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Hayabusa attitude control for delta-V operations
https://jaxa.repo.nii.ac.jp/records/7457
https://jaxa.repo.nii.ac.jp/records/7457ab83bbbb-3f2c-46e3-bd9a-c52b2634cb73
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 | Hayabusa attitude control for delta-V operations | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スピン安定化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽輻射 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | イオンエンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 安定化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | はやぶさ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | MUSES-C | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小惑星探査機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | デルタV運用 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽追尾 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3軸安定化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星向き | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | トルク | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 追尾 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spin stabilization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar radiation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ion engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | stabilization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Hayabusa | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | MUSES-C | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Asteroid Sample-return Spacecraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | delta-V operation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sun tracking | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three axis stabilization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite orientation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | torque | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tracking | |||||
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 | はやぶさのΔV姿勢運用 | |||||
著者 |
小湊, 隆
× 小湊, 隆× 白川, 健一× 松岡, 正敏× 浦谷, 知恵× 大島, 武× Kominato, Takashi× Shirakawa, Kenichi× Matsuoka, Masatoshi× Uratani, Chie× Oshima, Takeshi |
|||||
著者所属 | ||||||
NEC航空宇宙システム | ||||||
著者所属 | ||||||
NEC航空宇宙システム | ||||||
著者所属 | ||||||
NEC航空宇宙システム | ||||||
著者所属 | ||||||
NEC航空宇宙システム | ||||||
著者所属 | ||||||
日本電気 | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Aerospace Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Aerospace Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Aerospace Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Aerospace Systems Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NEC Corporation | ||||||
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. 120-125, 発行日 2008-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 小惑星探査機「はやぶさ(MUSES-C: Asteroid Sample-return Spacecraft)」は2007年4月から地球帰還のためのイオンエンジンによるΔVを開始した。昨年は太陽輻射圧を利用することで燃料を使わないスピン姿勢制御方式を確立し、太陽追尾を実施した。この方式を踏まえて、イオンエンジン運転時に発生する推力軸周りの外乱トルクと太陽輻射によるトルクを拮抗させて、太陽追尾をする3軸姿勢制御を確立し、地球帰還のためのΔV運用を開始した。本報告では姿勢制御をどのように実施したか飛行結果を交えて述べる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Hayabusa (MUSES-C: Asteroid Sample-return Spacecraft) spacecraft started the homeward journey with an ion engine driven in April, 2007 aiming at the Earth return. In 2006, the fuel-free sun-tracking attitude control strategy was established and performed during spin stabilization. Then, the non-spin attitude control has been executed since February 2007. The key point is the balance of the solar radiation torque and the swirl torque of ion engine thrust. This paper reports how those attitude control strategies were carried out, showing flight results. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063718020 |