this parameter is to silence ESCs when they are disarmed.</long_desc>
<long_desc>The trim value is the actuator control value the system needs for straight and level flight. It can be calibrated by flying manually straight and level using the RC trims and copying them using the GCS.</long_desc>
<long_desc>The trim value is the actuator control value the system needs for straight and level flight. It can be calibrated by flying manually straight and level using the RC trims and copying them using the GCS.</long_desc>
<long_desc>The trim value is the actuator control value the system needs for straight and level flight. It can be calibrated by flying manually straight and level using the RC trims and copying them using the GCS.</long_desc>
<long_desc>The trim value is the actuator control value the system needs for straight and level flight. It can be calibrated by flying manually straight and level using the RC trims and copying them using the GCS.</long_desc>
<long_desc>The trim value is the actuator control value the system needs for straight and level flight. It can be calibrated by flying manually straight and level using the RC trims and copying them using the GCS.</long_desc>
<long_desc>The trim value is the actuator control value the system needs for straight and level flight. It can be calibrated by flying manually straight and level using the RC trims and copying them using the GCS.</long_desc>
<short_desc>Threshold for selecting assist mode</short_desc>
<long_desc>0-1 indicate where in the full channel range the threshold sits 0 : min 1 : max sign indicates polarity of comparison positive : true when channel>th negative : true when channel<th</long_desc>
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@@ -5771,6 +5943,13 @@ EPV used if greater than this value</short_desc>
<short_desc>Threshold for the landing gear switch</short_desc>
<long_desc>0-1 indicate where in the full channel range the threshold sits 0 : min 1 : max sign indicates polarity of comparison positive : true when channel>th negative : true when channel<th</long_desc>
<long_desc>the difference in hours and minutes from Coordinated Universal Time (UTC) for a your place and date. for example, In case of South Korea(UTC+09:00), UTC offset is 540 min (9*60) refer to https://en.wikipedia.org/wiki/List_of_UTC_time_offsets</long_desc>
<long_desc>A value of -1 indicates the commandline argument should be obeyed. A value of 0 sets the minimum rate, any other value is interpreted as rate in Hertz. This parameter is only read out before logging starts (which commonly is before arming).</long_desc>
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@@ -5948,6 +6119,14 @@ This is used for gathering replay logs for the ekf2 module</short_desc>
<long_desc>the difference in hours and minutes from Coordinated Universal Time (UTC) for a your place and date. for example, In case of South Korea(UTC+09:00), UTC offset is 540 min (9*60) refer to https://en.wikipedia.org/wiki/List_of_UTC_time_offsets</long_desc>
<short_desc>Fixed wing thrust scale for hover forward flight</short_desc>
<long_desc>Scale applied to fixed wing thrust being used as source for forward acceleration in multirotor mode. This technique can be used to avoid the plane having to pitch down a lot in order to move forward. Setting this value to 0 (default) will disable this strategy.</long_desc>
<short_desc>Duration of front transition phase 2</short_desc>
<long_desc>Time in seconds it should take for the rotors to rotate forward completely from the point when the plane has picked up enough airspeed and is ready to go into fixed wind mode.</long_desc>
<short_desc>Duration of front transition phase 2</short_desc>
<long_desc>Time in seconds it should take for the rotors to rotate forward completely from the point when the plane has picked up enough airspeed and is ready to go into fixed wind mode.</long_desc>
<short_desc>Fixed wing thrust scale for hover forward flight</short_desc>
<long_desc>Scale applied to fixed wing thrust being used as source for forward acceleration in multirotor mode. This technique can be used to avoid the plane having to pitch down a lot in order to move forward. Setting this value to 0 (default) will disable this strategy.</long_desc>
<long_desc>The RC mapping index indicates which channel is used for failsafe If 0, whichever channel is mapped to throttle is used otherwise the value indicates the specific rc channel to use</long_desc>
<long_desc>The RC mapping index indicates which channel is used for failsafe If 0, whichever channel is mapped to throttle is used otherwise the value indicates the specific rc channel to use</long_desc>
