Taylor, Brian2014-07-282014-07-282014-07-28https://hdl.handle.net/11299/164228Thor flight 60 included the altitude/airspeed hold, and consisted of the same maneuvers as flight 59, in addition to three cases of simple straight and level flight. The airplane maintained airspeed within +/- 3 meters during straight and level flight, and +/- 5 meters during maneuvers. Software modules used were steady_level_tracker, alt_speed_test, EKF_15stateThorFlightControlLawsAnokaACRCAltitudeAirspeedTrackingOther