forked from Archive/PX4-Autopilot
sync attitude setpoint messages
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@ -15,14 +15,9 @@ float32 yaw_body # body angle in NED frame
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float32 yaw_sp_move_rate # rad/s (commanded by user)
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float32[9] R_body # Rotation matrix describing the setpoint as rotation from the current body frame
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bool R_valid # Set to true if rotation matrix is valid
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# For quaternion-based attitude control
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float32[4] q_d # Desired quaternion for quaternion control
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bool q_d_valid # Set to true if quaternion vector is valid
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float32[4] q_e # Attitude error in quaternion
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bool q_e_valid # Set to true if quaternion error vector is valid
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float32 thrust # Thrust in Newton the power system should generate
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@ -35,5 +30,7 @@ bool disable_mc_yaw_control # control yaw for mc (used for vtol weather-vane m
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bool apply_flaps
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float32 landing_gear
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# WAS vehicle_attitude_setpoint mc_virtual_attitude_setpoint fw_virtual_attitude_setpoint
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# TOPICS fw_virtual_attitude_setpoint
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@ -15,14 +15,9 @@ float32 yaw_body # body angle in NED frame
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float32 yaw_sp_move_rate # rad/s (commanded by user)
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float32[9] R_body # Rotation matrix describing the setpoint as rotation from the current body frame
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bool R_valid # Set to true if rotation matrix is valid
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# For quaternion-based attitude control
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float32[4] q_d # Desired quaternion for quaternion control
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bool q_d_valid # Set to true if quaternion vector is valid
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float32[4] q_e # Attitude error in quaternion
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bool q_e_valid # Set to true if quaternion error vector is valid
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float32 thrust # Thrust in Newton the power system should generate
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@ -35,5 +30,7 @@ bool disable_mc_yaw_control # control yaw for mc (used for vtol weather-vane m
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bool apply_flaps
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float32 landing_gear
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# WAS vehicle_attitude_setpoint mc_virtual_attitude_setpoint fw_virtual_attitude_setpoint
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# TOPICS mc_virtual_attitude_setpoint
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