DocumentCode
2848849
Title
A parameter-dependent performance criterion for linear parameter-varying systems
Author
Lee, Lawton H. ; Spillman, Mark
Author_Institution
Lockheed Martin Missiles & Space, Sunnyvale, CA, USA
Volume
2
fYear
1997
fDate
10-12 Dec 1997
Firstpage
984
Abstract
Existing control theory for linear parameter-varying systems uses a uniform-in-the-parameters upper bound (a constant scalar) on the induced-L2 norm. In this paper, this constant is generalized to a function of the parameters; the performance criterion generalizes to an integral quadratic constraint and implies a norm bound that depends naturally on the real-time parameter trajectory. As in existing theory, the synthesis problem reduces to convex optimization involving linear matrix inequalities. A motivating example, gain-scheduled flight control of the F-16 VISTA, demonstrates the flexibility gained by incorporating the new performance criterion
Keywords
control system synthesis; matrix algebra; optimal control; performance index; time-varying systems; F-16 VISTA; LMI; control synthesis; convex optimization; gain-scheduled flight control; induced-L2 norm; integral quadratic constraint; linear matrix inequalities; linear parameter-varying systems; parameter-dependent performance criterion; real-time parameter trajectory; uniform-in-the-parameters upper bound; Aerospace control; Control theory; Dynamic scheduling; Ear; Linear matrix inequalities; Missiles; Nonlinear control systems; Performance analysis; Time varying systems; Upper bound;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1997., Proceedings of the 36th IEEE Conference on
Conference_Location
San Diego, CA
ISSN
0191-2216
Print_ISBN
0-7803-4187-2
Type
conf
DOI
10.1109/CDC.1997.657572
Filename
657572
Link To Document