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