Design of a flight stabilizer system and automatic control using HIL test platform

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Akyürek Ş., Özden G. S., Atlas E., Kasnakoğlu C., Kaynak Ü.

International Journal of Mechanical Engineering and Robotics Research, cilt.5, sa.1, ss.77-81, 2016 (Scopus)

• Yayın Türü: Makale / Tam Makale
• Cilt numarası: 5 Sayı: 1
• Basım Tarihi: 2016
• Doi Numarası: 10.18178/ijmerr.5.1.77-81
• Dergi Adı: International Journal of Mechanical Engineering and Robotics Research
• Derginin Tarandığı İndeksler: Scopus
• Sayfa Sayıları: ss.77-81
• Anahtar Kelimeler: Autopilot, Flight control, Hardware-In-the-Loop, MIMO, PID controller, SISO, UAV
• Ankara Yıldırım Beyazıt Üniversitesi Adresli: Hayır

Özet

© 2016 Int. J. Mech. Eng. Rob. Res.In this paper a Hardware-In-the-Loop (HIL) test platform is used to design a flight stabilization system for Unmanned Aerial Vehicles (UAV). Controllers are first designed and tested separately for lateral and longitudinal axes using numerical simulations, and later these controllers are merged on the HIL platform. It is observed that the resulting controller successfully stabilizes the aircraft to achieve straight and level flight.