DocumentCode
2177913
Title
Flight control design using extended state observer and non-smooth feedback
Author
Huang, Yi ; Xu, Kekang ; Han, Jingqing ; Lam, James
Volume
1
fYear
2001
fDate
2001
Firstpage
223
Abstract
This paper proposes a novel nonlinear approach for high performance flight control design. The dynamic linearization is accomplished via a kind of unknown input observer, called extended state observer. A nonsmooth feedback law is employed to achieve the desirable dynamic performances. A Lyapunov function is constructed for the proposed method
Keywords
Lyapunov methods; aircraft control; control system synthesis; feedback; linearisation techniques; observers; Lyapunov function; dynamic linearization; extended state observer; flight control design; nonlinear high-performance flight control design; nonsmooth feedback; unknown input observer; Acceleration; Aerodynamics; Aerospace control; Aircraft manufacture; Angular velocity; Couplings; Lyapunov method; Mechanical engineering; Robust control; State feedback;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2001. Proceedings of the 40th IEEE Conference on
Conference_Location
Orlando, FL
Print_ISBN
0-7803-7061-9
Type
conf
DOI
10.1109/.2001.980102
Filename
980102
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