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Instability analysis of Hayabusa attitude control by using one momentum wheel
https://jaxa.repo.nii.ac.jp/records/7458
https://jaxa.repo.nii.ac.jp/records/74581edbee5b-9a4e-4bfa-bd78-f8b22f2b4c1c
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 | Instability analysis of Hayabusa attitude control by using one momentum wheel | |||||
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 | 姿勢安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機安定性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御理論 | |||||
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 | モーメンタムホイール | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | PD制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 角運動量 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ニューテーションダンパ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御シミュレーション | |||||
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 | 運動方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ニューテーション | |||||
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 | attitude stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft stability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control theory | |||||
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 | momentum wheel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | PD control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angular momentum | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nutation damper | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control simulation | |||||
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 | equation of motion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nutation | |||||
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 | 1ホイールによるはやぶさ姿勢制御の不安定性解析 | |||||
著者 |
北島, 明文
× 北島, 明文× 船瀬, 龍× 森, 治× 白川, 健一× 川口, 淳一郎× Kitajima, Akifumi× Funase, Ryu× Mori, Osamu× Shirakawa, Kenichi× Kawaguchi, Junichiro |
|||||
著者所属 | ||||||
東京大学 大学院 | ||||||
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 | ||||||
NEC航空宇宙システム | ||||||
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 Graduate School | ||||||
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 | ||||||
NEC Aerospace Systems Ltd. | ||||||
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. 126-131, 発行日 2008-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 地球へ向けて帰還中の「はやぶさ(MUSES-C: Asteroid Sample-return Spacecraft)」は現在3台中2台のホイールが故障し、いわばバイアスモーメンタム方式で1軸姿勢制御を行っている。この方式ではシンプルな姿勢安定が実現されるはずだが、2007年3月にニューテーションが発散する傾向を示した。本稿では、この現象がホイール回転軸と探査機慣性主軸の不一致によることを解析と数値シミュレーションによって示し、防止策を提案する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Since Hayabusa (MUSES-C: Asteroid Sample-return Spacecraft) has lost two of three wheels, its attitude is currently stabilized by one-axis bias-momentum wheel. This method should lead to simple attitude keeping, but the motion showed nutation divergence in March 2007. This paper shows that the cause of the instable motion lies in the difference between the axis of wheel and of inertia, and a way to avoid this instability is proposed. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063718021 |