| 一种拦截轨道的确定方法 |
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| 引用本文： | 程龙,陈勇. 一种拦截轨道的确定方法[J]. 航天控制, 2005, 23(1): 65-68 |
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| 作者姓名： | 程龙 陈勇 |
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| 作者单位： | 装备指挥技术学院,北京,101416;装备指挥技术学院,北京,101416 |
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| 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。
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| 关 键 词： | 轨道 空间交会 空间拦截 预测拦截点 |
| 文章编号： | 1006-3242(2005)01-0065-04 |
| 修稿时间： | 2004-08-26 |
A Method of Determining Intercepting Orbit |
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| Cheng Long,Chen Yong. A Method of Determining Intercepting Orbit[J]. Aerospace Control, 2005, 23(1): 65-68 |
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| Authors: | Cheng Long Chen Yong |
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| Affiliation: | Cheng Long Chen Yong The Academy of Equipment Command & Technology,Beijing 101416 |
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| Abstract: | 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. |
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| Keywords: | Orbit Space rendezvous Space interception Predictive interception point |
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