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Commit 20ec727d authored by tumbili's avatar tumbili Committed by Roman
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added option for direct yaw control with rudder for fixed wing

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msg/vehicle_attitude_setpoint.msg
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......@@ -21,3 +21,5 @@ float32 thrust # Thrust in Newton the power system should generate
bool roll_reset_integral # Reset roll integral part (navigation logic change)
bool pitch_reset_integral # Reset pitch integral part (navigation logic change)
bool yaw_reset_integral # Reset yaw integral part (navigation logic change)
bool fw_control_yaw # control heading with rudder (used for auto takeoff on runway)
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