The Variable Universe Fuzzy Controller and Its Application in Missile Homing Guidance Law Design

被引：0

作者：

Zhang Weidong ^{[1
]}

Huang Xianlin ^{[1
]}

Li Shiyong ^{[2
]}

Gao Xiao-Zhi ^{[3
]}

机构：

[1] Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin 150000, Peoples R China

[2] Harbin Inst Technol, Dept Control Sci & Technol, Harbin 150000, Peoples R China

[3] Aalto Univ, Sch Elect Engn, Dept Automat & Syst Technol, Helsinki 00076, Finland

来源：

2013 32ND CHINESE CONTROL CONFERENCE (CCC) | 2013年

关键词：

fuzzy control; variable universe fuzzy control; Adjustable factor;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

As to the high-speed and high-maneuver characteristics of the airspace targets, the method of variable universe fuzzy control is applied to convert the guidance law problem to control problem for designing. In the traditional variable universe fuzzy control, the adjustable factor is constructed by the form of artificial mathematical functions. In order to introduce artificial intelligence to make the adjustable factor more to adapt to the characteristics of the system. Through the association with dynamic characteristics of the system, an improved adjustable factor is designed, whose adjustable speed and coordination are enhanced. Through the simulation, we test the capability of the corresponding controllers in guidance law, and the ideal result is achieved.

引用

页码：3541 / 3546

页数：6