WEKO3
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Design and on-orbit evaluation of magnetic attitude control system for REIMEI microsatellite
https://jaxa.repo.nii.ac.jp/records/7544
https://jaxa.repo.nii.ac.jp/records/7544180a69fa-d8bb-492e-9086-79418ec13b7e
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 | Design and on-orbit evaluation of magnetic attitude control system for REIMEI microsatellite | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | れいめい | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | INDEX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小型高機能科学衛星 | |||||
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 | トルカ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 光ジャイロスコープ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小型衛星技術 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フィードバック制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 磁気モーメント | |||||
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 | 制御系設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 評価 | |||||
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 | 磁気トルカ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | REIMEI | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | INDEX | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | INnovative-technology Demonstration Experiment | |||||
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 | torquer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | optical gyroscope | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | small satellite technology | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | feedback control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | magnetic moment | |||||
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 | control system design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | evaluation | |||||
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 | magnetic torquer | |||||
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 | れいめい衛星の磁気姿勢制御とその軌道上評価 | |||||
著者 |
坂井, 真一郎
× 坂井, 真一郎× 福島, 洋介× 斎藤, 宏文× Sakai, Shinichiro× Fukushima, Yosuke× Saito, Hirobumi |
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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 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
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 | ||||||
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16回アストロダイナミクスシンポジウム講演後刷り集 2006 en : Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics p. 248-254, 発行日 2007-03 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 2005年8月に打ち上げられた小型科学衛星'れいめい(INDEX: INnovative-technology Demonstration EXperiment)'では、衛星小型化のためにホイールは1台のみを使用し、主に磁気トルカにより姿勢制御を行っている。このような磁気姿勢制御で0.1度以下の姿勢制御精度を実現している点が、'れいめい'衛星の1つの特徴ともなっている。本発表では、この磁気姿勢制御則の設計とその軌道上評価の結果について報告する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Magnetic attitude control methods for the REIMEI (INDEX: INnovative-technology Demonstration EXperiment) microsatellite is presented. REIMEI is a 70 (kg) microsatellite and was launched in 2005. REIMEI achieved pointing accuracy of 0.05 - 0.1 (deg), with actuators of three Magnetic Torquers (MTQs) and one moment wheel. With this configuration, the management of magnetic torque is important for attitude control. This paper proposes practical MTQs drive algorithm to generate required magnetic torque, maintaining undesirable disturbance torque to be low enough even in the neighborhood of singular points. Another key technology for the REIMEI satellite is in-orbit estimation of residual magnetic moment and its feedforward cancellation. This method will contribute a lot, not only for a bias momentum satellite, but also for small/micro satellites with pure magnetic ACS (Attitude Control System). These proposed methods are demonstrated with in-orbit data of the REIMEI microsatellite. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063481043 |