Title :
An optimization approach to integrated aircraft-controller design
Author :
Yang, Guang-hong ; Lum, Kai-Yew
Author_Institution :
National University of Singapore
Keywords :
Aerospace control; Aircraft; Constraint optimization; Control systems; Design optimization; Iterative algorithms; Linear feedback control systems; Linear matrix inequalities; Size control; Sufficient conditions;
Conference_Titel :
American Control Conference, 2003. Proceedings of the 2003
Print_ISBN :
0-7803-7896-2
DOI :
10.1109/ACC.2003.1239829