Mathematical modeling and vertical flight control of a tilt-wing UAV

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Öner, Kaan Taha and Çetinsoy, Ertuğrul and Sırımoğlu, Efe and Hançer, Cevdet and Ünel, Mustafa and Akşit, Mahmut Faruk and Gülez, Kayhan and Kandemir, İlyas (2012) Mathematical modeling and vertical flight control of a tilt-wing UAV. Turkish Journal of Electrical Engineering & Computer Sciences, 20 (1). pp. 149-157. ISSN 1300-0632

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Official URL: http://dx.doi.org/10.3906/elk-1007-624


This paper presents a mathematical model and vertical flight control algorithms for a new tilt-wing unmanned aerial vehicle (UAV). The vehicle is capable of vertical take-off and landing (VTOL). Due to its tilt-wing structure, it can also fly horizontally. The mathematical model of the vehicle is obtained using Newton-Euler formulation. A gravity compensated PID controller is designed for altitude control, and three PID controllers are designed for attitude stabilization of the vehicle. Performances of these controllers are found to be quite satisfactory as demonstrated by indoor and outdoor flight experiments.

Item Type:Article
Uncontrolled Keywords:Tilt-wing, quadrotor, PID, VTOL, hover
Subjects:T Technology > TK Electrical engineering. Electronics Nuclear engineering
T Technology > TL Motor vehicles. Aeronautics. Astronautics
ID Code:18609
Deposited By:Mustafa Ünel
Deposited On:23 Dec 2011 15:10
Last Modified:31 Jul 2019 09:49

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