DocumentCode
3344889
Title
Attitude control system design of a helicopter experimental system
Author
Inoue, Akira ; Deng, Mingcong ; Harima, Takanori ; Nakao, Seiji ; Ueki, Nobuyuki
Author_Institution
Dept. Syst. Eng., Okayama Univ.
fYear
2005
fDate
14-17 Dec. 2005
Firstpage
1240
Lastpage
1245
Abstract
In this paper, we consider the problem of attitude control of a helicopter experimental system. We design a nonlinear controller which combines nonlinear adaptive robust control and nonlinear feedback controls. Simulation and experimental results show the effectiveness of the proposed method
Keywords
adaptive control; aircraft control; control system synthesis; feedback; helicopters; nonlinear control systems; robust control; attitude control system; helicopter experimental system; nonlinear adaptive robust control; nonlinear controller; nonlinear feedback controls; Adaptive control; Control systems; Equations; Helicopters; Nonlinear control systems; Parameter estimation; Programmable control; Sliding mode control; Tail; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Technology, 2005. ICIT 2005. IEEE International Conference on
Conference_Location
Hong Kong
Print_ISBN
0-7803-9484-4
Type
conf
DOI
10.1109/ICIT.2005.1600825
Filename
1600825
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