现代防御技术2001,Vol.29Issue(2):31-34,38,5.
高空动能拦截器末制导导引方法设计与实现
Design and Realization of Terminal Guidance’s Method for
Kinetic Energy Interceptor at High Altitude
张雅声 1程国采 2陈克俊2
作者信息
- 1. 装备指挥技术学院试验指挥系,
- 2. 国防科技大学自动控制系,
- 折叠
摘要
Abstract
In this paper, an effective guidance method for kinetic energy interceptor′s terminal guidance is put forward, which makes the interce p tor knock against the target using the “Restrained turn rate of sight line grad ually”method. And a simulation is given to test the efficiency.关键词
动能拦截/末制导/比例导引/视线转率+/直接碰撞分类
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张雅声,程国采,陈克俊..高空动能拦截器末制导导引方法设计与实现[J].现代防御技术,2001,29(2):31-34,38,5.