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Optimum Low-Thrust Multiple Rendezvous
https://jaxa.repo.nii.ac.jp/records/34529
https://jaxa.repo.nii.ac.jp/records/345294d74d7cc-929c-4a6f-a2c3-524a67f13bad
名前 / ファイル | ライセンス | アクション |
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||||
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公開日 | 2015-03-26 | |||||||
タイトル | ||||||||
タイトル | Optimum Low-Thrust Multiple Rendezvous | |||||||
言語 | en | |||||||
言語 | ||||||||
言語 | eng | |||||||
資源タイプ | ||||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||||
資源タイプ | departmental bulletin paper | |||||||
著者 |
UESUGI, Kuninori
× UESUGI, Kuninori
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出版者 | ||||||||
出版者 | 東京大学宇宙航空研究所 | |||||||
出版者(英) | ||||||||
出版者 | Institute of Space and Aeronautical Science,University of Tokyo | |||||||
書誌情報 |
en : ISAS report/Institute of Space and Aeronautical Science,University of Tokyo 巻 42, 号 6, p. 167-207, 発行日 1977-11 |
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抄録(英) | ||||||||
内容記述タイプ | Other | |||||||
内容記述 | The problem of multiple rendezvous with low-thrust propulsion systems is discussed. The motivation of this problem is given by the necessity of the space sweep mission in future which will aim to revover or deorbit several mission completed orbiting bodies in succession. Optimization parameter is the fuel consumption required to complete a multiple rendezvous in a given mission time. Optimum targeting sequence and time allocation to each rendezvous are determined by a simple method developed on the basis of a linear theory. Solutions are obtainable not only for the case of variable thrust mode but for the case of constant thrust mode of low-thrust propulsion systems. Some numerical examples for the verification of the developed methods are presented and the feasibility of low-thrust propelled space sweeper is discussed. | |||||||
ISSN | ||||||||
収録物識別子タイプ | ISSN | |||||||
収録物識別子 | 0372-1418 | |||||||
書誌レコードID | ||||||||
収録物識別子タイプ | NCID | |||||||
収録物識別子 | AA00675986 | |||||||
資料番号 | ||||||||
内容記述タイプ | Other | |||||||
内容記述 | 資料番号: SA2401275000 |