DocumentCode :
2065516
Title :
A modal multimodel approach for controller order reduction and structuration
Author :
Chiappa, C. ; Magni, Jean-Franqois ; Gorrec, Yann Le
Author_Institution :
SUPAERO, Toulouse, France
fYear :
2001
fDate :
2001
Firstpage :
1156
Lastpage :
1161
Abstract :
This paper proposes a new design procedure aimed at controller order reduction and structuration. Our main objective is order reduction. However, the proposed method also allows the designer to take controller structuration into account (e.g. nullity of some feedback transfers, roll off and stop band properties). Such a method can be particularly advantageous for redesigning lower order and structured versions of H2/H or μ controllers which are known to be of very high order. The proposed method is based on the multi-model modal theory and is validated with a realistic example of flexible aircraft control law design
Keywords :
H control; aircraft control; control system synthesis; eigenstructure assignment; feedback; linear systems; reduced order systems; H control; eigenstructure assignment; feedback; flexible aircraft control; linear system; modal control; modal multimodel; optimal control; order reduction; structuration; Aerodynamics; Aerospace control; Control system synthesis; Control systems; Feedback; Filters; Hydrogen; Robust control; Robustness; Size control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Applications, 2001. (CCA '01). Proceedings of the 2001 IEEE International Conference on
Conference_Location :
Mexico City
Print_ISBN :
0-7803-6733-2
Type :
conf
DOI :
10.1109/CCA.2001.974028
Filename :
974028
Link To Document :
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