DocumentCode
1828355
Title
A velocity feedback fuzzy logic controller for stable hovering of a quad rotor UAV
Author
Abeywardena, D.M.W. ; Amaratunga, L.A.K. ; Shakoor, S.A.A. ; Munasinghe, S.R.
Author_Institution
Dept. of Electron. & Telecommun., Univ. of Moratuwa, Moratuwa, Sri Lanka
fYear
2009
fDate
28-31 Dec. 2009
Firstpage
558
Lastpage
562
Abstract
Quad Rotor unmanned aerial vehicle (UAV) is an aerial vehicle platform which has drawn much attention in the recent past due to its simple yet unique design. Despite the simplicity in the hardware, the vehicle is inherently unstable, and many control strategies have been proposed to achieve stability and control of the quad rotor platform. This paper presents a Fuzzy Logic based design to stabilize and control the quad rotor UAV. The fuzzy controller was designed and simulated along with a non-linear dynamic model of the quad rotor UAV. The fuzzy controller was then used to achieve stable hovering of the quad rotor UAV, amidst velocity disturbances. The simulation results show that stable hovering conditions can be achieved with the designed controller.
Keywords
aerospace control; aerospace robotics; control system synthesis; feedback; fuzzy control; fuzzy logic; nonlinear control systems; remotely operated vehicles; fuzzy controller; nonlinear dynamic model; quad rotor UAV stable hovering; quad rotor platform control; quad rotor platform stability; quad rotor unmanned aerial vehicle; velocity feedback fuzzy logic controller; Feedback; Fuzzy control; Fuzzy logic; Mathematical model; Mechanical variables control; Propellers; Stability; Unmanned aerial vehicles; Vehicle dynamics; Velocity control;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial and Information Systems (ICIIS), 2009 International Conference on
Conference_Location
Sri Lanka
Print_ISBN
978-1-4244-4836-4
Electronic_ISBN
978-1-4244-4837-1
Type
conf
DOI
10.1109/ICIINFS.2009.5429800
Filename
5429800
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