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
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;
Conference_Titel :
Computer Applications and Industrial Electronics (ICCAIE), 2010 International Conference on
Conference_Location :
Kuala Lumpur
Print_ISBN :
978-1-4244-9054-7
DOI :
10.1109/ICCAIE.2010.5735074
