mirror of
https://github.com/PX4/PX4-Autopilot.git
synced 2026-05-30 18:06:39 +08:00
docs: auto-sync metadata [skip ci]
Co-Authored-By: PX4 BuildBot <bot@px4.io>
This commit is contained in:
PX4BuildBot
+187
-187
@@ -95,202 +95,202 @@ They are not build into the module, and hence are neither published or subscribe
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::: details See messages
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- [VelocityLimits](../msg_docs/VelocityLimits.md)
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- [AirspeedValidatedV0](../msg_docs/AirspeedValidatedV0.md)
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- [EstimatorGpsStatus](../msg_docs/EstimatorGpsStatus.md)
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- [TecsStatus](../msg_docs/TecsStatus.md)
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- [EstimatorSensorBias](../msg_docs/EstimatorSensorBias.md)
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- [EscReport](../msg_docs/EscReport.md)
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- [PositionSetpoint](../msg_docs/PositionSetpoint.md)
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- [BatteryInfo](../msg_docs/BatteryInfo.md)
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- [PwmInput](../msg_docs/PwmInput.md)
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- [SensorSelection](../msg_docs/SensorSelection.md)
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- [InternalCombustionEngineStatus](../msg_docs/InternalCombustionEngineStatus.md)
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- [GimbalDeviceSetAttitude](../msg_docs/GimbalDeviceSetAttitude.md)
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- [CanInterfaceStatus](../msg_docs/CanInterfaceStatus.md)
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- [ActuatorOutputs](../msg_docs/ActuatorOutputs.md)
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- [DatamanResponse](../msg_docs/DatamanResponse.md)
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- [RegisterExtComponentReplyV0](../msg_docs/RegisterExtComponentReplyV0.md)
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- [VehicleRoi](../msg_docs/VehicleRoi.md)
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- [RoverAttitudeStatus](../msg_docs/RoverAttitudeStatus.md)
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- [NormalizedUnsignedSetpoint](../msg_docs/NormalizedUnsignedSetpoint.md)
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- [VehicleAirData](../msg_docs/VehicleAirData.md)
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- [GimbalDeviceInformation](../msg_docs/GimbalDeviceInformation.md)
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- [EstimatorAidSource1d](../msg_docs/EstimatorAidSource1d.md)
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- [VehicleLocalPositionV0](../msg_docs/VehicleLocalPositionV0.md)
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||||
- [SensorCorrection](../msg_docs/SensorCorrection.md)
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- [GimbalManagerStatus](../msg_docs/GimbalManagerStatus.md)
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- [SensorBaro](../msg_docs/SensorBaro.md)
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- [PpsCapture](../msg_docs/PpsCapture.md)
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- [AdcReport](../msg_docs/AdcReport.md)
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- [LedControl](../msg_docs/LedControl.md)
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- [OpenDroneIdSystem](../msg_docs/OpenDroneIdSystem.md)
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- [PositionControllerLandingStatus](../msg_docs/PositionControllerLandingStatus.md)
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- [OpenDroneIdOperatorId](../msg_docs/OpenDroneIdOperatorId.md)
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- [VehicleConstraints](../msg_docs/VehicleConstraints.md)
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- [FixedWingLateralStatus](../msg_docs/FixedWingLateralStatus.md)
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- [FailureDetectorStatus](../msg_docs/FailureDetectorStatus.md)
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- [PositionControllerStatus](../msg_docs/PositionControllerStatus.md)
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- [MissionResult](../msg_docs/MissionResult.md)
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- [GpioIn](../msg_docs/GpioIn.md)
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- [SensorAccel](../msg_docs/SensorAccel.md)
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- [InputRc](../msg_docs/InputRc.md)
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- [EstimatorEventFlags](../msg_docs/EstimatorEventFlags.md)
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- [SensorGnssStatus](../msg_docs/SensorGnssStatus.md)
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- [SensorPreflightMag](../msg_docs/SensorPreflightMag.md)
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- [FixedWingLateralGuidanceStatus](../msg_docs/FixedWingLateralGuidanceStatus.md)
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- [FollowTarget](../msg_docs/FollowTarget.md)
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- [MavlinkLog](../msg_docs/MavlinkLog.md)
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- [HeaterStatus](../msg_docs/HeaterStatus.md)
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- [Rpm](../msg_docs/Rpm.md)
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- [ArmingCheckReplyV0](../msg_docs/ArmingCheckReplyV0.md)
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- [LandingTargetPose](../msg_docs/LandingTargetPose.md)
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- [ActuatorTest](../msg_docs/ActuatorTest.md)
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- [PowerButtonState](../msg_docs/PowerButtonState.md)
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- [RegisterExtComponentRequestV0](../msg_docs/RegisterExtComponentRequestV0.md)
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- [OpenDroneIdArmStatus](../msg_docs/OpenDroneIdArmStatus.md)
|
||||
- [ConfigOverridesV0](../msg_docs/ConfigOverridesV0.md)
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- [VehicleStatusV0](../msg_docs/VehicleStatusV0.md)
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- [DeviceInformation](../msg_docs/DeviceInformation.md)
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- [ParameterSetValueResponse](../msg_docs/ParameterSetValueResponse.md)
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- [GeofenceStatus](../msg_docs/GeofenceStatus.md)
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- [DistanceSensorModeChangeRequest](../msg_docs/DistanceSensorModeChangeRequest.md)
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- [BatteryStatusV0](../msg_docs/BatteryStatusV0.md)
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- [EscStatus](../msg_docs/EscStatus.md)
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- [TiltrotorExtraControls](../msg_docs/TiltrotorExtraControls.md)
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- [GpioOut](../msg_docs/GpioOut.md)
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- [DebugArray](../msg_docs/DebugArray.md)
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- [MavlinkTunnel](../msg_docs/MavlinkTunnel.md)
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- [SensorUwb](../msg_docs/SensorUwb.md)
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||||
- [ParameterUpdate](../msg_docs/ParameterUpdate.md)
|
||||
- [GeneratorStatus](../msg_docs/GeneratorStatus.md)
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- [SensorGnssRelative](../msg_docs/SensorGnssRelative.md)
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- [NeuralControl](../msg_docs/NeuralControl.md)
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- [PurePursuitStatus](../msg_docs/PurePursuitStatus.md)
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- [GimbalManagerSetManualControl](../msg_docs/GimbalManagerSetManualControl.md)
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- [TuneControl](../msg_docs/TuneControl.md)
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- [EventV0](../msg_docs/EventV0.md)
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- [FlightPhaseEstimation](../msg_docs/FlightPhaseEstimation.md)
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- [NavigatorMissionItem](../msg_docs/NavigatorMissionItem.md)
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- [TrajectorySetpoint6dof](../msg_docs/TrajectorySetpoint6dof.md)
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- [Ekf2Timestamps](../msg_docs/Ekf2Timestamps.md)
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- [VehicleMagnetometer](../msg_docs/VehicleMagnetometer.md)
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- [VehicleLocalPositionV0](../msg_docs/VehicleLocalPositionV0.md)
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- [PositionSetpoint](../msg_docs/PositionSetpoint.md)
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- [VehicleImuStatus](../msg_docs/VehicleImuStatus.md)
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- [OrbTestLarge](../msg_docs/OrbTestLarge.md)
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- [MountOrientation](../msg_docs/MountOrientation.md)
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- [ButtonEvent](../msg_docs/ButtonEvent.md)
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- [DebugKeyValue](../msg_docs/DebugKeyValue.md)
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- [SensorAirflow](../msg_docs/SensorAirflow.md)
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- [FixedWingRunwayControl](../msg_docs/FixedWingRunwayControl.md)
|
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- [SensorMag](../msg_docs/SensorMag.md)
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- [OrbitStatus](../msg_docs/OrbitStatus.md)
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- [Event](../msg_docs/Event.md)
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- [EstimatorBias3d](../msg_docs/EstimatorBias3d.md)
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- [VehicleLocalPositionSetpoint](../msg_docs/VehicleLocalPositionSetpoint.md)
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- [EstimatorAidSource2d](../msg_docs/EstimatorAidSource2d.md)
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- [DebugVect](../msg_docs/DebugVect.md)
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- [QshellRetval](../msg_docs/QshellRetval.md)
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- [HomePositionV0](../msg_docs/HomePositionV0.md)
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- [RadioStatus](../msg_docs/RadioStatus.md)
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- [VehicleCommandAckV0](../msg_docs/VehicleCommandAckV0.md)
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||||
- [EstimatorAidSource3d](../msg_docs/EstimatorAidSource3d.md)
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||||
- [VehicleGlobalPositionV0](../msg_docs/VehicleGlobalPositionV0.md)
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||||
- [VehicleAngularVelocity](../msg_docs/VehicleAngularVelocity.md)
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||||
- [DebugValue](../msg_docs/DebugValue.md)
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||||
- [EstimatorSelectorStatus](../msg_docs/EstimatorSelectorStatus.md)
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||||
- [IridiumsbdStatus](../msg_docs/IridiumsbdStatus.md)
|
||||
- [SensorGyroFft](../msg_docs/SensorGyroFft.md)
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||||
- [ControlAllocatorStatus](../msg_docs/ControlAllocatorStatus.md)
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||||
- [SensorTemp](../msg_docs/SensorTemp.md)
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||||
- [GimbalManagerInformation](../msg_docs/GimbalManagerInformation.md)
|
||||
- [ActuatorArmed](../msg_docs/ActuatorArmed.md)
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||||
- [RateCtrlStatus](../msg_docs/RateCtrlStatus.md)
|
||||
- [VehicleStatusV1](../msg_docs/VehicleStatusV1.md)
|
||||
- [LoggerStatus](../msg_docs/LoggerStatus.md)
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||||
- [UlogStream](../msg_docs/UlogStream.md)
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||||
- [GpsInjectData](../msg_docs/GpsInjectData.md)
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||||
- [LaunchDetectionStatus](../msg_docs/LaunchDetectionStatus.md)
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||||
- [RcParameterMap](../msg_docs/RcParameterMap.md)
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||||
- [GimbalManagerSetAttitude](../msg_docs/GimbalManagerSetAttitude.md)
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- [SatelliteInfo](../msg_docs/SatelliteInfo.md)
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- [LogMessage](../msg_docs/LogMessage.md)
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- [VehicleAcceleration](../msg_docs/VehicleAcceleration.md)
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||||
- [ActuatorServosTrim](../msg_docs/ActuatorServosTrim.md)
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- [SensorsStatus](../msg_docs/SensorsStatus.md)
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||||
- [UlogStreamAck](../msg_docs/UlogStreamAck.md)
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- [FigureEightStatus](../msg_docs/FigureEightStatus.md)
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- [DronecanNodeStatus](../msg_docs/DronecanNodeStatus.md)
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- [YawEstimatorStatus](../msg_docs/YawEstimatorStatus.md)
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||||
- [DatamanRequest](../msg_docs/DatamanRequest.md)
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||||
- [MagWorkerData](../msg_docs/MagWorkerData.md)
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- [GimbalControls](../msg_docs/GimbalControls.md)
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||||
- [RaptorInput](../msg_docs/RaptorInput.md)
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||||
- [VehicleAttitudeSetpointV0](../msg_docs/VehicleAttitudeSetpointV0.md)
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||||
- [LandingGearWheel](../msg_docs/LandingGearWheel.md)
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||||
- [ParameterResetRequest](../msg_docs/ParameterResetRequest.md)
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||||
- [NavigatorStatus](../msg_docs/NavigatorStatus.md)
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||||
- [InternalCombustionEngineControl](../msg_docs/InternalCombustionEngineControl.md)
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||||
- [ActuatorControlsStatus](../msg_docs/ActuatorControlsStatus.md)
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||||
- [LandingTargetInnovations](../msg_docs/LandingTargetInnovations.md)
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||||
- [RoverSpeedStatus](../msg_docs/RoverSpeedStatus.md)
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||||
- [SensorGyroFifo](../msg_docs/SensorGyroFifo.md)
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||||
- [TaskStackInfo](../msg_docs/TaskStackInfo.md)
|
||||
- [Mission](../msg_docs/Mission.md)
|
||||
- [ActionRequest](../msg_docs/ActionRequest.md)
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||||
- [Cpuload](../msg_docs/Cpuload.md)
|
||||
- [ArmingCheckRequestV0](../msg_docs/ArmingCheckRequestV0.md)
|
||||
- [ParameterSetValueRequest](../msg_docs/ParameterSetValueRequest.md)
|
||||
- [RcChannels](../msg_docs/RcChannels.md)
|
||||
- [VehicleImu](../msg_docs/VehicleImu.md)
|
||||
- [IrlockReport](../msg_docs/IrlockReport.md)
|
||||
- [OpenDroneIdSelfId](../msg_docs/OpenDroneIdSelfId.md)
|
||||
- [Ping](../msg_docs/Ping.md)
|
||||
- [DifferentialPressure](../msg_docs/DifferentialPressure.md)
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||||
- [GeofenceResult](../msg_docs/GeofenceResult.md)
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||||
- [Px4ioStatus](../msg_docs/Px4ioStatus.md)
|
||||
- [SensorGyro](../msg_docs/SensorGyro.md)
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- [CameraCapture](../msg_docs/CameraCapture.md)
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||||
- [Vtx](../msg_docs/Vtx.md)
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||||
- [SystemPower](../msg_docs/SystemPower.md)
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||||
- [HoverThrustEstimate](../msg_docs/HoverThrustEstimate.md)
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||||
- [FollowTargetEstimator](../msg_docs/FollowTargetEstimator.md)
|
||||
- [UavcanParameterRequest](../msg_docs/UavcanParameterRequest.md)
|
||||
- [PowerMonitor](../msg_docs/PowerMonitor.md)
|
||||
- [OrbTestMedium](../msg_docs/OrbTestMedium.md)
|
||||
- [VehicleOpticalFlowVel](../msg_docs/VehicleOpticalFlowVel.md)
|
||||
- [GainCompression](../msg_docs/GainCompression.md)
|
||||
- [CameraTrigger](../msg_docs/CameraTrigger.md)
|
||||
- [GpioRequest](../msg_docs/GpioRequest.md)
|
||||
- [MagnetometerBiasEstimate](../msg_docs/MagnetometerBiasEstimate.md)
|
||||
- [VehicleAttitudeSetpointV0](../msg_docs/VehicleAttitudeSetpointV0.md)
|
||||
- [EventV0](../msg_docs/EventV0.md)
|
||||
- [FollowTarget](../msg_docs/FollowTarget.md)
|
||||
- [RcChannels](../msg_docs/RcChannels.md)
|
||||
- [DatamanRequest](../msg_docs/DatamanRequest.md)
|
||||
- [QshellRetval](../msg_docs/QshellRetval.md)
|
||||
- [VehicleStatusV0](../msg_docs/VehicleStatusV0.md)
|
||||
- [OrbTest](../msg_docs/OrbTest.md)
|
||||
- [RaptorStatus](../msg_docs/RaptorStatus.md)
|
||||
- [Airspeed](../msg_docs/Airspeed.md)
|
||||
- [VehicleImu](../msg_docs/VehicleImu.md)
|
||||
- [RaptorInput](../msg_docs/RaptorInput.md)
|
||||
- [Ekf2Timestamps](../msg_docs/Ekf2Timestamps.md)
|
||||
- [MagWorkerData](../msg_docs/MagWorkerData.md)
|
||||
- [VehicleMagnetometer](../msg_docs/VehicleMagnetometer.md)
|
||||
- [UavcanParameterValue](../msg_docs/UavcanParameterValue.md)
|
||||
- [OpenDroneIdArmStatus](../msg_docs/OpenDroneIdArmStatus.md)
|
||||
- [FixedWingLateralGuidanceStatus](../msg_docs/FixedWingLateralGuidanceStatus.md)
|
||||
- [EstimatorAidSource2d](../msg_docs/EstimatorAidSource2d.md)
|
||||
- [RoverAttitudeStatus](../msg_docs/RoverAttitudeStatus.md)
|
||||
- [DifferentialPressure](../msg_docs/DifferentialPressure.md)
|
||||
- [SensorsStatusImu](../msg_docs/SensorsStatusImu.md)
|
||||
- [SensorMag](../msg_docs/SensorMag.md)
|
||||
- [NormalizedUnsignedSetpoint](../msg_docs/NormalizedUnsignedSetpoint.md)
|
||||
- [SensorPreflightMag](../msg_docs/SensorPreflightMag.md)
|
||||
- [VehicleOpticalFlow](../msg_docs/VehicleOpticalFlow.md)
|
||||
- [ButtonEvent](../msg_docs/ButtonEvent.md)
|
||||
- [VehicleStatusV1](../msg_docs/VehicleStatusV1.md)
|
||||
- [BatteryInfo](../msg_docs/BatteryInfo.md)
|
||||
- [EstimatorAidSource3d](../msg_docs/EstimatorAidSource3d.md)
|
||||
- [EstimatorSensorBias](../msg_docs/EstimatorSensorBias.md)
|
||||
- [DistanceSensorModeChangeRequest](../msg_docs/DistanceSensorModeChangeRequest.md)
|
||||
- [GpioIn](../msg_docs/GpioIn.md)
|
||||
- [DebugValue](../msg_docs/DebugValue.md)
|
||||
- [RoverRateStatus](../msg_docs/RoverRateStatus.md)
|
||||
- [ActuatorControlsStatus](../msg_docs/ActuatorControlsStatus.md)
|
||||
- [SensorAccelFifo](../msg_docs/SensorAccelFifo.md)
|
||||
- [CameraStatus](../msg_docs/CameraStatus.md)
|
||||
- [CameraTrigger](../msg_docs/CameraTrigger.md)
|
||||
- [VehicleLocalPositionSetpoint](../msg_docs/VehicleLocalPositionSetpoint.md)
|
||||
- [SensorGyroFifo](../msg_docs/SensorGyroFifo.md)
|
||||
- [PwmInput](../msg_docs/PwmInput.md)
|
||||
- [VehicleGlobalPositionV0](../msg_docs/VehicleGlobalPositionV0.md)
|
||||
- [OpenDroneIdSelfId](../msg_docs/OpenDroneIdSelfId.md)
|
||||
- [CanInterfaceStatus](../msg_docs/CanInterfaceStatus.md)
|
||||
- [RateCtrlStatus](../msg_docs/RateCtrlStatus.md)
|
||||
- [RtlStatus](../msg_docs/RtlStatus.md)
|
||||
- [UavcanParameterRequest](../msg_docs/UavcanParameterRequest.md)
|
||||
- [AdcReport](../msg_docs/AdcReport.md)
|
||||
- [EstimatorStates](../msg_docs/EstimatorStates.md)
|
||||
- [SensorHygrometer](../msg_docs/SensorHygrometer.md)
|
||||
- [TuneControl](../msg_docs/TuneControl.md)
|
||||
- [BatteryStatusV0](../msg_docs/BatteryStatusV0.md)
|
||||
- [VelocityLimits](../msg_docs/VelocityLimits.md)
|
||||
- [GeofenceStatus](../msg_docs/GeofenceStatus.md)
|
||||
- [EscReport](../msg_docs/EscReport.md)
|
||||
- [RtlTimeEstimate](../msg_docs/RtlTimeEstimate.md)
|
||||
- [HeaterStatus](../msg_docs/HeaterStatus.md)
|
||||
- [GimbalControls](../msg_docs/GimbalControls.md)
|
||||
- [EstimatorGpsStatus](../msg_docs/EstimatorGpsStatus.md)
|
||||
- [VehicleAngularAccelerationSetpoint](../msg_docs/VehicleAngularAccelerationSetpoint.md)
|
||||
- [EstimatorBias](../msg_docs/EstimatorBias.md)
|
||||
- [Mission](../msg_docs/Mission.md)
|
||||
- [VehicleAcceleration](../msg_docs/VehicleAcceleration.md)
|
||||
- [ActuatorArmed](../msg_docs/ActuatorArmed.md)
|
||||
- [LogMessage](../msg_docs/LogMessage.md)
|
||||
- [NavigatorMissionItem](../msg_docs/NavigatorMissionItem.md)
|
||||
- [WheelEncoders](../msg_docs/WheelEncoders.md)
|
||||
- [EstimatorInnovations](../msg_docs/EstimatorInnovations.md)
|
||||
- [RtlStatus](../msg_docs/RtlStatus.md)
|
||||
- [RaptorStatus](../msg_docs/RaptorStatus.md)
|
||||
- [ActuatorOutputs](../msg_docs/ActuatorOutputs.md)
|
||||
- [DronecanNodeStatus](../msg_docs/DronecanNodeStatus.md)
|
||||
- [VehicleCommandAckV0](../msg_docs/VehicleCommandAckV0.md)
|
||||
- [VehicleAirData](../msg_docs/VehicleAirData.md)
|
||||
- [UlogStream](../msg_docs/UlogStream.md)
|
||||
- [MavlinkTunnel](../msg_docs/MavlinkTunnel.md)
|
||||
- [PositionControllerStatus](../msg_docs/PositionControllerStatus.md)
|
||||
- [GimbalManagerSetAttitude](../msg_docs/GimbalManagerSetAttitude.md)
|
||||
- [AirspeedValidatedV0](../msg_docs/AirspeedValidatedV0.md)
|
||||
- [OpenDroneIdOperatorId](../msg_docs/OpenDroneIdOperatorId.md)
|
||||
- [EstimatorSelectorStatus](../msg_docs/EstimatorSelectorStatus.md)
|
||||
- [ParameterSetValueRequest](../msg_docs/ParameterSetValueRequest.md)
|
||||
- [RcParameterMap](../msg_docs/RcParameterMap.md)
|
||||
- [LaunchDetectionStatus](../msg_docs/LaunchDetectionStatus.md)
|
||||
- [SensorGyroFft](../msg_docs/SensorGyroFft.md)
|
||||
- [SatelliteInfo](../msg_docs/SatelliteInfo.md)
|
||||
- [AirspeedWind](../msg_docs/AirspeedWind.md)
|
||||
- [SensorAccelFifo](../msg_docs/SensorAccelFifo.md)
|
||||
- [EstimatorBias](../msg_docs/EstimatorBias.md)
|
||||
- [RoverRateStatus](../msg_docs/RoverRateStatus.md)
|
||||
- [CellularStatus](../msg_docs/CellularStatus.md)
|
||||
- [QshellReq](../msg_docs/QshellReq.md)
|
||||
- [VehicleAngularAccelerationSetpoint](../msg_docs/VehicleAngularAccelerationSetpoint.md)
|
||||
- [GpsDump](../msg_docs/GpsDump.md)
|
||||
- [VehicleOpticalFlow](../msg_docs/VehicleOpticalFlow.md)
|
||||
- [SensorsStatusImu](../msg_docs/SensorsStatusImu.md)
|
||||
- [EstimatorStates](../msg_docs/EstimatorStates.md)
|
||||
- [Airspeed](../msg_docs/Airspeed.md)
|
||||
- [FuelTankStatus](../msg_docs/FuelTankStatus.md)
|
||||
- [TakeoffStatus](../msg_docs/TakeoffStatus.md)
|
||||
- [FollowTargetStatus](../msg_docs/FollowTargetStatus.md)
|
||||
- [Gripper](../msg_docs/Gripper.md)
|
||||
- [CameraStatus](../msg_docs/CameraStatus.md)
|
||||
- [ParameterSetUsedRequest](../msg_docs/ParameterSetUsedRequest.md)
|
||||
- [AutotuneAttitudeControlStatus](../msg_docs/AutotuneAttitudeControlStatus.md)
|
||||
- [VehicleImuStatus](../msg_docs/VehicleImuStatus.md)
|
||||
- [EstimatorStatus](../msg_docs/EstimatorStatus.md)
|
||||
- [UavcanParameterValue](../msg_docs/UavcanParameterValue.md)
|
||||
- [TaskStackInfo](../msg_docs/TaskStackInfo.md)
|
||||
- [GeneratorStatus](../msg_docs/GeneratorStatus.md)
|
||||
- [Vtx](../msg_docs/Vtx.md)
|
||||
- [Event](../msg_docs/Event.md)
|
||||
- [HealthReport](../msg_docs/HealthReport.md)
|
||||
- [GpioConfig](../msg_docs/GpioConfig.md)
|
||||
- [FuelTankStatus](../msg_docs/FuelTankStatus.md)
|
||||
- [UlogStreamAck](../msg_docs/UlogStreamAck.md)
|
||||
- [EstimatorEventFlags](../msg_docs/EstimatorEventFlags.md)
|
||||
- [MagnetometerBiasEstimate](../msg_docs/MagnetometerBiasEstimate.md)
|
||||
- [SensorsStatus](../msg_docs/SensorsStatus.md)
|
||||
- [TrajectorySetpoint6dof](../msg_docs/TrajectorySetpoint6dof.md)
|
||||
- [SensorAirflow](../msg_docs/SensorAirflow.md)
|
||||
- [VehicleRoi](../msg_docs/VehicleRoi.md)
|
||||
- [DebugVect](../msg_docs/DebugVect.md)
|
||||
- [ActuatorServosTrim](../msg_docs/ActuatorServosTrim.md)
|
||||
- [SensorTemp](../msg_docs/SensorTemp.md)
|
||||
- [FixedWingRunwayControl](../msg_docs/FixedWingRunwayControl.md)
|
||||
- [GpsDump](../msg_docs/GpsDump.md)
|
||||
- [ActuatorTest](../msg_docs/ActuatorTest.md)
|
||||
- [RegisterExtComponentReplyV0](../msg_docs/RegisterExtComponentReplyV0.md)
|
||||
- [GimbalManagerStatus](../msg_docs/GimbalManagerStatus.md)
|
||||
- [SensorUwb](../msg_docs/SensorUwb.md)
|
||||
- [SensorSelection](../msg_docs/SensorSelection.md)
|
||||
- [SensorGyro](../msg_docs/SensorGyro.md)
|
||||
- [SystemPower](../msg_docs/SystemPower.md)
|
||||
- [ConfigOverridesV0](../msg_docs/ConfigOverridesV0.md)
|
||||
- [SensorAccel](../msg_docs/SensorAccel.md)
|
||||
- [Px4ioStatus](../msg_docs/Px4ioStatus.md)
|
||||
- [FigureEightStatus](../msg_docs/FigureEightStatus.md)
|
||||
- [VehicleAngularVelocity](../msg_docs/VehicleAngularVelocity.md)
|
||||
- [EstimatorBias3d](../msg_docs/EstimatorBias3d.md)
|
||||
- [FailureDetectorStatus](../msg_docs/FailureDetectorStatus.md)
|
||||
- [Rpm](../msg_docs/Rpm.md)
|
||||
- [RoverSpeedStatus](../msg_docs/RoverSpeedStatus.md)
|
||||
- [DebugKeyValue](../msg_docs/DebugKeyValue.md)
|
||||
- [GimbalDeviceSetAttitude](../msg_docs/GimbalDeviceSetAttitude.md)
|
||||
- [MountOrientation](../msg_docs/MountOrientation.md)
|
||||
- [NeuralControl](../msg_docs/NeuralControl.md)
|
||||
- [HoverThrustEstimate](../msg_docs/HoverThrustEstimate.md)
|
||||
- [VehicleConstraints](../msg_docs/VehicleConstraints.md)
|
||||
- [InternalCombustionEngineStatus](../msg_docs/InternalCombustionEngineStatus.md)
|
||||
- [PowerButtonState](../msg_docs/PowerButtonState.md)
|
||||
- [ArmingCheckRequestV0](../msg_docs/ArmingCheckRequestV0.md)
|
||||
- [InternalCombustionEngineControl](../msg_docs/InternalCombustionEngineControl.md)
|
||||
- [AutotuneAttitudeControlStatus](../msg_docs/AutotuneAttitudeControlStatus.md)
|
||||
- [VehicleOpticalFlowVel](../msg_docs/VehicleOpticalFlowVel.md)
|
||||
- [ControlAllocatorStatus](../msg_docs/ControlAllocatorStatus.md)
|
||||
- [ActionRequest](../msg_docs/ActionRequest.md)
|
||||
- [DatamanResponse](../msg_docs/DatamanResponse.md)
|
||||
- [FlightPhaseEstimation](../msg_docs/FlightPhaseEstimation.md)
|
||||
- [FollowTargetStatus](../msg_docs/FollowTargetStatus.md)
|
||||
- [InputRc](../msg_docs/InputRc.md)
|
||||
- [ArmingCheckReplyV0](../msg_docs/ArmingCheckReplyV0.md)
|
||||
- [Ping](../msg_docs/Ping.md)
|
||||
- [EstimatorAidSource1d](../msg_docs/EstimatorAidSource1d.md)
|
||||
- [LandingGearWheel](../msg_docs/LandingGearWheel.md)
|
||||
- [TakeoffStatus](../msg_docs/TakeoffStatus.md)
|
||||
- [NavigatorStatus](../msg_docs/NavigatorStatus.md)
|
||||
- [MavlinkLog](../msg_docs/MavlinkLog.md)
|
||||
- [LandingTargetPose](../msg_docs/LandingTargetPose.md)
|
||||
- [GainCompression](../msg_docs/GainCompression.md)
|
||||
- [HomePositionV0](../msg_docs/HomePositionV0.md)
|
||||
- [GpioRequest](../msg_docs/GpioRequest.md)
|
||||
- [SensorGnssRelative](../msg_docs/SensorGnssRelative.md)
|
||||
- [ParameterSetValueResponse](../msg_docs/ParameterSetValueResponse.md)
|
||||
- [EscStatus](../msg_docs/EscStatus.md)
|
||||
- [CellularStatus](../msg_docs/CellularStatus.md)
|
||||
- [TiltrotorExtraControls](../msg_docs/TiltrotorExtraControls.md)
|
||||
- [PurePursuitStatus](../msg_docs/PurePursuitStatus.md)
|
||||
- [GimbalManagerSetManualControl](../msg_docs/GimbalManagerSetManualControl.md)
|
||||
- [GimbalManagerInformation](../msg_docs/GimbalManagerInformation.md)
|
||||
- [YawEstimatorStatus](../msg_docs/YawEstimatorStatus.md)
|
||||
- [Cpuload](../msg_docs/Cpuload.md)
|
||||
- [CameraCapture](../msg_docs/CameraCapture.md)
|
||||
- [QshellReq](../msg_docs/QshellReq.md)
|
||||
- [Gripper](../msg_docs/Gripper.md)
|
||||
- [OrbTestMedium](../msg_docs/OrbTestMedium.md)
|
||||
- [ParameterResetRequest](../msg_docs/ParameterResetRequest.md)
|
||||
- [SensorGnssStatus](../msg_docs/SensorGnssStatus.md)
|
||||
- [EstimatorStatus](../msg_docs/EstimatorStatus.md)
|
||||
- [RadioStatus](../msg_docs/RadioStatus.md)
|
||||
- [FollowTargetEstimator](../msg_docs/FollowTargetEstimator.md)
|
||||
- [LandingTargetInnovations](../msg_docs/LandingTargetInnovations.md)
|
||||
- [DebugArray](../msg_docs/DebugArray.md)
|
||||
- [IridiumsbdStatus](../msg_docs/IridiumsbdStatus.md)
|
||||
- [OrbitStatus](../msg_docs/OrbitStatus.md)
|
||||
- [ParameterSetUsedRequest](../msg_docs/ParameterSetUsedRequest.md)
|
||||
- [FixedWingLateralStatus](../msg_docs/FixedWingLateralStatus.md)
|
||||
- [SensorBaro](../msg_docs/SensorBaro.md)
|
||||
- [GeofenceResult](../msg_docs/GeofenceResult.md)
|
||||
- [TecsStatus](../msg_docs/TecsStatus.md)
|
||||
- [OpenDroneIdSystem](../msg_docs/OpenDroneIdSystem.md)
|
||||
- [PpsCapture](../msg_docs/PpsCapture.md)
|
||||
- [ManualControlSwitches](../msg_docs/ManualControlSwitches.md)
|
||||
- [SensorHygrometer](../msg_docs/SensorHygrometer.md)
|
||||
- [SensorCorrection](../msg_docs/SensorCorrection.md)
|
||||
- [GimbalDeviceInformation](../msg_docs/GimbalDeviceInformation.md)
|
||||
- [GpioOut](../msg_docs/GpioOut.md)
|
||||
- [GpsInjectData](../msg_docs/GpsInjectData.md)
|
||||
- [LoggerStatus](../msg_docs/LoggerStatus.md)
|
||||
- [DeviceInformation](../msg_docs/DeviceInformation.md)
|
||||
- [GpioConfig](../msg_docs/GpioConfig.md)
|
||||
- [PositionControllerLandingStatus](../msg_docs/PositionControllerLandingStatus.md)
|
||||
- [PowerMonitor](../msg_docs/PowerMonitor.md)
|
||||
- [ParameterUpdate](../msg_docs/ParameterUpdate.md)
|
||||
- [RegisterExtComponentRequestV0](../msg_docs/RegisterExtComponentRequestV0.md)
|
||||
:::
|
||||
|
||||
@@ -18,7 +18,7 @@ Published by the vehicle's allocation and consumed by the ESC protocol drivers e
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| timestamp_sample | `uint64` | us | | Sampling timestamp of the data this control response is based on |
|
||||
| reversible_flags | `uint16` | | | Bitset indicating which motors are configured to be reversible |
|
||||
| control | `float32[12]` | | [-1 : 1] | Normalized thrust. where 1 means maximum positive thrust, -1 maximum negative (if not supported by the output, <0 maps to NaN). NaN maps to disarmed (stop the motors) |
|
||||
| control | `float32[12]` | | [-1 : 1] | Normalized thrust. Where 1 means maximum positive thrust, -1 maximum negative (if not supported by the output, <0 maps to NaN). NaN maps to disarmed (stop the motors) |
|
||||
|
||||
## Constants
|
||||
|
||||
@@ -47,10 +47,10 @@ uint64 timestamp_sample # [us] Sampling timestamp of the data this control resp
|
||||
|
||||
uint16 reversible_flags # [-] Bitset indicating which motors are configured to be reversible
|
||||
|
||||
uint8 ACTUATOR_FUNCTION_MOTOR1 = 101 #
|
||||
uint8 ACTUATOR_FUNCTION_MOTOR1 = 101
|
||||
|
||||
uint8 NUM_CONTROLS = 12 #
|
||||
float32[12] control # [@range -1, 1] Normalized thrust. where 1 means maximum positive thrust, -1 maximum negative (if not supported by the output, <0 maps to NaN). NaN maps to disarmed (stop the motors)
|
||||
uint8 NUM_CONTROLS = 12
|
||||
float32[12] control # [@range -1, 1] Normalized thrust. Where 1 means maximum positive thrust, -1 maximum negative (if not supported by the output, <0 maps to NaN). NaN maps to disarmed (stop the motors)
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -43,7 +43,7 @@ uint32 MESSAGE_VERSION = 0
|
||||
uint64 timestamp # [us] Time since system start
|
||||
uint64 timestamp_sample # [us] Sampling timestamp of the data this control response is based on
|
||||
|
||||
uint8 NUM_CONTROLS = 8 #
|
||||
uint8 NUM_CONTROLS = 8
|
||||
float32[8] control # [-] [@range -1, 1] Normalized output. 1 means maximum positive position. -1 maximum negative position (if not supported by the output, <0 maps to NaN). NaN maps to disarmed.
|
||||
```
|
||||
|
||||
|
||||
@@ -57,7 +57,6 @@ Used by controllers, estimators and for airspeed reporting to operator.
|
||||
# Provides information about airspeed (indicated, true, calibrated) and the source of the data.
|
||||
# Used by controllers, estimators and for airspeed reporting to operator.
|
||||
|
||||
|
||||
uint32 MESSAGE_VERSION = 1
|
||||
|
||||
uint64 timestamp # [us] Time since system start
|
||||
|
||||
@@ -25,7 +25,7 @@ Battery instance information is also logged and streamed in MAVLink telemetry.
|
||||
| remaining | `float32` | | [0 : 1] | Remaining capacity (Invalid: -1) |
|
||||
| scale | `float32` | | [1 : -] | Scaling factor to compensate for lower actuation power caused by voltage sag (Invalid: -1) |
|
||||
| time_remaining_s | `float32` | s | | Predicted time remaining until battery is empty under previous averaged load (Invalid: NaN) |
|
||||
| temperature | `float32` | °C | | Temperature of the battery (Invalid: NaN) |
|
||||
| temperature | `float32` | degC | | Temperature of the battery (Invalid: NaN) |
|
||||
| cell_count | `uint8` | | | Number of cells (Invalid: 0) |
|
||||
| source | `uint8` | | [SOURCE](#SOURCE) | Battery source |
|
||||
| priority | `uint8` | | | Zero based priority is the connection on the Power Controller V1..Vn AKA BrickN-1 |
|
||||
@@ -132,10 +132,9 @@ float32 discharged_mah # [mAh] [@invalid -1] Discharged amount
|
||||
float32 remaining # [@range 0,1] [@invalid -1] Remaining capacity
|
||||
float32 scale # [-] [@range 1,] [@invalid -1] Scaling factor to compensate for lower actuation power caused by voltage sag
|
||||
float32 time_remaining_s # [s] [@invalid NaN] Predicted time remaining until battery is empty under previous averaged load
|
||||
float32 temperature # [°C] [@invalid NaN] Temperature of the battery
|
||||
float32 temperature # [degC] [@invalid NaN] Temperature of the battery
|
||||
uint8 cell_count # [-] [@invalid 0] Number of cells
|
||||
|
||||
|
||||
uint8 source # [@enum SOURCE] Battery source
|
||||
uint8 SOURCE_POWER_MODULE = 0 # Power module (analog ADC or I2C power monitor)
|
||||
uint8 SOURCE_EXTERNAL = 1 # External (MAVLink, CAN, or external driver)
|
||||
|
||||
@@ -4,7 +4,10 @@ pageClass: is-wide-page
|
||||
|
||||
# FixedWingLateralSetpoint (UORB message)
|
||||
|
||||
Fixed Wing Lateral Setpoint message. Used by the fw_lateral_longitudinal_control module. At least one of course, airspeed_direction, or lateral_acceleration must be finite.
|
||||
Fixed Wing Lateral Setpoint message.
|
||||
|
||||
Used by the fw_lateral_longitudinal_control module
|
||||
At least one of course, airspeed_direction, or lateral_acceleration must be finite.
|
||||
|
||||
**TOPICS:** fixed_wing_lateral_setpoint
|
||||
|
||||
@@ -12,10 +15,10 @@ Fixed Wing Lateral Setpoint message. Used by the fw_lateral_longitudinal_control
|
||||
|
||||
| Name | Type | Unit [Frame] | Range/Enum | Description |
|
||||
| -------------------- | --------- | ------------ | ---------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| course | `float32` | rad | [-pi : pi] | Desired direction of travel over ground w.r.t (true) North. NAN if not controlled directly. |
|
||||
| airspeed_direction | `float32` | rad | [-pi : pi] | Desired horizontal angle of airspeed vector w.r.t. (true) North. Same as vehicle heading if in the absence of sideslip. NAN if not controlled directly, takes precedence over course if finite. |
|
||||
| lateral_acceleration | `float32` | FRD | | Lateral acceleration setpoint. NAN if not controlled directly, used as feedforward if either course setpoint or airspeed_direction is finite. |
|
||||
| lateral_acceleration | `float32` | m/s^2 [FRD] | | Lateral acceleration setpoint. NAN if not controlled directly, used as feedforward if either course setpoint or airspeed_direction is finite. |
|
||||
|
||||
## Constants
|
||||
|
||||
@@ -31,16 +34,17 @@ Fixed Wing Lateral Setpoint message. Used by the fw_lateral_longitudinal_control
|
||||
|
||||
```c
|
||||
# Fixed Wing Lateral Setpoint message
|
||||
#
|
||||
# Used by the fw_lateral_longitudinal_control module
|
||||
# At least one of course, airspeed_direction, or lateral_acceleration must be finite.
|
||||
|
||||
uint32 MESSAGE_VERSION = 0
|
||||
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
uint64 timestamp # [us] Time since system start
|
||||
|
||||
float32 course # [rad] [@range -pi, pi] Desired direction of travel over ground w.r.t (true) North. NAN if not controlled directly.
|
||||
float32 airspeed_direction # [rad] [@range -pi, pi] Desired horizontal angle of airspeed vector w.r.t. (true) North. Same as vehicle heading if in the absence of sideslip. NAN if not controlled directly, takes precedence over course if finite.
|
||||
float32 lateral_acceleration # [m/s^2] [FRD] Lateral acceleration setpoint. NAN if not controlled directly, used as feedforward if either course setpoint or airspeed_direction is finite.
|
||||
float32 lateral_acceleration # [m/s^2] [@frame FRD] Lateral acceleration setpoint. NAN if not controlled directly, used as feedforward if either course setpoint or airspeed_direction is finite.
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -4,7 +4,11 @@ pageClass: is-wide-page
|
||||
|
||||
# FixedWingLongitudinalSetpoint (UORB message)
|
||||
|
||||
Fixed Wing Longitudinal Setpoint message. Used by the fw_lateral_longitudinal_control module. If pitch_direct and throttle_direct are not both finite, then the controller relies on altitude/height_rate and equivalent_airspeed to control vertical motion. If both altitude and height_rate are NAN, the controller maintains the current altitude.
|
||||
Fixed Wing Longitudinal Setpoint message.
|
||||
|
||||
Used by the fw_lateral_longitudinal_control module
|
||||
If pitch_direct and throttle_direct are not both finite, then the controller relies on altitude/height_rate and equivalent_airspeed to control vertical motion.
|
||||
If both altitude and height_rate are NAN, the controller maintains the current altitude.
|
||||
|
||||
**TOPICS:** fixed_wing_longitudinal_setpoint
|
||||
|
||||
@@ -12,11 +16,11 @@ Fixed Wing Longitudinal Setpoint message. Used by the fw_lateral_longitudinal_co
|
||||
|
||||
| Name | Type | Unit [Frame] | Range/Enum | Description |
|
||||
| ------------------- | --------- | ------------ | ---------- | ---------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| altitude | `float32` | m | | Altitude setpoint AMSL, not controlled directly if NAN or if height_rate is finite |
|
||||
| height_rate | `float32` | ENU | | Scalar height rate setpoint. NAN if not controlled directly |
|
||||
| height_rate | `float32` | m/s [ENU] | | Scalar height rate setpoint. NAN if not controlled directly |
|
||||
| equivalent_airspeed | `float32` | m/s | [0 : inf] | Scalar equivalent airspeed setpoint. NAN if system default should be used |
|
||||
| pitch_direct | `float32` | FRD | [-pi : pi] | NAN if not controlled, overrides total energy controller |
|
||||
| pitch_direct | `float32` | rad [FRD] | [-pi : pi] | NAN if not controlled, overrides total energy controller |
|
||||
| throttle_direct | `float32` | norm | [0 : 1] | NAN if not controlled, overrides total energy controller |
|
||||
|
||||
## Constants
|
||||
@@ -33,18 +37,19 @@ Fixed Wing Longitudinal Setpoint message. Used by the fw_lateral_longitudinal_co
|
||||
|
||||
```c
|
||||
# Fixed Wing Longitudinal Setpoint message
|
||||
#
|
||||
# Used by the fw_lateral_longitudinal_control module
|
||||
# If pitch_direct and throttle_direct are not both finite, then the controller relies on altitude/height_rate and equivalent_airspeed to control vertical motion.
|
||||
# If both altitude and height_rate are NAN, the controller maintains the current altitude.
|
||||
|
||||
uint32 MESSAGE_VERSION = 0
|
||||
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
uint64 timestamp # [us] Time since system start
|
||||
|
||||
float32 altitude # [m] Altitude setpoint AMSL, not controlled directly if NAN or if height_rate is finite
|
||||
float32 height_rate # [m/s] [ENU] Scalar height rate setpoint. NAN if not controlled directly
|
||||
float32 height_rate # [m/s] [@frame ENU] Scalar height rate setpoint. NAN if not controlled directly
|
||||
float32 equivalent_airspeed # [m/s] [@range 0, inf] Scalar equivalent airspeed setpoint. NAN if system default should be used
|
||||
float32 pitch_direct # [rad] [@range -pi, pi] [FRD] NAN if not controlled, overrides total energy controller
|
||||
float32 pitch_direct # [rad] [@range -pi, pi] [@frame FRD] NAN if not controlled, overrides total energy controller
|
||||
float32 throttle_direct # [norm] [@range 0,1] NAN if not controlled, overrides total energy controller
|
||||
```
|
||||
|
||||
|
||||
@@ -4,24 +4,30 @@ pageClass: is-wide-page
|
||||
|
||||
# GotoSetpoint (UORB message)
|
||||
|
||||
Position and (optional) heading setpoints with corresponding speed constraints. Setpoints are intended as inputs to position and heading smoothers, respectively. Setpoints do not need to be kinematically consistent. Optional heading setpoints may be specified as controlled by the respective flag. Unset optional setpoints are not controlled. Unset optional constraints default to vehicle specifications.
|
||||
Position and (optional) heading setpoints with corresponding speed constraints.
|
||||
|
||||
Setpoints are intended as inputs to position and heading smoothers, respectively.
|
||||
Setpoints do not need to be kinematically consistent.
|
||||
Optional heading setpoints may be specified as controlled by the respective flag.
|
||||
Unset optional setpoints are not controlled.
|
||||
Unset optional constraints default to vehicle specifications.
|
||||
|
||||
**TOPICS:** goto_setpoint
|
||||
|
||||
## Fields
|
||||
|
||||
| Name | Type | Unit [Frame] | Range/Enum | Description |
|
||||
| ----------------------------- | ------------ | ------------ | ---------- | --------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| position | `float32[3]` | m | | NED local world frame |
|
||||
| ----------------------------- | ------------ | ------------ | ---------- | ---------------------------------------------------- |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| position | `float32[3]` | m [NED] | | NED local world frame |
|
||||
| flag_control_heading | `bool` | | | true if heading is to be controlled |
|
||||
| heading | `float32` | | | (optional) [rad] [-pi,pi] from North |
|
||||
| flag_set_max_horizontal_speed | `bool` | | | true if setting a non-default horizontal speed limit |
|
||||
| max_horizontal_speed | `float32` | | | (optional) [m/s] maximum speed (absolute) in the NE-plane |
|
||||
| max_horizontal_speed | `float32` | m/s | | (optional) Maximum speed (absolute) in the NE-plane |
|
||||
| flag_set_max_vertical_speed | `bool` | | | true if setting a non-default vertical speed limit |
|
||||
| max_vertical_speed | `float32` | | | (optional) [m/s] maximum speed (absolute) in the D-axis |
|
||||
| max_vertical_speed | `float32` | m/s | | (optional) Maximum speed (absolute) in the D-axis |
|
||||
| flag_set_max_heading_rate | `bool` | | | true if setting a non-default heading rate limit |
|
||||
| max_heading_rate | `float32` | | | (optional) [rad/s] maximum heading rate (absolute) |
|
||||
| max_heading_rate | `float32` | rad/s | | (optional) Maximum heading rate (absolute) |
|
||||
|
||||
## Constants
|
||||
|
||||
@@ -37,31 +43,32 @@ Position and (optional) heading setpoints with corresponding speed constraints.
|
||||
|
||||
```c
|
||||
# Position and (optional) heading setpoints with corresponding speed constraints
|
||||
# Setpoints are intended as inputs to position and heading smoothers, respectively
|
||||
# Setpoints do not need to be kinematically consistent
|
||||
# Optional heading setpoints may be specified as controlled by the respective flag
|
||||
# Unset optional setpoints are not controlled
|
||||
# Unset optional constraints default to vehicle specifications
|
||||
#
|
||||
# Setpoints are intended as inputs to position and heading smoothers, respectively.
|
||||
# Setpoints do not need to be kinematically consistent.
|
||||
# Optional heading setpoints may be specified as controlled by the respective flag.
|
||||
# Unset optional setpoints are not controlled.
|
||||
# Unset optional constraints default to vehicle specifications.
|
||||
|
||||
uint32 MESSAGE_VERSION = 0
|
||||
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
uint64 timestamp # [us] Time since system start
|
||||
|
||||
# setpoints
|
||||
float32[3] position # [m] NED local world frame
|
||||
float32[3] position # [m] [@frame NED] NED local world frame
|
||||
|
||||
bool flag_control_heading # true if heading is to be controlled
|
||||
float32 heading # (optional) [rad] [-pi,pi] from North
|
||||
|
||||
# constraints
|
||||
bool flag_set_max_horizontal_speed # true if setting a non-default horizontal speed limit
|
||||
float32 max_horizontal_speed # (optional) [m/s] maximum speed (absolute) in the NE-plane
|
||||
float32 max_horizontal_speed # [m/s] (optional) Maximum speed (absolute) in the NE-plane
|
||||
|
||||
bool flag_set_max_vertical_speed # true if setting a non-default vertical speed limit
|
||||
float32 max_vertical_speed # (optional) [m/s] maximum speed (absolute) in the D-axis
|
||||
float32 max_vertical_speed # [m/s] (optional) Maximum speed (absolute) in the D-axis
|
||||
|
||||
bool flag_set_max_heading_rate # true if setting a non-default heading rate limit
|
||||
float32 max_heading_rate # (optional) [rad/s] maximum heading rate (absolute)
|
||||
float32 max_heading_rate # [rad/s] (optional) Maximum heading rate (absolute)
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -4,7 +4,9 @@ pageClass: is-wide-page
|
||||
|
||||
# LateralControlConfiguration (UORB message)
|
||||
|
||||
Fixed Wing Lateral Control Configuration message. Used by the fw_lateral_longitudinal_control module to constrain FixedWingLateralSetpoint messages.
|
||||
Fixed Wing Lateral Control Configuration message.
|
||||
|
||||
Used by the fw_lateral_longitudinal_control module to constrain FixedWingLateralSetpoint messages.
|
||||
|
||||
**TOPICS:** lateral_control_configuration
|
||||
|
||||
@@ -12,8 +14,8 @@ Fixed Wing Lateral Control Configuration message. Used by the fw_lateral_longitu
|
||||
|
||||
| Name | Type | Unit [Frame] | Range/Enum | Description |
|
||||
| ----------------- | --------- | ------------ | ---------- | ---------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| lateral_accel_max | `float32` | m/s^2 | | currently maps to a maximum roll angle, accel_max = tan(roll_max) \* GRAVITY |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| lateral_accel_max | `float32` | m/s^2 | | Currently maps to a maximum roll angle, accel_max = tan(roll_max) \* GRAVITY |
|
||||
|
||||
## Constants
|
||||
|
||||
@@ -29,13 +31,14 @@ Fixed Wing Lateral Control Configuration message. Used by the fw_lateral_longitu
|
||||
|
||||
```c
|
||||
# Fixed Wing Lateral Control Configuration message
|
||||
#
|
||||
# Used by the fw_lateral_longitudinal_control module to constrain FixedWingLateralSetpoint messages.
|
||||
|
||||
uint32 MESSAGE_VERSION = 0
|
||||
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
uint64 timestamp # [us] Time since system start
|
||||
|
||||
float32 lateral_accel_max # [m/s^2] currently maps to a maximum roll angle, accel_max = tan(roll_max) * GRAVITY
|
||||
float32 lateral_accel_max # [m/s^2] Currently maps to a maximum roll angle, accel_max = tan(roll_max) * GRAVITY
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -4,7 +4,10 @@ pageClass: is-wide-page
|
||||
|
||||
# LongitudinalControlConfiguration (UORB message)
|
||||
|
||||
Fixed Wing Longitudinal Control Configuration message. Used by the fw_lateral_longitudinal_control module and TECS to constrain FixedWingLongitudinalSetpoint messages. and configure the resultant setpoints.
|
||||
Fixed Wing Longitudinal Control Configuration message.
|
||||
|
||||
Used by the fw_lateral_longitudinal_control module and TECS to constrain FixedWingLongitudinalSetpoint messages
|
||||
and configure the resultant setpoints.
|
||||
|
||||
**TOPICS:** longitudinal_control_configuration
|
||||
|
||||
@@ -12,16 +15,16 @@ Fixed Wing Longitudinal Control Configuration message. Used by the fw_lateral_lo
|
||||
|
||||
| Name | Type | Unit [Frame] | Range/Enum | Description |
|
||||
| ----------------------------- | --------- | ------------ | ---------- | ------------------------------------------------------------------------------------------------------------------------------------------------- |
|
||||
| timestamp | `uint64` | | | time since system start (microseconds) |
|
||||
| pitch_min | `float32` | rad | [-pi : pi] | defaults to FW_P_LIM_MIN if NAN. |
|
||||
| pitch_max | `float32` | rad | [-pi : pi] | defaults to FW_P_LIM_MAX if NAN. |
|
||||
| throttle_min | `float32` | norm | [0 : 1] | deaults to FW_THR_MIN if NAN. |
|
||||
| throttle_max | `float32` | norm | [0 : 1] | defaults to FW_THR_MAX if NAN. |
|
||||
| climb_rate_target | `float32` | m/s | | target climbrate to change altitude. Defaults to FW_T_CLIMB_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint. |
|
||||
| sink_rate_target | `float32` | m/s | | target sinkrate to change altitude. Defaults to FW_T_SINK_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint. |
|
||||
| speed_weight | `float32` | | [0 : 2] | , 0=pitch controls altitude only, 2=pitch controls airspeed only |
|
||||
| enforce_low_height_condition | `bool` | boolean | | if true, the altitude controller is configured with an alternative timeconstant for tighter altitude tracking |
|
||||
| disable_underspeed_protection | `bool` | boolean | | if true, underspeed handling is disabled in the altitude controller |
|
||||
| timestamp | `uint64` | us | | Time since system start |
|
||||
| pitch_min | `float32` | rad | [-pi : pi] | Defaults to FW_P_LIM_MIN if NAN. |
|
||||
| pitch_max | `float32` | rad | [-pi : pi] | Defaults to FW_P_LIM_MAX if NAN. |
|
||||
| throttle_min | `float32` | norm | [0 : 1] | Defaults to FW_THR_MIN if NAN. |
|
||||
| throttle_max | `float32` | norm | [0 : 1] | Defaults to FW_THR_MAX if NAN. |
|
||||
| climb_rate_target | `float32` | m/s | | Target climbrate to change altitude. Defaults to FW_T_CLIMB_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint. |
|
||||
| sink_rate_target | `float32` | m/s | | Target sinkrate to change altitude. Defaults to FW_T_SINK_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint. |
|
||||
| speed_weight | `float32` | | [0 : 2] | 0=pitch controls altitude only, 2=pitch controls airspeed only |
|
||||
| enforce_low_height_condition | `bool` | | | If true, the altitude controller is configured with an alternative timeconstant for tighter altitude tracking |
|
||||
| disable_underspeed_protection | `bool` | | | If true, underspeed handling is disabled in the altitude controller |
|
||||
|
||||
## Constants
|
||||
|
||||
@@ -37,22 +40,23 @@ Fixed Wing Longitudinal Control Configuration message. Used by the fw_lateral_lo
|
||||
|
||||
```c
|
||||
# Fixed Wing Longitudinal Control Configuration message
|
||||
#
|
||||
# Used by the fw_lateral_longitudinal_control module and TECS to constrain FixedWingLongitudinalSetpoint messages
|
||||
# and configure the resultant setpoints.
|
||||
|
||||
uint32 MESSAGE_VERSION = 0
|
||||
|
||||
uint64 timestamp # time since system start (microseconds)
|
||||
uint64 timestamp # [us] Time since system start
|
||||
|
||||
float32 pitch_min # [rad][@range -pi, pi] defaults to FW_P_LIM_MIN if NAN.
|
||||
float32 pitch_max # [rad][@range -pi, pi] defaults to FW_P_LIM_MAX if NAN.
|
||||
float32 throttle_min # [norm] [@range 0,1] deaults to FW_THR_MIN if NAN.
|
||||
float32 throttle_max # [norm] [@range 0,1] defaults to FW_THR_MAX if NAN.
|
||||
float32 climb_rate_target # [m/s] target climbrate to change altitude. Defaults to FW_T_CLIMB_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint.
|
||||
float32 sink_rate_target # [m/s] target sinkrate to change altitude. Defaults to FW_T_SINK_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint.
|
||||
float32 speed_weight # [@range 0,2], 0=pitch controls altitude only, 2=pitch controls airspeed only
|
||||
bool enforce_low_height_condition # [boolean] if true, the altitude controller is configured with an alternative timeconstant for tighter altitude tracking
|
||||
bool disable_underspeed_protection # [boolean] if true, underspeed handling is disabled in the altitude controller
|
||||
float32 pitch_min # [rad] [@range -pi, pi] Defaults to FW_P_LIM_MIN if NAN.
|
||||
float32 pitch_max # [rad] [@range -pi, pi] Defaults to FW_P_LIM_MAX if NAN.
|
||||
float32 throttle_min # [norm] [@range 0,1] Defaults to FW_THR_MIN if NAN.
|
||||
float32 throttle_max # [norm] [@range 0,1] Defaults to FW_THR_MAX if NAN.
|
||||
float32 climb_rate_target # [m/s] Target climbrate to change altitude. Defaults to FW_T_CLIMB_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint.
|
||||
float32 sink_rate_target # [m/s] Target sinkrate to change altitude. Defaults to FW_T_SINK_MAX if NAN. Not used if height_rate is directly set in FixedWingLongitudinalSetpoint.
|
||||
float32 speed_weight # [-] [@range 0,2] 0=pitch controls altitude only, 2=pitch controls airspeed only
|
||||
bool enforce_low_height_condition # If true, the altitude controller is configured with an alternative timeconstant for tighter altitude tracking
|
||||
bool disable_underspeed_protection # If true, underspeed handling is disabled in the altitude controller
|
||||
```
|
||||
|
||||
:::
|
||||
|
||||
@@ -22,12 +22,12 @@ Graphs showing how these are used [can be found here](../middleware/uorb_graph.m
|
||||
- [BatteryStatus](BatteryStatus.md) — Battery status.
|
||||
- [ConfigOverrides](ConfigOverrides.md) — Configurable overrides by (external) modes or mode executors.
|
||||
- [Event](Event.md) — Events interface.
|
||||
- [FixedWingLateralSetpoint](FixedWingLateralSetpoint.md) — Fixed Wing Lateral Setpoint message. Used by the fw_lateral_longitudinal_control module. At least one of course, airspeed_direction, or lateral_acceleration must be finite.
|
||||
- [FixedWingLongitudinalSetpoint](FixedWingLongitudinalSetpoint.md) — Fixed Wing Longitudinal Setpoint message. Used by the fw_lateral_longitudinal_control module. If pitch_direct and throttle_direct are not both finite, then the controller relies on altitude/height_rate and equivalent_airspeed to control vertical motion. If both altitude and height_rate are NAN, the controller maintains the current altitude.
|
||||
- [GotoSetpoint](GotoSetpoint.md) — Position and (optional) heading setpoints with corresponding speed constraints. Setpoints are intended as inputs to position and heading smoothers, respectively. Setpoints do not need to be kinematically consistent. Optional heading setpoints may be specified as controlled by the respective flag. Unset optional setpoints are not controlled. Unset optional constraints default to vehicle specifications.
|
||||
- [FixedWingLateralSetpoint](FixedWingLateralSetpoint.md) — Fixed Wing Lateral Setpoint message.
|
||||
- [FixedWingLongitudinalSetpoint](FixedWingLongitudinalSetpoint.md) — Fixed Wing Longitudinal Setpoint message.
|
||||
- [GotoSetpoint](GotoSetpoint.md) — Position and (optional) heading setpoints with corresponding speed constraints.
|
||||
- [HomePosition](HomePosition.md) — GPS home position in WGS84 coordinates.
|
||||
- [LateralControlConfiguration](LateralControlConfiguration.md) — Fixed Wing Lateral Control Configuration message. Used by the fw_lateral_longitudinal_control module to constrain FixedWingLateralSetpoint messages.
|
||||
- [LongitudinalControlConfiguration](LongitudinalControlConfiguration.md) — Fixed Wing Longitudinal Control Configuration message. Used by the fw_lateral_longitudinal_control module and TECS to constrain FixedWingLongitudinalSetpoint messages. and configure the resultant setpoints.
|
||||
- [LateralControlConfiguration](LateralControlConfiguration.md) — Fixed Wing Lateral Control Configuration message.
|
||||
- [LongitudinalControlConfiguration](LongitudinalControlConfiguration.md) — Fixed Wing Longitudinal Control Configuration message.
|
||||
- [ManualControlSetpoint](ManualControlSetpoint.md)
|
||||
- [ModeCompleted](ModeCompleted.md) — Mode completion result, published by an active mode. The possible values of nav_state are defined in the VehicleStatus msg. Note that this is not always published (e.g. when a user switches modes or on. failsafe activation).
|
||||
- [RaptorInput](RaptorInput.md) — Raptor Input.
|
||||
|
||||
Reference in New Issue
Block a user