DocumentCode :
2252616
Title :
T-S fuzzy control for a quad-rotor UAV
Author :
Mao, Xiang ; Zhang, Hongbin ; Han, Dongfei
Author_Institution :
University of Electronic Science and Technology of China, Chengdu 611731, P.R. China
fYear :
2015
fDate :
28-30 July 2015
Firstpage :
3617
Lastpage :
3622
Abstract :
This paper investigates the problem of the position and attitude control of quad-rotor UAV. A new simplified model which is more reasonable for some actual cases is derived. Based on the simplified model, a T-S fuzzy state feedback controller to stabilize the attitude of quad-rotor UAV is designed. Proposed control strategy can steer quad-rotor UAV flight with a desired acceleration. In addition, it can guarantee the assumption for simplifying quad-rotor model is reasonable during the flight. Finally, numerical simulations are provided to illustrate the effectiveness of the obtained theoretical results.
Keywords :
Acceleration; Attitude control; Mathematical model; PD control; Position control; Rotors; Simulation; Quad-rotor; Simplified Model; T-S Fuzzy Control; UAV;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2015 34th Chinese
Conference_Location :
Hangzhou, China
Type :
conf
DOI :
10.1109/ChiCC.2015.7260198
Filename :
7260198
Link To Document :
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