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Design of Loose Formation Flying in the Vicinity of Halo Orbits Based on Initial Set Values
https://jaxa.repo.nii.ac.jp/records/7276
https://jaxa.repo.nii.ac.jp/records/7276a7b0ea13-a405-4f7a-8b50-07459ca26a3b
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 | ||||||
言語 | en | |||||
タイトル | Design of Loose Formation Flying in the Vicinity of Halo Orbits Based on Initial Set Values | |||||
言語 | ||||||
言語 | eng | |||||
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 |
中宮, 賢樹
× 中宮, 賢樹× 川勝, 康弘× Simanjuntak, Triwanto× Nakamiya, Masaki× Kawakatsu, Yasuhiro |
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著者所属 | ||||||
総合研究大学院大学 | ||||||
著者所属 | ||||||
総合研究大学院大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate University for Advanced Studies (Sokendai) | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate University for Advanced Studies (Sokendai) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | |||||
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 : The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 巻 20, p. 175-183, 発行日 2011-03 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県 | |||||
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 | The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper we address natural formation flying around L2 point of the Sun-Earth Circular Restricted Three-Body Problem (CR3BP) systems. Halo orbit is choosen as the reference orbit for the leader and the follower is conceived to follow loosely. This type of formation will be useful in future for constructing space based ports, long-baseline space telescope, sun-shielded astronomical spacecraft, etc. We approach this problem by utilizing Dynamical System Theory (DST). | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
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: AA0065115029 |