摘要
For the propulsion technology and orbit transfer control of low-thrust spacecraft, the previous traditional methods and technologies are relatively expensive and cannot guarantee the optimal solution. This paper proposes a new solution method for the low-thrust spacecraft propulsion technology and orbit transfer design, which can optimize the propulsion and orbit transfer flight of low-thrust spacecraft. Theoretical design shows that this method can quickly obtain the optimal analytical solution, and has good optimization effects on the propulsion and orbit transfer of low-thrust spacecraft.
源语言 | 英语 |
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主期刊名 | Proceedings of the 43rd Chinese Control Conference, CCC 2024 |
编辑 | Jing Na, Jian Sun |
出版商 | IEEE Computer Society |
页 | 3761-3766 |
页数 | 6 |
ISBN(电子版) | 9789887581581 |
DOI | |
出版状态 | 已出版 - 2024 |
活动 | 43rd Chinese Control Conference, CCC 2024 - Kunming, 中国 期限: 28 7月 2024 → 31 7月 2024 |
出版系列
姓名 | Chinese Control Conference, CCC |
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ISSN(印刷版) | 1934-1768 |
ISSN(电子版) | 2161-2927 |
会议
会议 | 43rd Chinese Control Conference, CCC 2024 |
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国家/地区 | 中国 |
市 | Kunming |
时期 | 28/07/24 → 31/07/24 |
指纹
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Han, S., Mo, B., Li, W., & Jin, B. (2024). A Low-thrust Spacecraft Propulsion Technology and Its Orbit Transfer Application. 在 J. Na, & J. Sun (编辑), Proceedings of the 43rd Chinese Control Conference, CCC 2024 (页码 3761-3766). (Chinese Control Conference, CCC). IEEE Computer Society. https://doi.org/10.23919/CCC63176.2024.10661584