地基激光清除空间碎片的策略

王成林; 张艳; 王鲲鹏

doi:10.13700/j.bh.1001-5965.2014.0696

地基激光清除空间碎片的策略

doi: 10.13700/j.bh.1001-5965.2014.0696

北京跟踪与通信技术研究所, 北京 100094

详细信息

作者简介:
王成林(1992-),男,安徽宿州人,硕士研究生,wcl4756308@163.com

通讯作者:
张艳(1975-),女,江苏阜宁人,副研究员,zhyan1227@sina.com,主要研究方向为空间目标探测与识别.

中图分类号: V221⁺.3;TB553
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- 被引次数: 0
出版历程
- 收稿日期: 2014-11-11
- 修回日期: 2015-02-12
- 网络出版日期: 2015-11-20

Strategy of removing space debris using ground-based lasers

Beijing Institute of Tracking and Telecommunications Technology, Beijing 100094, China

摘要

摘要: 空间碎片的清除策略是实现地基激光主动清除厘米级空间碎片的关键技术之一.为了制定有效的清除策略,首先对在碎片轨道不同位置上速度分量的变化对其新轨道近地点高度的影响进行了研究,指明了3种不同速度分量变化的降轨效果的差异;然后结合地基激光的几何和物理特性,推导了确定有效变轨区域的约束条件;最后据此提出了地基激光以连续脉冲变轨方式清除空间碎片的通用策略,并通过仿真实验,实现了利用地基激光清除空间碎片的目的,也验证了该清除策略的有效性.
- 地基激光 /
- 空间碎片 /
- 清除策略 /
- 变轨 /
- 仿真
Abstract: The removal strategy of space debris is one of the most key technologies to achieve the goal of clearing space debris in a wide range of sizes from 1 to 10 cm actively using ground-based lasers. In order to develop an effective strategy for removing space debris, we firstly studied on the influences, which the changes of different velocity components had on the altitude of new orbit's perigee, finding that the same velocity increment along different velocity components has different effects on lowering the altitude of perigee. And then combined with the geometrical and physical of ground-based lasers, the constraint conditions that determine the area of orbit transfer were deduced. Finally, a general strategy, removing space debris in the way of continuous impulse orbit transfer using ground-based lasers, was proposed based on those mentioned above. Moreover, space debris removal using ground-based lasers is realized and the effectiveness of the clearing strategy is also verified through simulation experiments.
- ground-based lasers /
- space debris /
- removal strategy /
- orbital variation /
- simulation

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参考文献(15)

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