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 :
https://search.ricest.ac.ir/dl/search/defaultta.aspx?DTC=49&DC=3550550
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