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本文从拦截流形的概念出发,对系统含有不确定因素,任意固有加速度的现代空间飞行器的拦截制导问题提出一个想法,它大大简化了制导过程,简单易行。在某种意义上,可以认为是传统方式的一种推广。
Based on the concept of intercepting manifolds, this paper presents an idea of the interception guidance problem of modern spacecraft with uncertainties and arbitrary accelerations. It simplifies the guidance process and is easy to implement. In a sense, can be regarded as a promotion of the traditional way.