VehicleAttitudeSetpoint (повідомлення UORB)
c
uint64 timestamp # time since system start (microseconds)
float32 roll_body # body angle in NED frame (can be NaN for FW)
float32 pitch_body # body angle in NED frame (can be NaN for FW)
float32 yaw_body # body angle in NED frame (can be NaN for FW)
float32 yaw_sp_move_rate # rad/s (commanded by user)
# For quaternion-based attitude control
float32[4] q_d # Desired quaternion for quaternion control
# For clarification: For multicopters thrust_body[0] and thrust[1] are usually 0 and thrust[2] is the negative throttle demand.
# Для фіксованих крил thrust_x - це запит ручки газу, а thrust_y, thrust_z зазвичай буде нульовими.
float32[3] thrust_body # Normalized thrust command in body NED frame [-1,1]
bool reset_integral # Reset roll/pitch/yaw integrals (navigation logic change)
bool fw_control_yaw_wheel # control heading with steering wheel (used for auto takeoff on runway)
# TOPICS vehicle_attitude_setpoint mc_virtual_attitude_setpoint fw_virtual_attitude_setpoint