摘要
The tethered space-tug system is recognized as one of the most promising techniques to reduce the population of space debris. In this paper, the debris is specified as a large defunct GEO satellite equipped with one or two flexible appendages. A precise 3D dynamic model using Kane's method is derived. The dynamical behavior of the system is studied via numerical simulations, and some characteristics are revealed through this process.
源语言 | 英语 |
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主期刊名 | Dynamics and Control of Space Systems |
编辑 | Jeng-Shing Chern, Ya-Zhong Luo, Xiao-Qian Chen, Lei Chen |
出版商 | Univelt Inc. |
页 | 2037-2052 |
页数 | 16 |
ISBN(印刷版) | 9780877036531 |
出版状态 | 已出版 - 2018 |
活动 | 4th IAA Conference on Dynamics and Control of Space Systems, DYCOSS 2018 - Changsha, 中国 期限: 21 5月 2018 → 23 5月 2018 |
出版系列
姓名 | Advances in the Astronautical Sciences |
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卷 | 165 |
ISSN(印刷版) | 0065-3438 |
会议
会议 | 4th IAA Conference on Dynamics and Control of Space Systems, DYCOSS 2018 |
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国家/地区 | 中国 |
市 | Changsha |
时期 | 21/05/18 → 23/05/18 |
指纹
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Yang, K., Lu, S., Qi, R., Liu, Y., & Zhang, J. (2018). Dynamics of the tethered space-tug system for the removal of geo defunct satellite. 在 J.-S. Chern, Y.-Z. Luo, X.-Q. Chen, & L. Chen (编辑), Dynamics and Control of Space Systems (页码 2037-2052). (Advances in the Astronautical Sciences; 卷 165). Univelt Inc..