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.
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;
Conference_Titel :
Industrial Technology, 2005. ICIT 2005. IEEE International Conference on
Conference_Location :
Hong Kong
Print_ISBN :
0-7803-9484-4
DOI :
10.1109/ICIT.2005.1600825
