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