Modeling and position control of a new quad-rotor unmanned aerial vehicle with tilt-wing mechanism

Warning The system is temporarily closed to updates for reporting purpose.

Öner, Kaan Taha and Çetinsoy, Ertuğrul and Ünel, Mustafa and Akşit, Mahmut Faruk and Kandemir, İlyas and Gülez, Kayhan (2008) Modeling and position control of a new quad-rotor unmanned aerial vehicle with tilt-wing mechanism. In: International Conference on Control, Automation, Robotics and Vision (ICCARV'08), Laval, France (Accepted/In Press)

Warning
There is a more recent version of this item available.
[thumbnail of ICCARV08.pdf] PDF
ICCARV08.pdf

Download (1MB)

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.
Divisions: Faculty of Engineering and Natural Sciences
Depositing User: Mustafa Ünel
Date Deposited: 31 Oct 2008 09:31
Last Modified: 26 Apr 2022 08:47
URI: https://research.sabanciuniv.edu/id/eprint/9847

Available Versions of this Item

Actions (login required)

View Item
View Item