摘要
以高空动能拦截器为研究对象 ,为其末制导段设计了一种“逐段限制视线转率”的导引方法 ,使之最终能直接命中目标 ,实现动能拦截的任务并通过仿真计算验证了该导引法的可行性。
In this paper, an effective guidance method for kinetic energy interceptor′s terminal guidance is put forward, which makes the interceptor knock against the target using the “Restrained turn rate of sight line gradually”method. And a simulation is given to test the efficiency.
出处
《现代防御技术》
2001年第2期31-34,38,共5页
Modern Defence Technology
关键词
动能拦截
末制导
比例导引
视线转率
直接碰撞
高空动能拦截器
Kinetic energy interception
Terminal guidance
proportional guidance
Line of sight turn rate +
Direct collision
