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A study of capture trajectories to the vicinity of L1 and L2 points
https://jaxa.repo.nii.ac.jp/records/7449
https://jaxa.repo.nii.ac.jp/records/7449648b3e2f-8cfc-4449-a73c-167c31a6a668
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 | A study of capture trajectories to the vicinity of L1 and L2 points | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ラグランジュ平衡点 | |||||
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 | 宇宙機軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 惑星間遷移軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 円制限3体問題 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CR3BP | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | L1点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | L2点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 近点 | |||||
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 | 軌道力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リアプノフ軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Lagrangian equilibrium point | |||||
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 | spacecraft trajectory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | interplanetary transfer orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | trajectory analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | circular restricted three body problem | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CR3BP | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | L1 point | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | L2 point | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | periapsis | |||||
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 | orbital mechanics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Lyapunov orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical analysis | |||||
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 | |||||
著者 |
中宮, 賢樹
× 中宮, 賢樹× Scheeres, Daniel× 山川, 宏× 吉川, 真× Nakamiya, Masaki× Scheeres, Daniel× Yamakawa, Hiroshi× Yoshikawa, Makoto |
|||||
著者所属 | ||||||
総合研究大学院大学 | ||||||
著者所属 | ||||||
University of Michigan | ||||||
著者所属 | ||||||
京都大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate University for Advanced Studies | ||||||
著者所属(英) | ||||||
en | ||||||
University of Michigan | ||||||
著者所属(英) | ||||||
en | ||||||
Kyoto University | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
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17回アストロダイナミクスシンポジウム講演後刷り集 2007 en : Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics p. 63-68, 発行日 2008-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We investigate spacecraft capture trajectories to the periodic orbits of the L1 and L2 points in the planar restricted Hill three-body problem are studied. The specific focus is on transfer to these vicinities from interplanetary trajectories. This application is motivated by future plan to use the Sun-Earth and Sun-Mars collinear libration points as space hub for Mars Mission. We utilize stable manifolds for capture trajectories to periodic orbits around the libration points. As a result, the cost of capture into a periodic orbit is also reduced relative to direct capture into a parabolic orbit. The way of linking between interplanetary transfer trajectories and the stable manifold is also discussed. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063718012 |