DocumentCode
1869279
Title
Research on fuzzy variable structure guidance law of the interceptor in aerosphere
Author
Yin, Yongxin ; Yang, Ming ; Wang, Zicai
Author_Institution
Harbin Inst. of Technol., Heilongjiang
fYear
2006
fDate
19-21 Jan. 2006
Lastpage
1377
Abstract
A fuzzy variable structure guidance law has been presented for intercepting the high-speed maneuverable target in aerosphere. The model of the relative movement between target and interceptor has been constructed. Taking the lateral thrust and aerodynamic force combining control into account, a three-dimensional fuzzy guidance law has been designed for tuning the variable structure guidance law, which can ensure the speediness and anti-jamming capability of the system and which can also reduce the chattering. This guidance law needs no information on the velocity and acceleration of the target, and hence is convenient for practical project. The simulation results show that this guidance law has highly precision for high-speed maneuverable target in aerosphere, and show that fuzzy variable structure guidance law has advantage
Keywords
fuzzy control; jamming; military systems; target tracking; variable structure systems; 3D fuzzy guidance law; aerosphere; antijamming capability; chattering; fuzzy variable structure guidance law; high-speed maneuverable target; interceptor; Acceleration; Aerodynamics; Arithmetic; Control systems; Equations; Force control; Fuzzy control; Fuzzy systems; Intelligent control; Kinetic theory;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aerospace and Astronautics, 2006. ISSCAA 2006. 1st International Symposium on
Conference_Location
Harbin
Print_ISBN
0-7803-9395-3
Type
conf
DOI
10.1109/ISSCAA.2006.1627540
Filename
1627540
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