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アイテム
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Application of ballistic capture trajectory for Jovian outpost establishment
https://jaxa.repo.nii.ac.jp/records/7578
https://jaxa.repo.nii.ac.jp/records/757867b21ccf-9a76-403b-9073-b5b782c28108
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 | Application of ballistic capture trajectory for Jovian outpost establishment | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 弾道軌道 | |||||
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 | 捕捉軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 木星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | カリスト | |||||
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 | 軌道最適化 | |||||
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 | CDTBP | |||||
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 | 運動方程式 | |||||
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 | ballistic trajectory | |||||
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 | capture trajectory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Jupiter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Callisto | |||||
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 | trajectory optimization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | circular districted three body problem | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CDTBP | |||||
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 | equation of motion | |||||
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 |
Poetro, Ridanto Eko
× Poetro, Ridanto Eko× 平山, 寛× 花田, 俊也× 八坂, 哲雄× Poetro, Ridanto Eko× Hirayama, Hiroshi× Hanada, Toshiya× Yasaka, Tetsuo |
|||||
著者所属 | ||||||
九州大学 | ||||||
著者所属 | ||||||
九州大学 | ||||||
著者所属 | ||||||
九州大学 | ||||||
著者所属 | ||||||
九州大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University | ||||||
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. 78-85, 発行日 2006-03 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Future exploration and exploitation of Jovian system is expected. Establishment of an outpost in Jovian system will ensure maximum benefit of the exploration with capability for extending the exploration to outer solar system and beyond. Outpost base around Callisto is tentatively selected to avoid the Jupiter's main radiation belt. Since multiple missions are required for the outpost establishment, the establishment trajectories must be optimized. Multiple gravity assists or low thrust propulsion is expected to be employed for the Jupiter en route trajectory. Braking using a Galilean moon prior to Jupiter insertion, followed by multiple Galilean moons resonance hopping for step by step apojove reduction are assumed to be taken as Callisto en route trajectory. This approach already save much Delta V compare to a direct trajectory scenario, but still leave a quite big Delta V for final orbit insertion. Final approach to Callisto along a trajectory on the weak stability boundary of Callisto with respect to Jupiter is examined. Numerical study of Callisto ballistic capture linked to an arriving joviocentric trajectory, with and without other Galilean moons effect, is performed for construction of an optimum final insertion maneuver. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063480013 |