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vehicle_attitude_setpoint: get rid of unused q_d_valid flag
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@@ -8,7 +8,6 @@ float32 yaw_sp_move_rate # rad/s (commanded by user)
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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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# For clarification: For multicopters thrust_body[0] and thrust[1] are usually 0 and thrust[2] is the negative throttle demand.
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# For fixed wings thrust_x is the throttle demand and thrust_y, thrust_z will usually be zero.
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