WEKO3
アイテム
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Ground experiment on formation deployment of spinning tethered formation flying
https://jaxa.repo.nii.ac.jp/records/7608
https://jaxa.repo.nii.ac.jp/records/7608521c0dcd-7cb3-4a09-876a-51302c0c8905
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 | Ground experiment on formation deployment of spinning tethered formation flying | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | テザー衛星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 編隊飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スピン安定化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | シミュレータ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御系設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 編隊展開 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スピン制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機ダイナミックシミュレータ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地上実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 角速度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | リール | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 実験 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tethered satellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | formation flying | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spin stabilization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | simulator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control system design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | formation deployment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spin control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft dynamic simulator | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ground experiment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude angle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | angular velocity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | trajectory | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | experimentation | |||||
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 | テザー制御型スピンフォーメーションフライングの隊列展開に関する地上実験 | |||||
著者 |
中谷, 幸司
× 中谷, 幸司× 居相, 政史× 松永, 三郎× Nakaya, Koji× Iai, Masafumi× Matsunaga, Saburo |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 | ||||||
著者所属 | ||||||
東京工業大学 | ||||||
著者所属 | ||||||
東京工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
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/ISAS) | |||||
書誌情報 |
第15回アストロダイナミクスシンポジウム講演後刷り集 2005 en : Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics p. 270-275, 発行日 2006-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本発表で扱うテザー制御型スピンフォーメーションフライングは、3機の宇宙機が張力制御可能なテザーで環状に結合され、系の質量中心周りにスピンしているシステムである。このタイプのフォーメーションフライングは高精度の隊列維持を少ない燃料で実現できるため注目されている。このシステムの基礎的研究として隊列の半径を拡大する隊列展開に着目し地上実験を行った。本発表ではこの地上実験結果を報告する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The spinning tethered formation flying that is treated in this study consists of three spacecraft connected by tension-controlled tethers each other, and rotates around the center of mass of the system. This type of formation flying has been growing because it is able to reduce fuel consumption as well as precisely control relative position and attitude. We conducted ground experiments on formation deployment of the system using two-dimensional micro-gravity simulators. In this presentation, the results of the experiments are discussed. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063480043 |