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  2. 紀要論文 (Departmental Bulletin Paper)
  1. 機関資料(JAXA, former ISAS, NAL, NASDA)
  2. 旧機関資料 (JAXA, former-ISAS, NAL, NASDA)
  3. 宇宙科学研究所: ISAS Report等を含む (former ISAS (The Institute of Space and Astronautical Science): Including ISAS Report etc.)
  4. ISAS report/Institute of Space and Aeronautical Science,University of Tokyo

A Graphical Solution of Optimum Time-Fixed Two-Impulse Rendezvous Problem

https://jaxa.repo.nii.ac.jp/records/34505
https://jaxa.repo.nii.ac.jp/records/34505
27e741a5-afa9-4aa7-b366-d0771979db37
名前 / ファイル ライセンス アクション
SA2401198.pdf SA2401198.pdf (808.3 kB)
Item type 紀要論文 / Departmental Bulletin Paper(1)
公開日 2015-03-26
タイトル
タイトル A Graphical Solution of Optimum Time-Fixed Two-Impulse Rendezvous Problem
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

en 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 40, 号 7, p. 191-204, 発行日 1975-05
抄録(英)
内容記述タイプ Other
内容記述 A method for numerical determination of optimum time-fixed two-impulse rendezvous between general-inclined noncoapsidal elliptical-orbits is described. In this report, impulse function, that is, required velocity increment, is numerically investigated, and a geometric representation of impulse function in takeoff-arrival time plane is adopted. This geometric representation ("T-space") allows visualization of equi-velocity increment contours, thus revealing the minimum value as a point in this space. At the same time, optimum take-off time and arrival time is also obtained. In addition, by combining these maps, it is possible to obtain an optimum solution to the problem including more than one target, that is, the problem of multi-targets rendezvous. Though this graphical method proves adequate for locating minima of the impulse function, its numerical accuracy is not enough for determination of those precise values. Therefore, McCue's adaptive descent method is employed so that optimum impulse value can be computed accurately.
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: SA2401198000
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