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2機の火星オービタの軌道設計に関する初期検討
https://jaxa.repo.nii.ac.jp/records/7399
https://jaxa.repo.nii.ac.jp/records/73990c88915e-29a8-4c1a-88a3-d891c9324d60
Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 2機の火星オービタの軌道設計に関する初期検討 | |||||
言語 | ||||||
言語 | jpn | |||||
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(英) | ||||||
その他のタイトル | Preliminary Study on Orbital Designs of Two Spacecraft around Mars | |||||
著者 |
尾川, 順子
× 尾川, 順子× 森本, 睦子× 川勝, 康弘× 川口, 淳一郎× Ogawa, Naoko× Morimoto, Mutsuko× Kawakatsu, Yasuhiro× Kawaguchi, Junichiro |
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著者所属 | ||||||
宇宙航空研究開発機構月惑星探査推進グループ | ||||||
著者所属 | ||||||
宇宙航空研究開発機構月惑星探査推進グループ | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 : 宇宙科学研究本部宇宙航空研究開発機構月惑星探査推進グループ | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 : 宇宙科学研究本部宇宙航空研究開発機構月惑星探査推進グループ | ||||||
著者所属(英) | ||||||
en | ||||||
JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC) | ||||||
著者所属(英) | ||||||
en | ||||||
JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) : JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) : JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC) | ||||||
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) | |||||
書誌情報 |
アストロダイナミクスシンポジウム講演後刷り集 en : Proceedings of 18th workshop on JAXA Astrodynamics and flight mechanics 巻 2008, 発行日 2009-03 |
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会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Symposium on Flight Mechanics and Astrodynamics 2008 (July 28-29, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 摘要: 2機の火星オービタの軌道設計に関して議論する.想定する2 機のオービタは軌道面が互いに直交していることが要求されているため,火星周回軌道投入後,軌道面やその方向を適切に調整する必要がある.これらの軌道を変更,維持する手法について考察する. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The orbit design of two spacecraft for Mars exploration mission is discussed. We assume two orbiters, whose orbits are required to be orthogonal. After Mars orbit insertion, it will be needed to adjust their orbital planes and eccentricity vectors appropriately for required configuration under J(sub 2) perturbation. We discuss how to insert S/C into these orbits and how to maintain them. | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11567475 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064733025 |