diff --git a/msg/vehicle_attitude_setpoint.msg b/msg/vehicle_attitude_setpoint.msg
index 7bbb670b31..3bbb5efa7b 100644
--- a/msg/vehicle_attitude_setpoint.msg
+++ b/msg/vehicle_attitude_setpoint.msg
@@ -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)