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Low-thrust periodic orbits in the restricted three-body problem
https://jaxa.repo.nii.ac.jp/records/7567
https://jaxa.repo.nii.ac.jp/records/75672f77ec84-27fc-4a7b-9f6f-0bb214a9bbc8
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Low-thrust periodic orbits in the restricted three-body problem | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3体問題 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低推力推進 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 運動方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 人為的平衡点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 振動運動 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 共振周期軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非平衡点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道計算 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 線形化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リサジュ図形 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three body problem | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low thrust propulsion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | equation of motion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | artificial equilibrium point | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | oscillatory motion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | resonant periodic orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | non-equilibrium point | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbit calculation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | linearization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Lissajous figure | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | trajectory | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル | ||||||
その他のタイトル | 低推力推進を利用した周期軌道に関する1考察 | |||||
著者 |
森本, 睦子
× 森本, 睦子× 山川, 宏× 上杉, 邦憲× Morimoto, Mutsuko× Yamakawa, Hiroshi× Uesugi, Kuninori |
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著者所属 | ||||||
総合研究大学院大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate University for Advanced Studies | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
第15回アストロダイナミクスシンポジウム講演後刷り集 2005 en : Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics p. 7-11, 発行日 2006-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本研究では3体問題における回転座標系において、低推力加速度を用いて任意の点(停留点)で宇宙機を周期的に周回させる事を考える。周期軌道を解析的に求めるために運動方程式を停留点で線形化する。停留点に固有の周回周期に着目し、面内と面外の運動周期が共鳴する周期軌道について考察を行う。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Periodic orbits around non-equilibrium points are generated systematically by utilizing continuous low-thrust propulsion in the restricted three-body problem. Equations of motion are linearized in order to analytically generate periodic orbits with constant acceleration. The mass ratio between two primary bodies is assumed to vary from 0 to 1/2. Periodic orbits around artificial equilibrium points which exist on the line connecting two primaries are investigated. Then, the frequencies of these periodic motions are analyzed. By choosing the frequencies of motions that are small-integer resonant, we have found the existence of points at which in-plane and out-of-plane motions are synchronized. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063480002 |