DocumentCode
1900798
Title
Nonlinear performance of a PI controlled missile: an explanation
Author
Fromion, Vincent ; Scorletti, Gerard ; Ferreres, Gilles
Author_Institution
Rome Univ., Italy
Volume
5
fYear
1997
fDate
10-12 Dec 1997
Firstpage
4198
Abstract
Considers the practical interest of an approach to nonlinear system analysis. Based on the incremental norm, this approach proposes performance and robustness analysis criteria. Using computationally efficient tests involving linear matrix inequality optimization, these criteria enable us to guarantee the performance and the robustness of a realistic PI controlled nonlinear missile
Keywords
control system analysis; matrix algebra; missile control; nonlinear control systems; optimisation; robust control; two-term control; PI controlled missile; incremental norm; linear matrix inequality optimization; nonlinear performance; nonlinear system analysis; robustness analysis criteria; Aerodynamics; Control nonlinearities; Control systems; Missiles; Nonlinear control systems; Performance analysis; Robust control; Robustness; Steady-state; Testing;
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.1997.649492
Filename
649492
Link To Document