An Efficient Guidance Law for Intercepting Maneuvering Evader in Three-Dimensions

被引:0
|
作者
肖昌美
张福恩
程恭
机构
关键词
Minimum energy guidance law; on-line linearizing; receding horizon control;
D O I
暂无
中图分类号
TP391.9 [计算机仿真];
学科分类号
080203 ;
摘要
Considering the nonlinear model between a realistic missile and an aircraft in three-dimensions, one minimun energy guidance law is obtained. By employing the linearizing method, an efficient and robust guidance law for intercepting randomly maneuvering evader is derived. A new approach to pursuit-evasion problem in two-dimensions and three-dimensions is provided, which can deal with the randomly maneuvering evader in time. Numerical simulations denote that the system designed by this method can cut down the miss distance remarkably.
引用
收藏
页码:34 / 38
页数:5
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