added option for direct yaw control with rudder for fixed wing

10 years ago · 20ec727d9f
1 changed files with 2 additions and 0 deletions
--- 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
				@@ -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)