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 :
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