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| 航天器碰撞分析方法研究 | |
| 引用本文： | 秋宏兴,祝转民,吴连大.航天器碰撞分析方法研究[J].宇航学报,2005,26(3):257-261. |
| 作者姓名： | 秋宏兴 祝转民 吴连大 |
| 作者单位： | 1. 中国科学院南京紫金山天文台,南京,210008;西安卫星测控中心,西安,710043 2. 西安交通大学理学院,西安,710049 3. 中国科学院南京紫金山天文台,南京,210008 |
| 基金项目： | 国家博士后科学基金资助项目(20040350685) |
| 摘 要： | 作为航天器碰撞与规避控制方法研究课题的一部分,为此分别建立了航天器及其它空间目标的轨道确定方法;并在此基础上,提出了可能与航天器碰撞的其它空间编目目标的初选准则和碰撞预报算法。实测数据计算表明,该方法对于航天器轨道设计以及飞行安全性分析等均是实用可行的。 |
| 关 键 词： | 航天器 轨道确定 碰撞预报 |
| 文章编号： | 1000-1328(2005)03-0257-05 |
A Study of Collision Analysis Method for Spacecraft |
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| QIU Hong-xing,ZHU Zhuan-min,WU Lian-da.A Study of Collision Analysis Method for Spacecraft[J].Journal of Astronautics,2005,26(3):257-261. | |
| Authors: | QIU Hong-xing ZHU Zhuan-min WU Lian-da |
| Institution: | QIU Hong-xing~1,ZHU Zhuan-min~2,WU Lian-da~1 |
| Abstract: | As part of the task to research a method for collision avoidance between the primary spacecraft and other space objects, this paper presents orbit determination methods for primary spacecraft and other space objects respectively. Based on this , a kind of criteria to filter the catalogue objects and collision predict algorithm were proposed. An example shows the method is particularly useful for designing the spacecraft orbit and analysising the orbit safety. |
| Keywords: | Spacecraft Orbit determination Collision predict |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |