From d34bf83d8e3341f13b8dad90275a100bbde86ef1 Mon Sep 17 00:00:00 2001 From: PX4 Jenkins Date: Wed, 1 Nov 2017 04:37:17 +0000 Subject: [PATCH] Update PX4 Firmware metadata Wed Nov 1 04:37:17 UTC 2017 --- .../PX4/PX4ParameterFactMetaData.xml | 1988 ++++++++++---------- 1 file changed, 994 insertions(+), 994 deletions(-) diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml index cc1d918..98b1329 100644 --- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml +++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml @@ -998,6 +998,31 @@ See COM_OBL_ACT and COM_OBL_RC_ACT to configure action + + Airfield home Lat + Latitude of airfield home waypoint + -900000000 + 900000000 + deg * 1e7 + modules/navigator + + + Airfield home Lon + Longitude of airfield home waypoint + -1800000000 + 1800000000 + deg * 1e7 + modules/navigator + + + Airfield home alt + Altitude of airfield home waypoint + -50 + m + 1 + 0.5 + modules/navigator + Comms hold wait time The amount of time in seconds the system should wait at the comms hold waypoint @@ -1057,31 +1082,6 @@ See COM_OBL_ACT and COM_OBL_RC_ACT to configure action modules/navigator - - Airfield home Lat - Latitude of airfield home waypoint - -900000000 - 900000000 - deg * 1e7 - modules/navigator - - - Airfield home Lon - Longitude of airfield home waypoint - -1800000000 - 1800000000 - deg * 1e7 - modules/navigator - - - Airfield home alt - Altitude of airfield home waypoint - -50 - m - 1 - 0.5 - modules/navigator - @@ -1912,16 +1912,6 @@ This parameter controls the time constant of the decay - - Attitude Wheel Time Constant - This defines the latency between a steering step input and the achieved setpoint (inverse to a P gain). Half a second is a good start value and fits for most average systems. Smaller systems may require smaller values, but as this will wear out servos faster, the value should only be decreased as needed. - 0.4 - 1.0 - s - 2 - 0.05 - modules/gnd_att_control - Attitude Roll Time Constant This defines the latency between a roll step input and the achieved setpoint (inverse to a P gain). Half a second is a good start value and fits for most average systems. Smaller systems may require smaller values, but as this will wear out servos faster, the value should only be decreased as needed. @@ -2313,6 +2303,16 @@ This parameter controls the time constant of the decay 0.01 modules/fw_att_control + + Attitude Wheel Time Constant + This defines the latency between a steering step input and the achieved setpoint (inverse to a P gain). Half a second is a good start value and fits for most average systems. Smaller systems may require smaller values, but as this will wear out servos faster, the value should only be decreased as needed. + 0.4 + 1.0 + s + 2 + 0.05 + modules/gnd_att_control + @@ -3651,111 +3651,6 @@ by initializing the estimator to the LPE_LAT/LON parameters when global informat - - Set offboard loss failsafe mode - The offboard loss failsafe will only be entered after a timeout, set by COM_OF_LOSS_T in seconds. - modules/commander - - Loiter - Land at current position - Return to Land - - - - Set offboard loss failsafe mode when RC is available - The offboard loss failsafe will only be entered after a timeout, set by COM_OF_LOSS_T in seconds. - modules/commander - - Altitude control - Position control - Return to Land - Manual - Loiter - Land at current position - - - - Position control navigation loss response - This sets the flight mode that will be used if navigation accuracy is no longer adequte for position control. Navigation accuracy checks can be disabled using the CBRK_VELPOSERR parameter, but doing so will remove protection for all flight modes. - modules/commander - - Assume no use of remote control after fallback. Switch to DESCEND if a height estimate is available, else switch to TERMINATION. - Assume use of remote control after fallback. Switch to ALTCTL if a height estimate is available, else switch to MANUAL. - - - - Loiter radius (FW only) - Default value of loiter radius for missions, loiter, RTL, etc. (fixedwing only). - 25 - 1000 - m - 1 - 0.5 - modules/navigator - - - Acceptance Radius - Default acceptance radius, overridden by acceptance radius of waypoint if set. For fixed wing the L1 turning distance is used for horizontal acceptance. - 0.05 - 200.0 - m - 1 - 0.5 - modules/navigator - - - FW Altitude Acceptance Radius - Acceptance radius for fixedwing altitude. - 0.05 - 200.0 - m - 1 - 0.5 - modules/navigator - - - MC Altitude Acceptance Radius - Acceptance radius for multicopter altitude. - 0.05 - 200.0 - m - 1 - 0.5 - modules/navigator - - - Set data link loss failsafe mode - 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. - modules/navigator - - Loiter - Disabled - Land at current position - Return to Land - Terminate - Data Link Auto Recovery (CASA Outback Challenge rules) - Lockdown - - - - Set RC loss failsafe mode - 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. - modules/navigator - - Loiter - Disabled - Land at current position - Return to Land - Terminate - RC Auto Recovery (CASA Outback Challenge rules) - Lockdown - - - - Force VTOL mode takeoff and land - - modules/navigator - Take-off altitude This is the minimum altitude the system will take off to. @@ -3846,6 +3741,79 @@ by initializing the estimator to the LPE_LAT/LON parameters when global informat 1 modules/navigator + + Loiter radius (FW only) + Default value of loiter radius for missions, loiter, RTL, etc. (fixedwing only). + 25 + 1000 + m + 1 + 0.5 + modules/navigator + + + Acceptance Radius + Default acceptance radius, overridden by acceptance radius of waypoint if set. For fixed wing the L1 turning distance is used for horizontal acceptance. + 0.05 + 200.0 + m + 1 + 0.5 + modules/navigator + + + FW Altitude Acceptance Radius + Acceptance radius for fixedwing altitude. + 0.05 + 200.0 + m + 1 + 0.5 + modules/navigator + + + MC Altitude Acceptance Radius + Acceptance radius for multicopter altitude. + 0.05 + 200.0 + m + 1 + 0.5 + modules/navigator + + + Set data link loss failsafe mode + 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. + modules/navigator + + Loiter + Disabled + Land at current position + Return to Land + Terminate + Data Link Auto Recovery (CASA Outback Challenge rules) + Lockdown + + + + Set RC loss failsafe mode + 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. + modules/navigator + + Loiter + Disabled + Land at current position + Return to Land + Terminate + RC Auto Recovery (CASA Outback Challenge rules) + Lockdown + + + + Force VTOL mode takeoff and land + + modules/navigator + Enable weather-vane mode takeoff for missions @@ -3861,14 +3829,46 @@ by initializing the estimator to the LPE_LAT/LON parameters when global informat modules/vtol_att_control - - - - Mount input mode - RC uses the AUX input channels (see MNT_MAN_* parameters), MAVLINK_ROI uses the MAV_CMD_DO_SET_ROI Mavlink message, and MAVLINK_DO_MOUNT the MAV_CMD_DO_MOUNT_CONFIGURE and MAV_CMD_DO_MOUNT_CONTROL messages to control a mount. - -1 - 3 - true + + Set offboard loss failsafe mode + The offboard loss failsafe will only be entered after a timeout, set by COM_OF_LOSS_T in seconds. + modules/commander + + Loiter + Land at current position + Return to Land + + + + Set offboard loss failsafe mode when RC is available + The offboard loss failsafe will only be entered after a timeout, set by COM_OF_LOSS_T in seconds. + modules/commander + + Altitude control + Position control + Return to Land + Manual + Loiter + Land at current position + + + + Position control navigation loss response + This sets the flight mode that will be used if navigation accuracy is no longer adequte for position control. Navigation accuracy checks can be disabled using the CBRK_VELPOSERR parameter, but doing so will remove protection for all flight modes. + modules/commander + + Assume no use of remote control after fallback. Switch to DESCEND if a height estimate is available, else switch to TERMINATION. + Assume use of remote control after fallback. Switch to ALTCTL if a height estimate is available, else switch to MANUAL. + + + + + + Mount input mode + RC uses the AUX input channels (see MNT_MAN_* parameters), MAVLINK_ROI uses the MAV_CMD_DO_SET_ROI Mavlink message, and MAVLINK_DO_MOUNT the MAV_CMD_DO_MOUNT_CONFIGURE and MAV_CMD_DO_MOUNT_CONTROL messages to control a mount. + -1 + 3 + true drivers/vmount RC @@ -4344,26 +4344,6 @@ applied to input of all axis: roll, pitch, yaw 0.05 modules/mc_att_control - - Max manual roll - 0.0 - 90.0 - deg - examples/mc_pos_control_multiplatform - - - Max manual pitch - 0.0 - 90.0 - deg - examples/mc_pos_control_multiplatform - - - Max manual yaw rate - 0.0 - deg/s - examples/mc_pos_control_multiplatform - Roll P gain Roll proportional gain, i.e. desired angular speed in rad/s for error 1 rad. @@ -4473,6 +4453,26 @@ applied to input of all axis: roll, pitch, yaw deg/s examples/mc_att_control_multiplatform + + Max manual roll + 0.0 + 90.0 + deg + examples/mc_pos_control_multiplatform + + + Max manual pitch + 0.0 + 90.0 + deg + examples/mc_pos_control_multiplatform + + + Max manual yaw rate + 0.0 + deg/s + examples/mc_pos_control_multiplatform + @@ -4948,109 +4948,194 @@ towards MPC_ACC_HOR_MAX/MPC_ACC_UP_MAX with jerk limit - - Invert direction of aux output channel 1 - Set to 1 to invert the channel, 0 for default direction. - + + Set the PWM output frequency for the main outputs + Set to 400 for industry default or 1000 for high frequency ESCs. Set to 0 for Oneshot125. + -1 + 2000 + Hz true - drivers/px4fmu + modules/sensors - - Invert direction of aux output channel 2 - Set to 1 to invert the channel, 0 for default direction. - + + Set the minimum PWM for the main outputs + Set to 1000 for industry default or 900 to increase servo travel. + 800 + 1400 + us true - drivers/px4fmu + modules/sensors - - Invert direction of aux output channel 3 - Set to 1 to invert the channel, 0 for default direction. - + + Set the maximum PWM for the main outputs + Set to 2000 for industry default or 2100 to increase servo travel. + 1600 + 2200 + us true - drivers/px4fmu + modules/sensors - - Invert direction of aux output channel 4 - Set to 1 to invert the channel, 0 for default direction. - + + Set the disarmed PWM for the main outputs + 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. + 0 + 2200 + us true - drivers/px4fmu + modules/sensors - - Invert direction of aux output channel 5 - Set to 1 to invert the channel, 0 for default direction. - + + Set the disarmed PWM for the main 1 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used + -1 + 2200 + us true - drivers/px4fmu + modules/sensors - - Invert direction of aux output channel 6 - Set to 1 to invert the channel, 0 for default direction. - + + Set the disarmed PWM for the main 2 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used + -1 + 2200 + us true - drivers/px4fmu + modules/sensors - - Trim value for FMU PWM output channel 1 - Set to normalized offset - -0.2 - 0.2 - 2 - drivers/px4fmu + + Set the disarmed PWM for the main 3 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used + -1 + 2200 + us + true + modules/sensors - - Trim value for FMU PWM output channel 2 - Set to normalized offset - -0.2 - 0.2 - 2 - drivers/px4fmu + + Set the disarmed PWM for the main 4 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used + -1 + 2200 + us + true + modules/sensors - - Trim value for FMU PWM output channel 3 - Set to normalized offset - -0.2 - 0.2 - 2 - drivers/px4fmu + + Set the disarmed PWM for the main 5 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used + -1 + 2200 + us + true + modules/sensors - - Trim value for FMU PWM output channel 4 - Set to normalized offset - -0.2 - 0.2 - 2 - drivers/px4fmu + + Set the disarmed PWM for the main 6 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used + -1 + 2200 + us + true + modules/sensors - - Trim value for FMU PWM output channel 5 - Set to normalized offset - -0.2 - 0.2 - 2 - drivers/px4fmu + + Set the disarmed PWM for the main 7 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used + -1 + 2200 + us + true + modules/sensors - - Trim value for FMU PWM output channel 6 - Set to normalized offset - -0.2 - 0.2 - 2 - drivers/px4fmu + + Set the disarmed PWM for the main 8 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used + -1 + 2200 + us + true + modules/sensors - - Thrust to PWM model parameter - Parameter used to model the relationship between static thrust and motor input PWM. Model is: thrust = (1-factor)*PWM + factor * PWM^2 - 0.0 - 1.0 - drivers/px4fmu + + Set the disarmed PWM for the AUX 1 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_AUX_DISARMED will be used + -1 + 2200 + us + true + modules/sensors - - Minimum motor rise time (slew rate limit) - 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. - 0.0 - s/(1000*PWM) - drivers/px4fmu + + Set the disarmed PWM for the AUX 2 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_AUX_DISARMED will be used + -1 + 2200 + us + true + modules/sensors + + + Set the disarmed PWM for the AUX 3 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_AUX_DISARMED will be used + -1 + 2200 + us + true + modules/sensors + + + Set the disarmed PWM for the AUX 4 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_AUX_DISARMED will be used + -1 + 2200 + us + true + modules/sensors + + + Set the disarmed PWM for the AUX 5 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_AUX_DISARMED will be used + -1 + 2200 + us + true + modules/sensors + + + Set the disarmed PWM for the AUX 6 output + This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_AUX_DISARMED will be used + -1 + 2200 + us + true + modules/sensors + + + Set the minimum PWM for the auxiliary outputs + Set to 1000 for default or 900 to increase servo travel + 800 + 1400 + us + true + modules/sensors + + + Set the maximum PWM for the auxiliary outputs + Set to 2000 for default or 2100 to increase servo travel + 1600 + 2200 + us + true + modules/sensors + + + Set the disarmed PWM for auxiliary outputs + 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. + 0 + 2200 + us + true + modules/sensors Invert direction of main output channel 1 @@ -5178,194 +5263,109 @@ towards MPC_ACC_HOR_MAX/MPC_ACC_UP_MAX with jerk limit drivers/px4io - - Set the PWM output frequency for the main outputs - Set to 400 for industry default or 1000 for high frequency ESCs. Set to 0 for Oneshot125. - -1 - 2000 - Hz + + Invert direction of aux output channel 1 + Set to 1 to invert the channel, 0 for default direction. + true - modules/sensors + drivers/px4fmu - - Set the minimum PWM for the main outputs - Set to 1000 for industry default or 900 to increase servo travel. - 800 - 1400 - us + + Invert direction of aux output channel 2 + Set to 1 to invert the channel, 0 for default direction. + true - modules/sensors + drivers/px4fmu - - Set the maximum PWM for the main outputs - Set to 2000 for industry default or 2100 to increase servo travel. - 1600 - 2200 - us + + Invert direction of aux output channel 3 + Set to 1 to invert the channel, 0 for default direction. + true - modules/sensors + drivers/px4fmu - - Set the disarmed PWM for the main outputs - 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. - 0 - 2200 - us + + Invert direction of aux output channel 4 + Set to 1 to invert the channel, 0 for default direction. + true - modules/sensors + drivers/px4fmu - - Set the disarmed PWM for the main 1 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used - -1 - 2200 - us + + Invert direction of aux output channel 5 + Set to 1 to invert the channel, 0 for default direction. + true - modules/sensors + drivers/px4fmu - - Set the disarmed PWM for the main 2 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used - -1 - 2200 - us + + Invert direction of aux output channel 6 + Set to 1 to invert the channel, 0 for default direction. + true - modules/sensors + drivers/px4fmu - - Set the disarmed PWM for the main 3 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used - -1 - 2200 - us - true - modules/sensors + + Trim value for FMU PWM output channel 1 + Set to normalized offset + -0.2 + 0.2 + 2 + drivers/px4fmu - - Set the disarmed PWM for the main 4 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used - -1 - 2200 - us - true - modules/sensors + + Trim value for FMU PWM output channel 2 + Set to normalized offset + -0.2 + 0.2 + 2 + drivers/px4fmu - - Set the disarmed PWM for the main 5 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used - -1 - 2200 - us - true - modules/sensors + + Trim value for FMU PWM output channel 3 + Set to normalized offset + -0.2 + 0.2 + 2 + drivers/px4fmu - - Set the disarmed PWM for the main 6 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used - -1 - 2200 - us - true - modules/sensors + + Trim value for FMU PWM output channel 4 + Set to normalized offset + -0.2 + 0.2 + 2 + drivers/px4fmu - - Set the disarmed PWM for the main 7 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used - -1 - 2200 - us - true - modules/sensors + + Trim value for FMU PWM output channel 5 + Set to normalized offset + -0.2 + 0.2 + 2 + drivers/px4fmu - - Set the disarmed PWM for the main 8 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_DISARMED will be used - -1 - 2200 - us - true - modules/sensors + + Trim value for FMU PWM output channel 6 + Set to normalized offset + -0.2 + 0.2 + 2 + drivers/px4fmu - - Set the disarmed PWM for the AUX 1 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_AUX_DISARMED will be used - -1 - 2200 - us - true - modules/sensors + + Thrust to PWM model parameter + Parameter used to model the relationship between static thrust and motor input PWM. Model is: thrust = (1-factor)*PWM + factor * PWM^2 + 0.0 + 1.0 + drivers/px4fmu - - Set the disarmed PWM for the AUX 2 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_AUX_DISARMED will be used - -1 - 2200 - us - true - modules/sensors - - - Set the disarmed PWM for the AUX 3 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_AUX_DISARMED will be used - -1 - 2200 - us - true - modules/sensors - - - Set the disarmed PWM for the AUX 4 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_AUX_DISARMED will be used - -1 - 2200 - us - true - modules/sensors - - - Set the disarmed PWM for the AUX 5 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_AUX_DISARMED will be used - -1 - 2200 - us - true - modules/sensors - - - Set the disarmed PWM for the AUX 6 output - This is the PWM pulse the autopilot is outputting if not armed. When set to -1 the value for PWM_AUX_DISARMED will be used - -1 - 2200 - us - true - modules/sensors - - - Set the minimum PWM for the auxiliary outputs - Set to 1000 for default or 900 to increase servo travel - 800 - 1400 - us - true - modules/sensors - - - Set the maximum PWM for the auxiliary outputs - Set to 2000 for default or 2100 to increase servo travel - 1600 - 2200 - us - true - modules/sensors - - - Set the disarmed PWM for auxiliary outputs - 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. - 0 - 2200 - us - true - modules/sensors + + Minimum motor rise time (slew rate limit) + 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. + 0.0 + s/(1000*PWM) + drivers/px4fmu @@ -5777,75 +5777,6 @@ towards MPC_ACC_HOR_MAX/MPC_ACC_UP_MAX with jerk limit - - PWM input channel that provides RSSI - 0: do not read RSSI from input channel 1-18: read RSSI from specified input channel Specify the range for RSSI input with RC_RSSI_PWM_MIN and RC_RSSI_PWM_MAX parameters. - 0 - 18 - drivers/px4io - - Channel 11 - Channel 10 - Channel 13 - Channel 12 - Channel 15 - Channel 14 - Channel 17 - Channel 16 - Channel 18 - Channel 1 - Unassigned - Channel 3 - Channel 2 - Channel 5 - Channel 4 - Channel 7 - Channel 6 - Channel 9 - Channel 8 - - - - Max input value for RSSI reading - Only used if RC_RSSI_PWM_CHAN > 0 - 0 - 2000 - drivers/px4io - - - Min input value for RSSI reading - Only used if RC_RSSI_PWM_CHAN > 0 - 0 - 2000 - drivers/px4io - - - Roll trim - 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. - -0.25 - 0.25 - 2 - 0.01 - modules/commander - - - Pitch trim - 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. - -0.25 - 0.25 - 2 - 0.01 - modules/commander - - - Yaw trim - 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. - -0.25 - 0.25 - 2 - 0.01 - modules/commander - RC channel 1 minimum Minimum value for RC channel 1 @@ -6941,6 +6872,75 @@ towards MPC_ACC_HOR_MAX/MPC_ACC_UP_MAX with jerk limit Hz modules/sensors + + Roll trim + 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. + -0.25 + 0.25 + 2 + 0.01 + modules/commander + + + Pitch trim + 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. + -0.25 + 0.25 + 2 + 0.01 + modules/commander + + + Yaw trim + 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. + -0.25 + 0.25 + 2 + 0.01 + modules/commander + + + PWM input channel that provides RSSI + 0: do not read RSSI from input channel 1-18: read RSSI from specified input channel Specify the range for RSSI input with RC_RSSI_PWM_MIN and RC_RSSI_PWM_MAX parameters. + 0 + 18 + drivers/px4io + + Channel 11 + Channel 10 + Channel 13 + Channel 12 + Channel 15 + Channel 14 + Channel 17 + Channel 16 + Channel 18 + Channel 1 + Unassigned + Channel 3 + Channel 2 + Channel 5 + Channel 4 + Channel 7 + Channel 6 + Channel 9 + Channel 8 + + + + Max input value for RSSI reading + Only used if RC_RSSI_PWM_CHAN > 0 + 0 + 2000 + drivers/px4io + + + Min input value for RSSI reading + Only used if RC_RSSI_PWM_CHAN > 0 + 0 + 2000 + drivers/px4io + @@ -7588,6 +7588,46 @@ FW_AIRSPD_MIN * RWTO_AIRSPD_SCL + + Logging rate + 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). + -1 + 250 + Hz + modules/sdlog2 + + + Extended logging mode + A value of -1 indicates the command line argument should be obeyed. A value of 0 disables extended logging mode, a value of 1 enables it. This parameter is only read out before logging starts (which commonly is before arming). + -1 + 1 + modules/sdlog2 + + Enable + Disable + Command Line + + + + Use timestamps only if GPS 3D fix is available + Constrain the log folder creation to only use the time stamp if a 3D GPS lock is present. + + modules/sdlog2 + + + Give logging app higher thread priority to avoid data loss. +This is used for gathering replay logs for the ekf2 module + A value of 0 indicates that the default priority is used. Increasing the parameter in steps of one increases the priority. + 0 + 3 + modules/sdlog2 + + Default priority + Low priority + Max priority + Medium priority + + UTC offset (unit: min) 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 @@ -7640,46 +7680,6 @@ FW_AIRSPD_MIN * RWTO_AIRSPD_SCL modules/logger - - Logging rate - 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). - -1 - 250 - Hz - modules/sdlog2 - - - Extended logging mode - A value of -1 indicates the command line argument should be obeyed. A value of 0 disables extended logging mode, a value of 1 enables it. This parameter is only read out before logging starts (which commonly is before arming). - -1 - 1 - modules/sdlog2 - - Enable - Disable - Command Line - - - - Use timestamps only if GPS 3D fix is available - Constrain the log folder creation to only use the time stamp if a 3D GPS lock is present. - - modules/sdlog2 - - - Give logging app higher thread priority to avoid data loss. -This is used for gathering replay logs for the ekf2 module - A value of 0 indicates that the default priority is used. Increasing the parameter in steps of one increases the priority. - 0 - 3 - modules/sdlog2 - - Default priority - Low priority - Max priority - Medium priority - - @@ -7696,94 +7696,6 @@ This is used for gathering replay logs for the ekf2 module - - Primary accel ID - modules/sensors - - - ID of the Accelerometer that the calibration is for - modules/sensors - - - Accelerometer X-axis offset - modules/sensors - - - Accelerometer Y-axis offset - modules/sensors - - - Accelerometer Z-axis offset - modules/sensors - - - Accelerometer X-axis scaling factor - modules/sensors - - - Accelerometer Y-axis scaling factor - modules/sensors - - - Accelerometer Z-axis scaling factor - modules/sensors - - - ID of the Accelerometer that the calibration is for - modules/sensors - - - Accelerometer X-axis offset - modules/sensors - - - Accelerometer Y-axis offset - modules/sensors - - - Accelerometer Z-axis offset - modules/sensors - - - Accelerometer X-axis scaling factor - modules/sensors - - - Accelerometer Y-axis scaling factor - modules/sensors - - - Accelerometer Z-axis scaling factor - modules/sensors - - - ID of the Accelerometer that the calibration is for - modules/sensors - - - Accelerometer X-axis offset - modules/sensors - - - Accelerometer Y-axis offset - modules/sensors - - - Accelerometer Z-axis offset - modules/sensors - - - Accelerometer X-axis scaling factor - modules/sensors - - - Accelerometer Y-axis scaling factor - modules/sensors - - - Accelerometer Z-axis scaling factor - modules/sensors - Primary mag ID modules/sensors @@ -8167,25 +8079,347 @@ This is used for gathering replay logs for the ekf2 module HB Pitot - - Airspeed sensor tube length - 0.01 - 0.5 - meter + + Airspeed sensor tube length + 0.01 + 0.5 + meter + modules/sensors + + + Differential pressure sensor offset + The offset (zero-reading) in Pascal + modules/sensors + + + Differential pressure sensor analog scaling + Pick the appropriate scaling from the datasheet. this number defines the (linear) conversion from voltage to Pascal (pa). For the MPXV7002DP this is 1000. NOTE: If the sensor always registers zero, try switching the static and dynamic tubes. + modules/sensors + + + Primary accel ID + modules/sensors + + + ID of the Accelerometer that the calibration is for + modules/sensors + + + Accelerometer X-axis offset + modules/sensors + + + Accelerometer Y-axis offset + modules/sensors + + + Accelerometer Z-axis offset + modules/sensors + + + Accelerometer X-axis scaling factor + modules/sensors + + + Accelerometer Y-axis scaling factor + modules/sensors + + + Accelerometer Z-axis scaling factor + modules/sensors + + + ID of the Accelerometer that the calibration is for + modules/sensors + + + Accelerometer X-axis offset + modules/sensors + + + Accelerometer Y-axis offset + modules/sensors + + + Accelerometer Z-axis offset + modules/sensors + + + Accelerometer X-axis scaling factor + modules/sensors + + + Accelerometer Y-axis scaling factor + modules/sensors + + + Accelerometer Z-axis scaling factor + modules/sensors + + + ID of the Accelerometer that the calibration is for + modules/sensors + + + Accelerometer X-axis offset + modules/sensors + + + Accelerometer Y-axis offset + modules/sensors + + + Accelerometer Z-axis offset + modules/sensors + + + Accelerometer X-axis scaling factor + modules/sensors + + + Accelerometer Y-axis scaling factor + modules/sensors + + + Accelerometer Z-axis scaling factor + modules/sensors + + + + + Set to 1 to enable thermal compensation for accelerometer sensors. Set to 0 to disable + 0 + 1 + modules/sensors + + + ID of Accelerometer that the calibration is for + modules/sensors + + + Accelerometer offset temperature ^3 polynomial coefficient - X axis + modules/sensors + + + Accelerometer offset temperature ^3 polynomial coefficient - Y axis + modules/sensors + + + Accelerometer offset temperature ^3 polynomial coefficient - Z axis + modules/sensors + + + Accelerometer offset temperature ^2 polynomial coefficient - X axis + modules/sensors + + + Accelerometer offset temperature ^2 polynomial coefficient - Y axis + modules/sensors + + + Accelerometer offset temperature ^2 polynomial coefficient - Z axis + modules/sensors + + + Accelerometer offset temperature ^1 polynomial coefficient - X axis + modules/sensors + + + Accelerometer offset temperature ^1 polynomial coefficient - Y axis + modules/sensors + + + Accelerometer offset temperature ^1 polynomial coefficient - Z axis + modules/sensors + + + Accelerometer offset temperature ^0 polynomial coefficient - X axis + modules/sensors + + + Accelerometer offset temperature ^0 polynomial coefficient - Y axis + modules/sensors + + + Accelerometer offset temperature ^0 polynomial coefficient - Z axis + modules/sensors + + + Accelerometer scale factor - X axis + modules/sensors + + + Accelerometer scale factor - Y axis + modules/sensors + + + Accelerometer scale factor - Z axis + modules/sensors + + + Accelerometer calibration reference temperature + modules/sensors + + + Accelerometer calibration minimum temperature + modules/sensors + + + Accelerometer calibration maximum temperature + modules/sensors + + + ID of Accelerometer that the calibration is for + modules/sensors + + + Accelerometer offset temperature ^3 polynomial coefficient - X axis + modules/sensors + + + Accelerometer offset temperature ^3 polynomial coefficient - Y axis + modules/sensors + + + Accelerometer offset temperature ^3 polynomial coefficient - Z axis + modules/sensors + + + Accelerometer offset temperature ^2 polynomial coefficient - X axis + modules/sensors + + + Accelerometer offset temperature ^2 polynomial coefficient - Y axis + modules/sensors + + + Accelerometer offset temperature ^2 polynomial coefficient - Z axis + modules/sensors + + + Accelerometer offset temperature ^1 polynomial coefficient - X axis + modules/sensors + + + Accelerometer offset temperature ^1 polynomial coefficient - Y axis + modules/sensors + + + Accelerometer offset temperature ^1 polynomial coefficient - Z axis + modules/sensors + + + Accelerometer offset temperature ^0 polynomial coefficient - X axis + modules/sensors + + + Accelerometer offset temperature ^0 polynomial coefficient - Y axis + modules/sensors + + + Accelerometer offset temperature ^0 polynomial coefficient - Z axis + modules/sensors + + + Accelerometer scale factor - X axis + modules/sensors + + + Accelerometer scale factor - Y axis + modules/sensors + + + Accelerometer scale factor - Z axis + modules/sensors + + + Accelerometer calibration reference temperature + modules/sensors + + + Accelerometer calibration minimum temperature + modules/sensors + + + Accelerometer calibration maximum temperature + modules/sensors + + + ID of Accelerometer that the calibration is for + modules/sensors + + + Accelerometer offset temperature ^3 polynomial coefficient - X axis + modules/sensors + + + Accelerometer offset temperature ^3 polynomial coefficient - Y axis + modules/sensors + + + Accelerometer offset temperature ^3 polynomial coefficient - Z axis + modules/sensors + + + Accelerometer offset temperature ^2 polynomial coefficient - X axis + modules/sensors + + + Accelerometer offset temperature ^2 polynomial coefficient - Y axis + modules/sensors + + + Accelerometer offset temperature ^2 polynomial coefficient - Z axis + modules/sensors + + + Accelerometer offset temperature ^1 polynomial coefficient - X axis + modules/sensors + + + Accelerometer offset temperature ^1 polynomial coefficient - Y axis + modules/sensors + + + Accelerometer offset temperature ^1 polynomial coefficient - Z axis + modules/sensors + + + Accelerometer offset temperature ^0 polynomial coefficient - X axis + modules/sensors + + + Accelerometer offset temperature ^0 polynomial coefficient - Y axis + modules/sensors + + + Accelerometer offset temperature ^0 polynomial coefficient - Z axis + modules/sensors + + + Accelerometer scale factor - X axis + modules/sensors + + + Accelerometer scale factor - Y axis + modules/sensors + + + Accelerometer scale factor - Z axis + modules/sensors + + + Accelerometer calibration reference temperature modules/sensors - - Differential pressure sensor offset - The offset (zero-reading) in Pascal + + Accelerometer calibration minimum temperature modules/sensors - - Differential pressure sensor analog scaling - Pick the appropriate scaling from the datasheet. this number defines the (linear) conversion from voltage to Pascal (pa). For the MPXV7002DP this is 1000. NOTE: If the sensor always registers zero, try switching the static and dynamic tubes. + + Accelerometer calibration maximum temperature modules/sensors - - Set to 1 to enable thermal compensation for barometric pressure sensors. Set to 0 to disable 0 @@ -8538,258 +8772,24 @@ This is used for gathering replay logs for the ekf2 module Gyro scale factor - X axis modules/sensors - - Gyro scale factor - Y axis - modules/sensors - - - Gyro scale factor - Z axis - modules/sensors - - - Gyro calibration reference temperature - modules/sensors - - - Gyro calibration minimum temperature - modules/sensors - - - Gyro calibration maximum temperature - modules/sensors - - - Set to 1 to enable thermal compensation for accelerometer sensors. Set to 0 to disable - 0 - 1 - modules/sensors - - - ID of Accelerometer that the calibration is for - modules/sensors - - - Accelerometer offset temperature ^3 polynomial coefficient - X axis - modules/sensors - - - Accelerometer offset temperature ^3 polynomial coefficient - Y axis - modules/sensors - - - Accelerometer offset temperature ^3 polynomial coefficient - Z axis - modules/sensors - - - Accelerometer offset temperature ^2 polynomial coefficient - X axis - modules/sensors - - - Accelerometer offset temperature ^2 polynomial coefficient - Y axis - modules/sensors - - - Accelerometer offset temperature ^2 polynomial coefficient - Z axis - modules/sensors - - - Accelerometer offset temperature ^1 polynomial coefficient - X axis - modules/sensors - - - Accelerometer offset temperature ^1 polynomial coefficient - Y axis - modules/sensors - - - Accelerometer offset temperature ^1 polynomial coefficient - Z axis - modules/sensors - - - Accelerometer offset temperature ^0 polynomial coefficient - X axis - modules/sensors - - - Accelerometer offset temperature ^0 polynomial coefficient - Y axis - modules/sensors - - - Accelerometer offset temperature ^0 polynomial coefficient - Z axis - modules/sensors - - - Accelerometer scale factor - X axis - modules/sensors - - - Accelerometer scale factor - Y axis - modules/sensors - - - Accelerometer scale factor - Z axis - modules/sensors - - - Accelerometer calibration reference temperature - modules/sensors - - - Accelerometer calibration minimum temperature - modules/sensors - - - Accelerometer calibration maximum temperature - modules/sensors - - - ID of Accelerometer that the calibration is for - modules/sensors - - - Accelerometer offset temperature ^3 polynomial coefficient - X axis - modules/sensors - - - Accelerometer offset temperature ^3 polynomial coefficient - Y axis - modules/sensors - - - Accelerometer offset temperature ^3 polynomial coefficient - Z axis - modules/sensors - - - Accelerometer offset temperature ^2 polynomial coefficient - X axis - modules/sensors - - - Accelerometer offset temperature ^2 polynomial coefficient - Y axis - modules/sensors - - - Accelerometer offset temperature ^2 polynomial coefficient - Z axis - modules/sensors - - - Accelerometer offset temperature ^1 polynomial coefficient - X axis - modules/sensors - - - Accelerometer offset temperature ^1 polynomial coefficient - Y axis - modules/sensors - - - Accelerometer offset temperature ^1 polynomial coefficient - Z axis - modules/sensors - - - Accelerometer offset temperature ^0 polynomial coefficient - X axis - modules/sensors - - - Accelerometer offset temperature ^0 polynomial coefficient - Y axis - modules/sensors - - - Accelerometer offset temperature ^0 polynomial coefficient - Z axis - modules/sensors - - - Accelerometer scale factor - X axis - modules/sensors - - - Accelerometer scale factor - Y axis - modules/sensors - - - Accelerometer scale factor - Z axis - modules/sensors - - - Accelerometer calibration reference temperature - modules/sensors - - - Accelerometer calibration minimum temperature - modules/sensors - - - Accelerometer calibration maximum temperature - modules/sensors - - - ID of Accelerometer that the calibration is for - modules/sensors - - - Accelerometer offset temperature ^3 polynomial coefficient - X axis - modules/sensors - - - Accelerometer offset temperature ^3 polynomial coefficient - Y axis - modules/sensors - - - Accelerometer offset temperature ^3 polynomial coefficient - Z axis - modules/sensors - - - Accelerometer offset temperature ^2 polynomial coefficient - X axis - modules/sensors - - - Accelerometer offset temperature ^2 polynomial coefficient - Y axis - modules/sensors - - - Accelerometer offset temperature ^2 polynomial coefficient - Z axis - modules/sensors - - - Accelerometer offset temperature ^1 polynomial coefficient - X axis - modules/sensors - - - Accelerometer offset temperature ^1 polynomial coefficient - Y axis - modules/sensors - - - Accelerometer offset temperature ^1 polynomial coefficient - Z axis - modules/sensors - - - Accelerometer offset temperature ^0 polynomial coefficient - X axis - modules/sensors - - - Accelerometer offset temperature ^0 polynomial coefficient - Y axis - modules/sensors - - - Accelerometer offset temperature ^0 polynomial coefficient - Z axis - modules/sensors - - - Accelerometer scale factor - X axis - modules/sensors - - - Accelerometer scale factor - Y axis + + Gyro scale factor - Y axis modules/sensors - - Accelerometer scale factor - Z axis + + Gyro scale factor - Z axis modules/sensors - - Accelerometer calibration reference temperature + + Gyro calibration reference temperature modules/sensors - - Accelerometer calibration minimum temperature + + Gyro calibration minimum temperature modules/sensors - - Accelerometer calibration maximum temperature + + Gyro calibration maximum temperature modules/sensors @@ -8998,29 +8998,6 @@ This is used for gathering replay logs for the ekf2 module - - Run the FMU as a task to reduce latency - If true, the FMU will run in a separate task instead of on the work queue. Set this if low latency is required, for example for racing. This is a trade-off between RAM usage and latency: running as a task, it requires a separate stack and directly polls on the control topics, whereas running on the work queue, it runs at a fixed update rate. - - true - drivers/px4fmu - - - RGB Led brightness limit - Set to 0 to disable, 1 for minimum brightness up to 15 (max) - 0 - 15 - drivers/rgbled - - - Set usage of IO board - Can be used to use a standard startup script but with a FMU only set-up. Set to 0 to force the FMU only set-up. - 0 - 1 - - true - drivers/px4io - Auto-start script index CHANGING THIS VALUE REQUIRES A RESTART. Defines the auto-start script used to bootstrap the system. @@ -9156,6 +9133,29 @@ This is used for gathering replay logs for the ekf2 module deg C modules/systemlib + + Set usage of IO board + Can be used to use a standard startup script but with a FMU only set-up. Set to 0 to force the FMU only set-up. + 0 + 1 + + true + drivers/px4io + + + RGB Led brightness limit + Set to 0 to disable, 1 for minimum brightness up to 15 (max) + 0 + 15 + drivers/rgbled + + + Run the FMU as a task to reduce latency + If true, the FMU will run in a separate task instead of on the work queue. Set this if low latency is required, for example for racing. This is a trade-off between RAM usage and latency: running as a task, it requires a separate stack and directly polls on the control topics, whereas running on the work queue, it runs at a fixed update rate. + + true + drivers/px4fmu + @@ -9263,93 +9263,91 @@ This is used for gathering replay logs for the ekf2 module true modules/uavcan - + UAVCAN Node ID Read the specs at http://uavcan.org to learn more about Node ID. 1 125 - modules/uavcanesc + modules/uavcannode - + UAVCAN CAN bus bitrate 20000 1000000 - modules/uavcanesc + modules/uavcannode - + UAVCAN Node ID Read the specs at http://uavcan.org to learn more about Node ID. 1 125 - modules/uavcannode + modules/uavcanesc - + UAVCAN CAN bus bitrate 20000 1000000 - modules/uavcannode + modules/uavcanesc - - Target throttle value for pusher/puller motor during the transition to fw mode + + Position of tilt servo in mc mode 0.0 1.0 3 0.01 modules/vtol_att_control - - Maximum allowed down-pitch the controller is able to demand. This prevents large, negative -lift values being created when facing strong winds. The vehicle will use the pusher motor -to accelerate forward if necessary + + Position of tilt servo in transition mode 0.0 - 45.0 + 1.0 + 3 + 0.01 modules/vtol_att_control - - Fixed wing thrust scale for hover forward flight - 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. + + Position of tilt servo in fw mode 0.0 - 2.0 + 1.0 + 3 + 0.01 modules/vtol_att_control - - Back transition MC motor ramp up time - This sets the duration during wich the MC motors ramp up to the commanded thrust during the back transition stage. - 0.0 - 20.0 + + Duration of front transition phase 2 + 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. + 0.1 + 5.0 s - modules/vtol_att_control - - - Output on airbrakes channel during back transition -Used for airbrakes or with ESCs that have reverse thrust enabled on a seperate channel -Airbrakes need to be enables for your selected model/mixer - 0 - 1 - 2 + 3 0.01 modules/vtol_att_control - - Delay in seconds before applying back transition throttle -Set this to a value greater than 0 to give the motor time to spin down - unit s + + The channel number of motors that must be turned off in fixed wing mode 0 - 10 - 2 + 12345678 + 0 1 modules/vtol_att_control - - Thottle output during back transition -For ESCs and mixers that support reverse thrust on low PWM values set this to a negative value to apply active breaking -For ESCs that support thrust reversal with a control channel please set VT_B_REV_OUT and set this to a positive value to apply active breaking - -1 + + Differential thrust in forwards flight + Set to 1 to enable differential thrust in fixed-wing flight. + 0 1 + 0 + modules/vtol_att_control + + + Differential thrust scaling factor + This factor specifies how the yaw input gets mapped to differential thrust in forwards flight. + 0.0 + 1.0 2 - 0.01 + 0.1 modules/vtol_att_control @@ -9578,83 +9576,69 @@ For ESCs that support thrust reversal with a control channel please set VT_B_REV 0.01 modules/vtol_att_control - - Position of tilt servo in mc mode + + Target throttle value for pusher/puller motor during the transition to fw mode 0.0 1.0 3 0.01 modules/vtol_att_control - - Position of tilt servo in transition mode + + Maximum allowed down-pitch the controller is able to demand. This prevents large, negative +lift values being created when facing strong winds. The vehicle will use the pusher motor +to accelerate forward if necessary 0.0 - 1.0 - 3 - 0.01 + 45.0 modules/vtol_att_control - - Position of tilt servo in fw mode + + Fixed wing thrust scale for hover forward flight + 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. 0.0 - 1.0 - 3 - 0.01 + 2.0 modules/vtol_att_control - - Duration of front transition phase 2 - 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. - 0.1 - 5.0 + + Back transition MC motor ramp up time + This sets the duration during wich the MC motors ramp up to the commanded thrust during the back transition stage. + 0.0 + 20.0 s - 3 - 0.01 modules/vtol_att_control - - The channel number of motors that must be turned off in fixed wing mode + + Output on airbrakes channel during back transition +Used for airbrakes or with ESCs that have reverse thrust enabled on a seperate channel +Airbrakes need to be enables for your selected model/mixer 0 - 12345678 - 0 - 1 + 1 + 2 + 0.01 modules/vtol_att_control - - Differential thrust in forwards flight - Set to 1 to enable differential thrust in fixed-wing flight. + + Delay in seconds before applying back transition throttle +Set this to a value greater than 0 to give the motor time to spin down + unit s 0 - 1 - 0 + 10 + 2 + 1 modules/vtol_att_control - - Differential thrust scaling factor - This factor specifies how the yaw input gets mapped to differential thrust in forwards flight. - 0.0 - 1.0 + + Thottle output during back transition +For ESCs and mixers that support reverse thrust on low PWM values set this to a negative value to apply active breaking +For ESCs that support thrust reversal with a control channel please set VT_B_REV_OUT and set this to a positive value to apply active breaking + -1 + 1 2 - 0.1 + 0.01 modules/vtol_att_control - - EXFW_HDNG_P - examples/fixedwing_control - - - EXFW_ROLL_P - examples/fixedwing_control - - - EXFW_PITCH_P - examples/fixedwing_control - - - RV_YAW_P - examples/rover_steering_control - SEG_TH2V_P examples/segway @@ -9671,5 +9655,21 @@ For ESCs that support thrust reversal with a control channel please set VT_B_REV SEG_Q2V examples/segway + + EXFW_HDNG_P + examples/fixedwing_control + + + EXFW_ROLL_P + examples/fixedwing_control + + + EXFW_PITCH_P + examples/fixedwing_control + + + RV_YAW_P + examples/rover_steering_control +