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Optimization of trajectories from Earth to L2
https://jaxa.repo.nii.ac.jp/records/7569
https://jaxa.repo.nii.ac.jp/records/7569a33c582f-ff9d-494f-b6a1-14c69cf7b935
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 | Optimization of trajectories from Earth to L2 | |||||
言語 | ||||||
言語 | eng | |||||
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 | ラグランジュ平衡点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | L2点 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道 | |||||
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 | スイングバイ技術 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 推進薬消費 | |||||
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 | 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 | 電気推進 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | DNCLP | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 評価関数 | |||||
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 | Lagrangian equilibrium 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 | trajectory | |||||
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 | swingby technique | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | propellant consumption | |||||
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 | 3 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 | electric propulsion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | DNCLP | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | evaluation function | |||||
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 | LEOからL2点への輸送軌道の最適化 | |||||
著者 |
相田, 彩夏
× 相田, 彩夏× 松本, 道弘× 川勝, 康弘× 川口, 淳一郎× Aida, Saika× Matsumoto, Michihiro× Kawakatsu, Yasuhiro× Kawaguchi, Junichiro |
|||||
著者所属 | ||||||
東京大学 大学院工学系研究科 | ||||||
著者所属 | ||||||
東京大学 大学院工学系研究科 | ||||||
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 | ||||||
University of Tokyo School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo School of Engineering | ||||||
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. 18-22, 発行日 2006-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 太陽-地球間のL2点周りにおける深宇宙港、赤外線天文衛星などのミッションを想定し、LEO(Low Earth Orbit)からL2点への輸送軌道の最適化を行った。本研究では、まず化学推進を用いた輸送について、ΔV最小のための軌道投入角と投入速度の最適化を検討する。ここでは月スウィングバイを利用した輸送についても検討する。次に、化学推進での検討結果を元にしてIspの高い電気推進を利用した輸送軌道を検討する。各輸送の場合について飛行時間・消費燃料の点から輸送軌道を評価する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Optimization of trajectories from the Earth to the Sun-Earth L2 point is discussed, supposing their applications to missions around L2, such as deep-space ports and infrared astronomical satellites. Trade-off between short transit time and small fuel consumption is considered in detail. Transfers are studied in several cases, ballistic flight using chemical propulsion without lunar swing-by and with lunar swing-by, and multi-impulse flight using electrical propulsion. We discuss each case from the viewpoints of transit time and fuel consumption. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063480004 |