DocumentCode
3550550
Title
Fuzzy gain-scheduled missile autopilot design using evolutionary algorithms
Author
Sreenuch, T. ; Tsourdos, A. ; Hughes, E.J. ; White, B.A.
Author_Institution
Dept. of Aerosp., Power & Sensors, Cranfield Univ., Swindon, UK
fYear
2005
fDate
June 8-10, 2005
Firstpage
346
Lastpage
351
Keywords
closed loop systems; control system synthesis; evolutionary computation; fuzzy control; fuzzy systems; missile guidance; optimisation; piecewise linear techniques; poles and zeros; robust control; closed loop system; evolutionary algorithms; fuzzy controller; fuzzy gain-scheduled missile autopilot; fuzzy rule optimization; gain function shape variation; gain surface; lateral acceleration control; missile model; nonlinear fixed-structure-like controller; optimal decomposition; perturbation vertices; robust tracking controller; singleton fuzzy model; Acceleration; Algorithm design and analysis; Control systems; Evolutionary computation; Fuzzy control; Fuzzy sets; Fuzzy systems; Missiles; Optimal control; Shape;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2005. Proceedings of the 2005
ISSN
0743-1619
Print_ISBN
0-7803-9098-9
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2005.1469957
Filename
1469957
Link To Document