摘要
This paper considers the guidance problem from a relative motion perspective. Acceleration, caused by gravity, of the interceptor is considered as the target's relative maneuver. The optimal guidance problem is designed to minimize the interceptor's real control effort, that is the normal acceleration in addition to gravity. Then the minimum effort guidance law is derived, where the relative maneuver caused by gravity is utilized rather than overcome during guidance. Finally, the performance of the proposed guidance law is proved through numerical simulations.
源语言 | 英语 |
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主期刊名 | 2023 42nd Chinese Control Conference, CCC 2023 |
出版商 | IEEE Computer Society |
页 | 3743-3747 |
页数 | 5 |
ISBN(电子版) | 9789887581543 |
DOI | |
出版状态 | 已出版 - 2023 |
活动 | 42nd Chinese Control Conference, CCC 2023 - Tianjin, 中国 期限: 24 7月 2023 → 26 7月 2023 |
出版系列
姓名 | Chinese Control Conference, CCC |
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卷 | 2023-July |
ISSN(印刷版) | 1934-1768 |
ISSN(电子版) | 2161-2927 |
会议
会议 | 42nd Chinese Control Conference, CCC 2023 |
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国家/地区 | 中国 |
市 | Tianjin |
时期 | 24/07/23 → 26/07/23 |
指纹
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Wei, L., Chen, Y., Liu, D., Dong, S., & Liu, J. (2023). Relative Maneuver and Minimum Effort Guidance Under Gravity. 在 2023 42nd Chinese Control Conference, CCC 2023 (页码 3743-3747). (Chinese Control Conference, CCC; 卷 2023-July). IEEE Computer Society. https://doi.org/10.23919/CCC58697.2023.10240271