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宇宙ステーション搭載アームを用いた捕獲ミッションにおけるLEE(Latching End Effector)とターゲットの接触力学解析
https://jaxa.repo.nii.ac.jp/records/7383
https://jaxa.repo.nii.ac.jp/records/738382ecb41a-c502-4275-911b-1ba2f013cebb
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 | ||||||
タイトル | 宇宙ステーション搭載アームを用いた捕獲ミッションにおけるLEE(Latching End Effector)とターゲットの接触力学解析 | |||||
言語 | ||||||
言語 | jpn | |||||
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(英) | ||||||
その他のタイトル | Analysis on Contact Dynamics Between LEE (Latching End Effector) of Space Station Remote Manipulator System and a Floating Target | |||||
著者 |
鵜山, 尚大
× 鵜山, 尚大× 中西, 洋喜× 吉田, 和哉× 澤田, 弘崇× 小田, 光茂× 鈴木, 悟× Uyama, N.× Nakanishi, Hiroki× Yoshida, Kazuya× Sawada, Hirotaka× Oda, Mitsushige× Suzuki, S. |
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著者所属 | ||||||
東北大学 | ||||||
著者所属 | ||||||
東北大学 | ||||||
著者所属 | ||||||
東北大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
エイ・イー・エス | ||||||
著者所属(英) | ||||||
en | ||||||
Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Advanced Engineering Services (AES) | ||||||
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, 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 | In capturing a target in space, it is significant to confirm the safety of the procedure even contingency cases. This paper describes contact dynamics of Space Station Remote Manipulator System (SSRMS) capturing H-II Transfer Vehicle (HTV). The focus is made on the contact between snare wires of Latching End Effector (LEE) and grapple fixture of HTV. | |||||
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: AA0064733009 |