DocumentCode :
391382
Title :
Reliable aircraft tracking control via quadratic parameter-dependent Lyapunov functions: state feedback case
Author :
Liao, Fang ; Wang, Jian Liang ; Yang, Guang Hang
Author_Institution :
Sch. of Electr. & Electron. Eng., Nanyang Technol. Univ., Singapore, Singapore
Volume :
4
fYear :
2002
fDate :
10-13 Dec. 2002
Firstpage :
4474
Abstract :
This paper investigates the reliable tracking problem against aircraft control surface impairment. A new analysis and synthesis methods of reliable tracking control using quadratic parameter-dependent Lyapunov functions are provided in the term of solvability of iterative linear matrix inequalities. The proposed method has less conservativeness than that via the common (parameter-independent) Lyapunov function, which is demonstrated by an aircraft example.
Keywords :
Lyapunov methods; aircraft control; linear matrix inequalities; optimal control; robust control; state feedback; tracking; H2 tracking; aircraft control; exponential stability; iterative linear matrix inequality; quadratic parameter dependent Lyapunov functions; reliable tracking; robust tracking; state feedback; Actuators; Aerospace control; Aircraft; Computer aided software engineering; Control systems; Design methodology; Lyapunov method; Robust control; Robust stability; State feedback;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
ISSN :
0191-2216
Print_ISBN :
0-7803-7516-5
Type :
conf
DOI :
10.1109/CDC.2002.1185078
Filename :
1185078
Link To Document :
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