Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/1322
Title: Design of a Flight Stabilizer System and Automatic Control Using Hil Test Platform
Authors: Akyürek, Şeyma
Özden, G. S.
Atlas, E.
Kasnakoğlu, Coşku
Kaynak, Ünver
Keywords: Autopilot
Flight control
Hardware-In-the-Loop
MIMO
PID controller
SISO
UAV
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
https://hdl.handle.net/20.500.11851/1322
ISSN: 22780149
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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