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Optimal trajectories in Earth Transfer Orbit for lunar transportation system
https://jaxa.repo.nii.ac.jp/records/7489
https://jaxa.repo.nii.ac.jp/records/7489ff912823-eb7e-41f0-879a-61dfa68f3689
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 | Optimal trajectories in Earth Transfer Orbit for lunar transportation system | |||||
言語 | ||||||
言語 | eng | |||||
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 | 遷移軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃料消費 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地球-月軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再使用宇宙機 | |||||
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 | 月輸送システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地球遷移軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ETO | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再使用軌道間輸送機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ROTV | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低推力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 大気減速 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 月軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御理論 | |||||
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 | transfer orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fuel consumption | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Earth-moon trajectory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reusable spacecraft | |||||
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 | lunar transportation system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Earth Transfer Orbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ETO | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Reusable Orbital Transfer Vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ROTV | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low thrust | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerobraking | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lunar trajectory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control theory | |||||
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 | 月輸送システムの地球帰還軌道における最適軌道制御 | |||||
著者 |
芝崎, 裕介
× 芝崎, 裕介× 船瀬, 龍× 津田, 雄一× 川口, 淳一郎× Shibasaki, Yusuke× Funase, Ryu× Tsuda, Yuichi× Kawaguchi, Junichiro |
|||||
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 | ||||||
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 | ||||||
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. 317-322, 発行日 2008-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 地球低軌道から月低軌道へ宇宙機を片道輸送する再使用型月輸送システムを提案し、復路(地球遷移軌道)において、制約される飛行時間に対し燃料消費最小の最適軌道を考察する。再使用型輸送システムの実現にとって、復路における燃料消費低減は最も重要な課題の1つである。燃料消費低減とシステムの複数回利用により、再使用型が従来の使い捨て型よりも輸送能力で有利になる。本研究では現実的な制約条件下で、復路における低推力推進と地球大気減速を利用した燃料消費最小の最適軌道を調べる。また、低推力推進による最適軌道制御に関して、運用性の観点から、解析的な準最適軌道制御則を導出しその有効性を示す。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, optimum trajectories of minimum fuel consumption in Earth Transfer Orbit (ETO) for a lunar transportation system are proposed according to the flight time restricted. The lunar transportation system is the Reusable Orbital Transfer Vehicle (ROTV), which transports a spacecraft from Low Earth Orbit (LEO) to Lunar Low Orbit (LLO) and returns to LEO. It is one of the most important problems for this system to minimize fuel consumption in ETO. The reusable transportation system is superior to the expendable one by minimizing fuel consumption in ETO and utilizing the system a few times. In ETO, we discuss multi-impulse flight using electrical propulsion and aero-assisted flight using aero-braking, and the optimum trajectory control law for the ROTV is shown. The analytical suboptimum control strategy is also shown and the effect of the strategy is investigated. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063718052 |