DocumentCode :
2670250
Title :
Fuzzy logical guidance based on particle swarm optimized parameters
Author :
Ting, Fang ; Delin, Luo ; Zhong, Yang ; Qiongjian, Fan
Author_Institution :
Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing
fYear :
2008
fDate :
16-18 July 2008
Firstpage :
398
Lastpage :
401
Abstract :
Fuzzy logic control guidance (FLCG) law has been proved to be effective and robust, but the parameters of the fuzzy logical controller are usually difficult to determine and have great influence on the pursuit and intercept performance. In this paper, an optimal fuzzy logic control guidance (OFLCG) law is designed by applying particle swarm optimization method to optimize parameters of fuzzy logic controller. The objective is to improve the performance of FLCG by possibly minimizing the cost function, which is properly designed as a weight sum of pursuit time and energy consumptions. The parameters selected to be optimized are width of the membership functions, number of fuzzy partitions, and defuzzification method. Simulation results show that the intercept performance of the designed guidance law is better than that of FLCG and proportional navigation guidance (PNG) law.
Keywords :
aircraft navigation; control system synthesis; fuzzy control; minimisation; optimal control; robust control; aircraft maneuverability; cost function minimization; defuzzification method; membership function; optimal fuzzy logical control guidance design; particle swarm optimized parameter; robust control; Cost function; Design optimization; Energy consumption; Fuzzy control; Fuzzy logic; Navigation; Optimal control; Optimization methods; Particle swarm optimization; Robust control; Fuzzy logic control; Guidance; Intercept; Particle swarm optimization;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference, 2008. CCC 2008. 27th Chinese
Conference_Location :
Kunming
Print_ISBN :
978-7-900719-70-6
Electronic_ISBN :
978-7-900719-70-6
Type :
conf
DOI :
10.1109/CHICC.2008.4605747
Filename :
4605747
Link To Document :
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