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Preliminary Study of the trajectory design for SPICA mission
https://jaxa.repo.nii.ac.jp/records/7326
https://jaxa.repo.nii.ac.jp/records/7326aa0ce361-0f26-4e80-a373-3d16d8d65242
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 | Preliminary Study of the trajectory design for SPICA mission | |||||
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 | |||||
その他のタイトル | ||||||
その他のタイトル | 次期赤外線天文衛星SPICAミッション軌道設計の初期検討 | |||||
著者 |
中宮, 賢樹
× 中宮, 賢樹× 川勝, 康弘× Nakamiya, Masaki× Kawakatsu, Yasuhiro |
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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(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
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 19th workshop on JAXA Astrodynamics and Flight Mechanics 巻 2009, 発行日 2010-03 |
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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 | アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部)) | |||||
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 | Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 摘要: 本研究では、太陽-地球系L2周りのハロー軌道での観測を予定している次期赤外線天文衛星SPICAミッションの軌道設計の初期検討を行った。SPICAミッションではホイールに蓄積される外乱トルクをスラスタによりアンローディングすることを想定しており、その際に発生する余剰並進力の軌道保持への影響について検討を行った。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Preliminary mission design for the next-generation infrared astronomical mission, SPICA, which is to be launched into the Sun-Earth L2 Halo orbit, was studied. Our specific focus is on investigating the impact of translational force (unloading DeltaV), with respect to the orbit maintenance, caused by the thrusters unloading for accumulated angular momentum on the spacecraft reaction wheels. In addition, suppression methods for orbital disturbances caused by the unloading DeltaV are proposed and validated. | |||||
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: AA0064734021 |