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
Link To Document :
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