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Formulation Methods of Rigid Multibody Systems for Large Space Structures and Some Results of Computer Simulation
https://jaxa.repo.nii.ac.jp/records/45201
https://jaxa.repo.nii.ac.jp/records/45201e39bbd99-576f-41fb-afb5-e5c5b6b06ed2
名前 / ファイル | ライセンス | アクション |
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naltr00942.pdf (1.2 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Formulation Methods of Rigid Multibody Systems for Large Space Structures and Some Results of Computer Simulation | |||||
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_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル | ||||||
その他のタイトル | 多剛体宇宙構造物のモデリング手法とシミュレーション結果 | |||||
著者 |
狼, 嘉彰
× 狼, 嘉彰× 岡本, 修× 木田, 隆× 山口, 功× 山田, 克彦× 土屋, 和雄× OOKAMI, Yoshiaki× OKAMOTO, Osamu× KIDA, Takashi× YAMAGUCHI, Isao× YAMADA, Katsuhiko× TSUCHIYA, Kazuo |
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著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属 | ||||||
三菱電機株式会社中央研究所 | ||||||
著者所属 | ||||||
三菱電機株式会社中央研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Space Technology Research Group, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Space Technology Research Group, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Space Technology Research Group, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Space Technology Research Group, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Electric Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Electric Corporation | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-942 巻 942, p. 17, 発行日 1987-08 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper we describe a comparative study of the simulation algorithms for dynamics of large space structures modeled as a collection of rigid multibodies connected by hinges. Two different algorithms have been independently developed at two different research institutes. One method is basically based upon the well-known Euler Newton formulation and the unified matrix approach. The unified matrix approach solves the dynamical equation for the derivatives of the non-holonomic velocities and the internal torques and forces simultaneously, hence permitting us to deal with an aribitrary LSS configuration. The other method provides for an efficient and fast algorithm based on Kane’s method with modification in the inertia dyadic and other quantities. Both methods have been applied to two typical examples: the first one is a satellite with a four-link manipulator as a model of a chain structure, and the second is a satellite with a closed loop deployment mechanism. The results coincide satisfactorily and the validity of the two methods has been proven perfectly. The numerical values given in this report will be useful as a reference in other simulations. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0942000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-942 |