DocumentCode
2777560
Title
Fuzzy self-tuning gain scheduled control design for an autopilot missile
Author
Tabatabaei, Sajad ; Tohidi, Shahab-o-din ; Sadeghi, Mokhtar Sha ; Mirjafari, Parinaz Sadat
fYear
2010
fDate
5-8 Dec. 2010
Firstpage
197
Lastpage
201
Abstract
The paper presents the lateral acceleration control design of a missile model in which the parameters of fuzzy logic are designed to optimize the performance characteristics of the plant. The control scheme utilizes three fuzzy controllers to achieve the performances for lateral acceleration. The control scheme is based on classical compensator which its parameters are self-tuned by fuzzy logic. The simulation results show that the designed fuzzy self-tuning gain scheduled controller has excellent performance.
Keywords
acceleration control; control system synthesis; fuzzy control; missile control; autopilot missile; compensator; fuzzy control; fuzzy logic parameter; lateral acceleration control design; self-tuning gain scheduled control; Acceleration; Accelerometers; Aerodynamics; Control systems; Fuzzy logic; Mathematical model; Missiles; Fuzzy Control; Gain Scheduled Control; Lateral Acceleration Control; Missile control;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Applications and Industrial Electronics (ICCAIE), 2010 International Conference on
Conference_Location
Kuala Lumpur
Print_ISBN
978-1-4244-9054-7
Type
conf
DOI
10.1109/ICCAIE.2010.5735074
Filename
5735074
Link To Document