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Attitude determination and control system for QSAT
https://jaxa.repo.nii.ac.jp/records/7443
https://jaxa.repo.nii.ac.jp/records/7443e54eb8b9-4b4f-4569-a9bf-4979c06dba1d
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 | Attitude determination and control system for QSAT | |||||
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 | 衛星向き | |||||
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 | シミュレーション | |||||
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 | QSAT | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢決定・制御システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ADCS | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 比例微分制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | B-dot制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | カルマンフィルタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 最小自乗法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 太陽センサ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ジャイロスコープ | |||||
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 | satellite orientation | |||||
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 | simulation | |||||
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 | QSAT | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude determination and control system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ADCS | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | proportional-derivative control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | B-dot control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Kalman filter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | least square method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar sensor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | gyroscope | |||||
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 | QSATにおける姿勢決定及び姿勢制御 | |||||
著者 |
三桝, 裕也
× 三桝, 裕也× 宮田, 喜久子× 鳴海, 智博× vanderHa, Jozef Cyrillus× Mimasu, Yuya× Miyata, Kikuko× Narumi, Tomohiro× vanderHa, Jozef Cyrillus |
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著者所属 | ||||||
九州大学 大学院工学府 | ||||||
著者所属 | ||||||
九州大学 大学院工学府 | ||||||
著者所属 | ||||||
九州大学 大学院工学府 | ||||||
著者所属 | ||||||
九州大学 大学院工学府 | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Faculty of Engineering | ||||||
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. 30-34, 発行日 2008-03 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 九州大学の宇宙機ダイナミクス研究室では、小型衛星QSATの開発が進められている。ミッション達成のために正確に姿勢決定および姿勢制御を行うことが不可欠で、QSATにおいては太陽センサ、磁気センサ、ジャイロセンサを用いた姿勢決定、および磁気トルカを用いた姿勢制御を行う。最小2乗法とKalman Filterを併用した姿勢決定法、B-dot制御とPD(Proportional-Derivative)制御を使用した制御則の確立のために、独自で開発したシミュレータを用いて検証を行っており、今回はその進捗を報告する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In Space Systems Dynamics Laboratory (SSDL) at Kyushu University, the small satellite QSAT is being developed. In order to achieve the mission objectives, the attitude must be determined and controlled precisely. One function of the Attitude Determination and Control Subsystem (ADCS) is to estimate the attitude of the satellite by means of a Sun sensor, magnetometer and gyro rate sensor. Another function is to control the attitude by using the three-axis magnetorquer. The attitude determination of QSAT is based on a combination of the Weighted-Least-Square and Kalman-filter estimation methods. The Weighted-Least-Square method uses the Sun sensor and magnetometer measurements and the Kalman-filter combines the resulting angular observations with the gyro rate measurements. The attitude control is performed by a magnetorquer on the basis of a B-dot control for the de-tumbling phase and a Proportional-Derivative (PD) control law for the normal-mode. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063718006 |