Modeling and control of a new tilt-wing unmanned aerial vehicle SUAVI

Öner, Kaan Taha and Çetinsoy, Ertuğrul and Sırımoğlu, Efe and Hançer, Cevdet and Ayken, Taylan and Ünel, Mustafa and Akşit, Mahmut Faruk and Gülez, Kayhan and Kandemir, İlyas (2009) Modeling and control of a new tilt-wing unmanned aerial vehicle SUAVI. (Accepted/In Press)

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Abstract

This paper presents a new quad-rotor aerial vehicle with a tilt-wing mechanism. The vehicle is capable of take-off/landing in vertical flight mode (VTOL) and flying over long distances in horizontal flight mode. The dynamic model of the vehicle is obtained using Newton-Euler formulation. An LQR control scheme is applied to the dynamic model in simulation environment for position and full range yaw control of the vehicle. Besides, a PID controller is designed for attitude and altitude stabilization of the vehicle. The performance of the PID controller is verified with simulations and experiments.
Item Type: Article
Divisions: Faculty of Engineering and Natural Sciences
Depositing User: Mustafa Ünel
Date Deposited: 22 Dec 2009 09:42
Last Modified: 24 Jul 2019 14:35
URI: https://research.sabanciuniv.edu/id/eprint/13598

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