DocumentCode
441688
Title
Design of fuzzy-logic-based terminal guidance law
Author
Lu, Ya-Dong ; Yang, Ming ; Wang, Zi-cai
Author_Institution
Control & Simulation Center, Harbin Inst. of Technol., China
Volume
2
fYear
2005
fDate
18-21 Aug. 2005
Firstpage
888
Abstract
In order to intercept the high-speed maneuverable target in three-dimensional space, a terminal guidance law based on self-tuning fuzzy logic systems is presented. When constructing the model of the relative movement between target and interceptor, guidance knowledge base which including fuzzy data and rules is obtained. Moreover, considering the time-variant and nonlinear factors in the thrust vector control system, the interceptor´s mass is identified in real time. By using learning algorithms, the logic rules are also revised correspondingly according to the fuzzy performance index. Simulation results show that this method can implement efficiently the precise guidance of the interceptor as well as preferable robust stability.
Keywords
fuzzy control; fuzzy logic; fuzzy systems; learning (artificial intelligence); missile guidance; nonlinear control systems; robust control; self-adjusting systems; fuzzy performance index; high-speed maneuverable target; learning algorithm; nonlinear factor; robust stability; self-tuning fuzzy logic system; terminal guidance law; thrust vector control system; time-variant factor; Acceleration; Aerodynamics; Azimuth; Fuzzy logic; Geometry; Missiles; Performance analysis; Real time systems; Space technology; Trajectory; Fuzzy Logic; Guidance Law; Learning Algorithms; Self Tuning;
fLanguage
English
Publisher
ieee
Conference_Titel
Machine Learning and Cybernetics, 2005. Proceedings of 2005 International Conference on
Conference_Location
Guangzhou, China
Print_ISBN
0-7803-9091-1
Type
conf
DOI
10.1109/ICMLC.2005.1527069
Filename
1527069
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