Dynamic model and control of a new quadrotor unmanned aerial vehicle with tilt-wing mechanism

Öner, Kaan Taha and Çetinsoy, Ertuğrul and Ünel, Mustafa and Akşit, Mahmut Faruk and Kandemir, İlyas and Gülez, Kayhan (2008) Dynamic model and control of a new quadrotor unmanned aerial vehicle with tilt-wing mechanism. In: ICCARV 2008 : "International Conference on Control, Automation, Robotics and Vision", Paris, France

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Abstract

In this work a dynamic model of a new quadrotor aerial vehicle that is equipped with a tilt-wing mechanism is presented. The vehicle has the capabilities of vertical take-off/landing (VTOL) like a helicopter and flying horizontal like an airplane. Dynamic model of the vehicle is derived both for vertical and horizontal flight modes using Newton-Euler formulation. An LQR controller for the vertical flight mode has also been developed and its performance has been tested with several simulations.

Item Type:	Papers in Conference Proceedings
Uncontrolled Keywords:	Control, Dynamic model, LQR, Quadrotor, Tilt-wing, VTOL
Subjects:	T Technology > TJ Mechanical engineering and machinery T Technology > TA Engineering (General). Civil engineering (General)
ID Code:	11198
Deposited By:	Mahmut Faruk Akşit
Deposited On:	24 Dec 2008 10:55
Last Modified:	12 Nov 2009 14:22

Available Versions of this Item

Modeling and position control of a new quad-rotor unmanned aerial vehicle with tilt-wing mechanism. (deposited 31 Oct 2008 09:31)
- Dynamic model and control of a new quadrotor unmanned aerial vehicle with tilt-wing mechanism. (deposited 24 Dec 2008 10:55) [Currently Displayed]

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