DocumentCode
300462
Title
Linear matrix inequalities in integrated aircraft/controller design
Author
Niewhoener, Robert J. ; Kaminer, Ido
Author_Institution
US Navy, USA
Volume
1
fYear
1995
fDate
21-23 Jun 1995
Firstpage
177
Abstract
This paper presents a new methodology to solve the problem of optimizing the plant parameters, such as control surface sizes of aircraft, while meeting open and closed-loop static and dynamic performance requirements. The basic approach is to rewrite the performance specifications as linear matrix inequalities
Keywords
aircraft control; control engineering; control system synthesis; design engineering; matrix algebra; optimisation; closed-loop performance requirements; control surface sizes; dynamic performance requirements; integrated aircraft/controller design; linear matrix inequalities; open-loop performance requirements; plant parameter optimization; static performance requirements; Aerodynamics; Aerospace control; Aerospace engineering; Aircraft propulsion; Control systems; Cost function; Design engineering; Linear matrix inequalities; Size control; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, Proceedings of the 1995
Conference_Location
Seattle, WA
Print_ISBN
0-7803-2445-5
Type
conf
DOI
10.1109/ACC.1995.529232
Filename
529232
Link To Document