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Membrane deployment for spinning formation-flight solar sail
https://jaxa.repo.nii.ac.jp/records/7643
https://jaxa.repo.nii.ac.jp/records/7643df668513-dc5b-4d1c-993c-8b3357e39737
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 | Membrane deployment for spinning formation-flight solar sail | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 膜面展開 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 編成飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ソーラーセール | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 微小重力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 人工衛星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 予備調査 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | membrane deployment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | formation flight | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solar sail | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | microgravity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | artificial satellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | feasibility study | |||||
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 | スピンフォーメーション・ソーラーセールの膜面展開 | |||||
著者 |
松永, 三郎
× 松永, 三郎× 矢部, 秀幸× 中谷, 幸司× 居相, 政史× 尾曲, 邦之× 森, 治× Matsunaga, Saburo× Yabe, Hideyuki× Nakaya, Koji× Iai, Masafumi× Omagari, Kuniyuki× Mori, Osamu |
|||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属 | ||||||
東京工業大学 大学院理工学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology Graduate School of Science and 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 |
平成16年度アストロダイナミクスシンポジウム:講演後刷り集 en : ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers p. 55-60, 発行日 2005-03 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In the paper, a new type membrane deployment method is proposed, and locally full-deployment state can be achieved in the deployment from folded state. Fundamental ground experiments of the proposed membrane deployment are conducted using an experimental set-up system including two-dimensional micro-gravity simulators, and tether and membrane control mechanisms developed at Tokyo Institute of Technology. The simulator system is composed of a 3 m x 5 m flat-floor glass and floating satellite simulators with gas-thruster. Here, used are three satellite simulators, triangular membranes, the tether control system and newly developed drum mechanisms for membrane control. The drum mechanism can control membrane extension speed. A virtual structure control method is applied to control the three satellites for formation flight, and PID type control is adopted to control the membrane control. From the experiment obtained is two-dimentional deployment behavior and the feasibility of the proposed method is discussed comparing with corresponding numerical simulation results. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0918-8053 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047897010 |