Control Loss Recovery Autopilot Design for Fixed-Wing Aircraft
IFAC-PapersOnLine, cilt.49, sa.9, ss.117-123, 2016 (Scopus)
- Yayın Türü: Makale / Özet
- Cilt numarası: 49 Sayı: 9
- Basım Tarihi: 2016
- Doi Numarası: 10.1016/j.ifacol.2016.07.509
- Dergi Adı: IFAC-PapersOnLine
- Derginin Tarandığı İndeksler: Scopus
- Sayfa Sayıları: ss.117-123
- Anahtar Kelimeler: autopilot design, Loop-shaping, loss of control, numerical simulation, power loss, surface jam
- Ankara Yıldırım Beyazıt Üniversitesi Adresli: Hayır
Özet
© 2016In this paper a loop-shaping design approach is investigated for distressed fixed-wing aircraft experiencing control loss due to surface or power failure. An accurate nonlinear model of the aircraft dynamics is utilized to obtain a target aircraft behavior in the emergency situation, for which a loop-shaping controller is designed to balance performance and robustness, and to decouple different command channels. A rudder servoactuator jam scenario is presented as an example where it is seen that the autopilot recovers level flight and responds well to fly-by-wire commands from the operator.