<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">
<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>Set bits to 1 to enable checks. Checks enabled by the following bit positions 0 : Minimum required sat count set by EKF2_REQ_NSATS 1 : Minimum required GDoP set by EKF2_REQ_GDOP 2 : Maximum allowed horizontal position error set by EKF2_REQ_EPH 3 : Maximum allowed vertical position error set by EKF2_REQ_EPV 4 : Maximum allowed speed error set by EKF2_REQ_SACC 5 : Maximum allowed horizontal position rate set by EKF2_REQ_HDRIFT. This check can only be used if the vehciel is stationary during alignment. 6 : Maximum allowed vertical position rate set by EKF2_REQ_VDRIFT. This check can only be used if the vehciel is stationary during alignment. 7 : Maximum allowed horizontal speed set by EKF2_REQ_HDRIFT. This check can only be used if the vehciel is stationary during alignment. 8 : Maximum allowed vertical velocity discrepancy set by EKF2_REQ_VDRIFT</long_desc>
<long_desc>Set bits to 1 to enable checks. Checks enabled by the following bit positions 0 : Minimum required sat count set by EKF2_REQ_NSATS 1 : Minimum required GDoP set by EKF2_REQ_GDOP 2 : Maximum allowed horizontal position error set by EKF2_REQ_EPH 3 : Maximum allowed vertical position error set by EKF2_REQ_EPV 4 : Maximum allowed speed error set by EKF2_REQ_SACC 5 : Maximum allowed horizontal position rate set by EKF2_REQ_HDRIFT. This check can only be used if the vehicle is stationary during alignment. 6 : Maximum allowed vertical position rate set by EKF2_REQ_VDRIFT. This check can only be used if the vehicle is stationary during alignment. 7 : Maximum allowed horizontal speed set by EKF2_REQ_HDRIFT. This check can only be used if the vehicle is stationary during alignment. 8 : Maximum allowed vertical velocity discrepancy set by EKF2_REQ_VDRIFT</long_desc>
<min>0</min>
<min>0</min>
<max>511</max>
<max>511</max>
<scope>modules/ekf2</scope>
<scope>modules/ekf2</scope>
<bitmask>
<bitindex="0">Min sat count (EKF2_REQ_NSATS)</bit>
<bitindex="1">Min GDoP (EKF2_REQ_GDOP)</bit>
<bitindex="2">Max horizontal position error (EKF2_REQ_EPH)</bit>
<bitindex="3">Max vertical position error (EKF2_REQ_EPV)</bit>
<short_desc>Integer bitmask controlling handling of magnetic declination</short_desc>
<short_desc>Integer bitmask controlling handling of magnetic declination</short_desc>
<long_desc>Set bits in the following positions to enable functions. 0 : Set to true to use the declination from the geo_lookup library when the GPS position becomes available, set to false to always use the EKF2_MAG_DECL value. 1 : Set to true to save the EKF2_MAG_DECL parameter to the value returned by the EKF when the vehicle disarms. 2 : Set to true to always use the declination as an observaton when 3-axis magnetometer fusion is being used.</long_desc>
<long_desc>Set bits in the following positions to enable functions. 0 : Set to true to use the declination from the geo_lookup library when the GPS position becomes available, set to false to always use the EKF2_MAG_DECL value. 1 : Set to true to save the EKF2_MAG_DECL parameter to the value returned by the EKF when the vehicle disarms. 2 : Set to true to always use the declination as an observation when 3-axis magnetometer fusion is being used.</long_desc>
<min>0</min>
<min>0</min>
<max>7</max>
<max>7</max>
<scope>modules/ekf2</scope>
<scope>modules/ekf2</scope>
<bitmask>
<bitindex="0">use geo_lookup declination</bit>
<bitindex="1">save EKF2_MAG_DECL on disarm</bit>
<bitindex="2">use declination as an observation</bit>
<short_desc>Integer bitmask controlling data fusion and aiding methods</short_desc>
<short_desc>Integer bitmask controlling data fusion and aiding methods</short_desc>
<long_desc>Set bits in the following positions to enable: 0 : Set to true to use GPS data if available 1 : Set to true to use optical flow data if available 2 : Set to true to inhibit IMU bias estimation 3 : Set to true to enable vision position fusion 4 : Set to true to enable vision yaw fusion *</long_desc>
<long_desc>Set bits in the following positions to enable: 0 : Set to true to use GPS data if available 1 : Set to true to use optical flow data if available 2 : Set to true to inhibit IMU bias estimation 3 : Set to true to enable vision position fusion 4 : Set to true to enable vision yaw fusion</long_desc>
<long_desc>Data sheet sqrt(Noise power) = 150ug/sqrt(Hz) std dev = (150*9.8*1e-6)*sqrt(1000 Hz) m/s^2 Since accels sampled at 1000 Hz. should be 0.0464</long_desc>
<long_desc>Data sheet noise density = 150ug/sqrt(Hz) = 0.0015 m/s^2/sqrt(Hz) Larger than data sheet to account for tilt error.</long_desc>
<short_desc>Set data link loss failsafe mode</short_desc>
<long_desc>The data link loss failsafe will only be entered after a timeout, set by COM_DL_LOSS_T in seconds. Once the timeout occurs the selected action will be executed. Setting this parameter to 4 will enable CASA Outback Challenge rules, which are only recommended to participants of that competition.</long_desc>
<short_desc>Set RC loss failsafe mode</short_desc>
<long_desc>The RC loss failsafe will only be entered after a timeout, set by COM_RC_LOSS_T in seconds. If RC input checks have been disabled by setting the COM_RC_IN_MODE param it will not be triggered. Setting this parameter to 4 will enable CASA Outback Challenge rules, which are only recommended to participants of that competition.</long_desc>
<short_desc>Set data link loss failsafe mode</short_desc>
<long_desc>The data link loss failsafe will only be entered after a timeout, set by COM_DL_LOSS_T in seconds. Once the timeout occurs the selected action will be executed. Setting this parameter to 4 will enable CASA Outback Challenge rules, which are only recommended to participants of that competition.</long_desc>
<short_desc>Set RC loss failsafe mode</short_desc>
<long_desc>The RC loss failsafe will only be entered after a timeout, set by COM_RC_LOSS_T in seconds. If RC input checks have been disabled by setting the COM_RC_IN_MODE param it will not be triggered. Setting this parameter to 4 will enable CASA Outback Challenge rules, which are only recommended to participants of that competition.</long_desc>
<short_desc>Invert direction of aux output channel 1</short_desc>
<short_desc>Set the minimum PWM for the MAIN outputs</short_desc>
<long_desc>Set to 1 to invert the channel, 0 for default direction.</long_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>Invert direction of aux output channel 2</short_desc>
<short_desc>Set the maximum PWM for the MAIN outputs</short_desc>
<long_desc>Set to 1 to invert the channel, 0 for default direction.</long_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>Invert direction of aux output channel 3</short_desc>
<short_desc>Set the disarmed PWM for MAIN outputs</short_desc>
<long_desc>Set to 1 to invert the channel, 0 for default direction.</long_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>Invert direction of aux output channel 4</short_desc>
<short_desc>Set the minimum PWM for the MAIN outputs</short_desc>
<long_desc>Set to 1 to invert the channel, 0 for default direction.</long_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>Invert direction of aux output channel 5</short_desc>
<short_desc>Set the maximum PWM for the MAIN outputs</short_desc>
<long_desc>Set to 1 to invert the channel, 0 for default direction.</long_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>Invert direction of aux output channel 6</short_desc>
<short_desc>Set the disarmed PWM for AUX outputs</short_desc>
<long_desc>Set to 1 to invert the channel, 0 for default direction.</long_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>
<short_desc>Invert direction of aux output channel 1</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>
<long_desc>Set to 1 to invert the channel, 0 for default direction.</long_desc>
<short_desc>Set the maximum PWM for the MAIN outputs</short_desc>
<short_desc>Invert direction of aux output channel 2</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>
<long_desc>Set to 1 to invert the channel, 0 for default direction.</long_desc>
<short_desc>Set the disarmed PWM for MAIN outputs</short_desc>
<short_desc>Invert direction of aux output channel 3</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>Set to 1 to invert the channel, 0 for default direction.</long_desc>
<short_desc>Set the minimum PWM for the MAIN outputs</short_desc>
<short_desc>Invert direction of aux output channel 4</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>
<long_desc>Set to 1 to invert the channel, 0 for default direction.</long_desc>
<short_desc>Set the maximum PWM for the MAIN outputs</short_desc>
<short_desc>Invert direction of aux output channel 5</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>
<long_desc>Set to 1 to invert the channel, 0 for default direction.</long_desc>
<short_desc>Set the disarmed PWM for AUX outputs</short_desc>
<short_desc>Invert direction of aux output channel 6</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>Set to 1 to invert the channel, 0 for default direction.</long_desc>
<min>0</min>
<boolean/>
<max>2200</max>
<unit>us</unit>
<reboot_required>true</reboot_required>
<reboot_required>true</reboot_required>
<scope>modules/sensors</scope>
<scope>drivers/px4fmu</scope>
</parameter>
</parameter>
</group>
</group>
<groupname="Payload drop">
<groupname="Payload drop">
...
@@ -4162,33 +4198,6 @@ but also ignore less noise</short_desc>
...
@@ -4162,33 +4198,6 @@ but also ignore less noise</short_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>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>Minimum altitude for fixed wing flight, when in fixed wing the altitude drops below this altitude the vehicle will transition back to MC mode and enter failsafe RTL</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>Minimum altitude for fixed wing flight, when in fixed wing the altitude drops below this altitude the vehicle will transition back to MC mode and enter failsafe RTL</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>
