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Trajectory analysis of post-Hayabusa asteroid explorer mission
https://jaxa.repo.nii.ac.jp/records/7587
https://jaxa.repo.nii.ac.jp/records/7587a6e2089a-8f63-4ae7-9236-1406c48fd51b
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 | Trajectory analysis of post-Hayabusa asteroid explorer mission | |||||
言語 | ||||||
言語 | eng | |||||
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 | スイングバイ技術 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 電気推進 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小惑星ミッション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | サンプルリターンミッション | |||||
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 | M-V打上げ機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 逐次2次計画法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SQP法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | EDVEGA | |||||
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 | 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 | ||||||
主題Scheme | Other | |||||
主題 | マヌーバ | |||||
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 | swingby technique | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | electric propulsion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | asteroid mission | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sample return mission | |||||
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 | M-V launcher | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sequential quadratic programming method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SQP method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | EDVEGA | |||||
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 | equation of motion | |||||
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 | maneuver | |||||
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 | 次期小惑星探査ミッションの軌道計画の検討状況 | |||||
著者 |
川勝, 康弘
× 川勝, 康弘× 山川, 宏× 安部, 正真× Kawakatsu, Yasuhiro× Yamakawa, Hiroshi× Abe, Masanao |
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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 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
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 | ||||||
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. 135-140, 発行日 2006-03 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本発表では、次期小惑星探査ミッションの検討の中で進めている軌道計画の検討状況を報告する。昨年度のシンポジウムでは、対象天体と探査シーケンスを絞り込むための予備検討として、弾道飛行とスウィングバイを組み合わせた探査シーケンスの検討結果を報告した。今回は、その結果を元に選定したミッション候補に対し、電気推進を主推進として地球スウィングバイを組み合わせたE-ΔVEGAの使用を想定した軌道計画を検討したので、その結果を報告する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Reported in this paper is the status of the trajectory analysis of the asteroid explorer mission now under study in JAXA/ISAS. In the previous symposium, we have reported the results of the preliminary analysis to select the candidates of the target asteroids and the exploration sequence. The global search of the targets and sequences in the space of the combinations of the ballistic trajectories and planetary swing-bys successfully made clear the mission candidates suited our objective. Following the preliminary analysis, more detailed trajectory analysis is performed assuming the usage of the electric propulsion, and the results of which are reported in this paper. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063480022 |