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Consensus Control for Rotational Dynamics of Multiple Spacecraft
https://jaxa.repo.nii.ac.jp/records/7408
https://jaxa.repo.nii.ac.jp/records/740814aa515c-3e43-4e33-92c0-e9944922f9b0
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 | Consensus Control for Rotational Dynamics of Multiple Spacecraft | |||||
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 |
早川, 朋久
× 早川, 朋久× Mohanarajah, Gajamohan× Hayakawa, Tomohisa |
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著者所属 | ||||||
東京工業大学大学院情報理工学研究科情報環境学専攻 | ||||||
著者所属 | ||||||
東京工業大学大学院情報理工学研究科情報環境学専攻 | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical and Environmental Informatics, Tokyo Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Mechanical and Environmental Informatics, Tokyo Institute of Technology | ||||||
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 18th workshop on JAXA Astrodynamics and flight mechanics 巻 2008, p. 215-220, 発行日 2009-03 |
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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 | Symposium on Flight Mechanics and Astrodynamics 2008 (July 28-29, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A consensus control framework for the rotational dynamics of multiple spacecraft is developed. The approach is energy based and guarantees asymptotic convergence of relative states between the spacecraft. Since the proposed control law emulates internal forces between the spacecraft, the overall angular momentum is kept constant. Furthermore, it is shown that the angular velocities of each spacecraft can be made to asymptotically converge towards a constant value, i.e. each spacecraft can be made to rotate around a fixed common rotational axis. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
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: AA0064733034 |