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アイテム
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Attitude Control of an Axisymmetric Spinning Satellite
https://jaxa.repo.nii.ac.jp/records/7355
https://jaxa.repo.nii.ac.jp/records/735546f86e87-bed9-483e-a811-39878f658c5f
Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Attitude Control of an Axisymmetric Spinning Satellite | |||||
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 | |||||
著者 |
樋口, 和也
× 樋口, 和也× 市川, 朗× Higuchi, Kazuya× Ichikawa, Akira |
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著者所属 | ||||||
京都大学大学院工学研究科航空宇宙工学専攻 | ||||||
著者所属 | ||||||
京都大学大学院工学研究科航空宇宙工学専攻 | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aeronautics and Astronautics, Graduate School of Engineering, Kyoto University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aeronautics and Astronautics, Graduate School of Engineering, Kyoto University | ||||||
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: 目標姿勢運動と現在の姿勢運動との相対運動方程式を導出し、その安定化制御を行うことにより、軸対称スピン衛星の姿勢制御を行う。原点周りの線形化方程式に基づく線形制御を非線形システムに適用し、その挙動を考察する。主に入力トルクのL(sub 1)ノルムに基づいて評価を行う。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, we discuss attitude control of a satellite from the minimum fuel point of view. We derive equations of relative motion between a desired attitude motion and the present attitiude motion, and consider its stabilization. We design a linear feedback controller based on the linearizied equations of relative motion around the origin. The main perforamance index is the L(sub 1) norm of the feedback controller. | |||||
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: AA0064734050 |