, speed V=%d /velocities/airspeed-kt heading H=%02d /orientation/heading-deg 57.29578 altitiude A=%02d /position/altitiude-ft rate of climb R=%02d /velocities/vertical-speed-fps pitch angle P=%05.1f float /orientation/pitch-deg bank angle B=%05.1f float /orientation/roll-deg engine E=%02d; /engines/engine[0]/rpm