摘要
提出了一种确定预测拦截点的方法,在此基础上解决了拦截轨道的确 定问题,并对结果进行了深层分析。方法简捷,易于编程实现。仿真结果合理, 满足要求,为航天试验及相关仿真工作提供了一个基础的轨道机动算法。
In this paper, a method of determining a predictive intercept point is put forward so as to determine an intercept orbit, and a further analysis is performed. The method is simple and easy to be realized by progranming, and the simulation result is reasonable and satisfying. It provides a basic orbital maneuver arithmetic for aerospace tests and correlative simulations.
出处
《航天控制》
CSCD
北大核心
2005年第1期65-68,共4页
Aerospace Control
关键词
轨道
空间交会
空间拦截
预测拦截点
Orbit Space rendezvous Space interception Predictive interception point
