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
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