▸ AirSTARis a UAS designed for flight dynamics and control research ▸ Allows control law injection in-line with internal research pilot commands ▸ Project development in a series of phases • Developed project UAV/RC experience • Developed LaRC policies and procedures ▸ Phase-III utilized a commercial-of-the-shelf (COTS) airframe ▸ Phase-IV flew a 5.5% dynamically scaled generic transport model (GTM) aircraft.
Expanding AirSTAR capability in an existing avionics design
01.10.2012
2368310 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
L~1 Adaptive Control Design for NASA AirSTAR Flight Test Vehicle
British Library Conference Proceedings | 2009
|