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Optimization of Low Thrust Trajectories for Collinear Largrange Point Mission
https://jaxa.repo.nii.ac.jp/records/31174
https://jaxa.repo.nii.ac.jp/records/31174323e1bfe-8921-4433-be79-6051821858c4
名前 / ファイル | ライセンス | アクション |
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SA0033407.pdf (676.0 kB)
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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 | ||||||
言語 | en | |||||
タイトル | Optimization of Low Thrust Trajectories for Collinear Largrange Point Mission | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | optimum transfer-low thrust transfer-Lagrange point | |||||
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 |
MATSUO, Hiroki
× MATSUO, Hiroki× MATOGAWA, Yasunori× NOZUE, Tatsuhiro× SHIMODA, Toshio |
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著者所属(英) | ||||||
en | ||||||
Totsuka Works, Hitachi, Ltd. | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science | |||||
書誌情報 |
en : The Institute of Space and Astronautical Science report. S.P. : Proceedings of the Symposium on Mechanics for Space Flight 巻 1, p. 87-102, 発行日 1983-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Two kinds of optimization problems on low thrust transfer trajectories are discussed. One is a transfer from earth parking orbit to Sun-Earth interior libration point L_1.So-called J-minimum trajectories are obtained for this case. It is shown that, in spite of some injection error, spececraft can reach L_1 by optimizing low thrust programs. The other problem treated in this paper pertains to a transfer between collinear Lagrange points, L_1 and L_2,of Sun-Earth system. In this case, two types of low thrust, that is, power-constant and thrust-constant trajectories are studied. In the former case, J-minimum trajectories are obtained, and, in the latter, fuel optimum trajectories with a single coasting arc were sought including optimal steering programs as a function of total mission time. Computational results show that spacecraft can travel between two points within a mission time that stands comparison with high thrust impulsive transfer. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0288-433X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA10455137 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0033407000 |