DocumentCode :
2202143
Title :
An optimization approach to integrated aircraft-controller design
Author :
Yang, Guang-hong ; Lum, Kai-Yew
Author_Institution :
National University of Singapore
Volume :
2
fYear :
2003
fDate :
June 4-6, 2003
Firstpage :
1649
Lastpage :
1654
Keywords :
Aerospace control; Aircraft; Constraint optimization; Control systems; Design optimization; Iterative algorithms; Linear feedback control systems; Linear matrix inequalities; Size control; Sufficient conditions;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2003. Proceedings of the 2003
ISSN :
0743-1619
Print_ISBN :
0-7803-7896-2
Type :
conf
DOI :
10.1109/ACC.2003.1239829
Filename :
1239829
Link To Document :
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