common.xml Different flight modes Gliding mode with motors off Autonomous flight RC controlled Position estimate of the observer in global frame Longitude expressed in 1E7 Latitude expressed in 1E7 Altitude expressed in milimeters velocity estimate of the observer in NED inertial frame Velocity attitude estimate of the observe Quaternion re;im Wind estimate in NED inertial frame Wind Estimate of the air velocity Air speed angle of attack slip angle IMU biases accelerometer bias gyroscope bias estimate of the pressure at sea level Wind ambient air temperature Air Temperatur filtered rotational velocity rotational velocity low level control output Servo signal motor signal Power managment current power consumption battery status Power generation from each module system status gps status actuator status module status module status change commanded air speed Target ID commanded airspeed accept change of airspeed commanded airspeed 0:ack, 1:nack