小行星捕获轨道优化研究综述

宝音贺西; 包长春

doi:10.6052/1000-0879-19-106

小行星捕获轨道优化研究综述

宝音贺西^*,1), ,,
包长春^†,2), ,

^*清华大学航天航空学院,北京100084
^†内蒙古工业大学航空学院,呼和浩特010051

详细信息

作者简介:
1) E-mail: baoyin@tsinghua.edu.cn
宝音贺西，清华大学航天航空学院教授，博导，国家杰出青年基金获得者。1999 年哈尔滨工业大学飞行器设计专业博士毕业，后在日本、英国等地工作。2005 年回国后于清华大学工作，开展航天器动力学与控制基础理论和重大航天工程中的应用研究。2014—2018连续五年进入Elsevier 公布的中国高被引学者榜单(航天工程方向)。获国防科技进步一等奖、上海市科技进步一等奖；其小行星捕获、空间碎片发动机等成果两度被MITtech Review评论，引起国际广泛关注。攻克载人航天远距离最优导引的关键技术，研究成果应用于我国交会对接工程。AIAA 终身高级会员、Astrodynamics主编、Science China (Technology)、《航天器环境工程》《飞控与探测》《动力学与控制学报》等编委。培养的博士生5 人获得清华大学优秀博士论文奖，2 人获得全国优秀博士论文奖。

包长春: 2) E-mail: imut007@163.com

通讯作者:
宝音贺西

包长春

中图分类号: V412.4
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出版历程
- 收稿日期: 2019-03-18
- 发布日期: 2019-10-19

REVIEW ON OPTIMIZATION OF ASTEROID CAPTURE ORBITS

BAOYIN Hexi^*,1), ,,
BAO Changchun^†,2), ,

^*School of Aerospace Engineering, Tsinghua University, Beijing 100084, China
^†Aviation College, Inner Mongolia University of Technology, Huhhot 010051, China

More Information

Corresponding author:
BAOYIN Hexi

BAO Changchun

摘要

摘要: 小行星捕获对研究行星起源、地球生命来源、防御小行星撞击地球和开采行星矿产资源具有重要的意义。由于现有的推进器能力不足,小行星捕获任务中优化小行星捕获所需要的速度增量是任务成败的关键。本文分别从利用引力辅助轨道优化、连续小推力轨迹优化、小行星捕获任务轨道优化设计及小行星临时捕获等4 个方向介绍小行星捕获轨道优化方面国内外研究进展及现状。基于对上述研究现状的分析,尝试展望小行星捕获轨道优化研究的未来发展趋势。
- 小行星捕获 /
- 引力辅助 /
- 共振轨道 /
- 连续小推力
Abstract: The asteroid is of great significance for studying the formation of planets, the origin of life on the Earth, the defense against the collision of asteroids to the Earth and the mining on asteroids. Due to the insufficient capacity of the existing propulsion technology, the velocity increment needed to optimize the asteroid capture is the key for a successful capture mission. This paper reviews the capture orbit optimization method for asteroid and the extended capture period with the impulse thrust and lowthrust propulsions, including the strategy to capture asteroids by the gravity assisted and resonant orbital techniques, the continuous low thrust and temporary asteroid capture, and the scheme of extending the capture period.
- asteroid capture /
- gravity assisted /
- resonant orbits /
- continuous low-thrust

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参考文献(76)

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