VehicleAttitudeSetpoint.msg: remove reset_integral and fw_control_yaw_wheel

Signed-off-by: Silvan <silvan@auterion.com>

msg/px4_msgs_old/msg/VehicleAttitudeSetpointV0.msg

@@ -0,0 +1,18 @@
+uint32 MESSAGE_VERSION = 0
+
+uint64 timestamp		# time since system start (microseconds)
+
+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.
+# For fixed wings thrust_x is the throttle demand and thrust_y, thrust_z will usually be zero.
+float32[3] thrust_body		# Normalized thrust command in body FRD 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