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|Title:||Design of a flight stabilizer system and automatic control using HIL test platform||Authors:||Akyürek, Şeyma
Özden, G. S.
|Issue Date:||2016||Publisher:||International Journal Of Mechanical Engineering And Robotics Research||Source:||Akyürek, S., Özden, G. S., Atlas, E., Kasnakoglu, C., & Kaynak, Ü. (2016). Design of a flight stabilizer system and automatic control using HIL test platform. International Journal of Mechanical Engineering and Robotics Research, 5(1), 77.||Abstract:||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. © 2016 Int. J. Mech. Eng. Rob. Res.||URI:||http://www.ijmerr.com/index.php?m=content&c=index&a=show&catid=140&id=725
|Appears in Collections:||Elektrik ve Elektronik Mühendisliği Bölümü / Department of Electrical & Electronics Engineering|
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
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