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Refining Membrane Model via Multi Particle Method combined with Vibration Experiment in Vacuum Chamber
https://jaxa.repo.nii.ac.jp/records/7248
https://jaxa.repo.nii.ac.jp/records/7248b776cc43-edcf-4b67-9a59-47292bffe4b7
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 | Refining Membrane Model via Multi Particle Method combined with Vibration Experiment in Vacuum Chamber | |||||
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 | |||||
その他のタイトル | ||||||
その他のタイトル | 真空環境下での振動実験による多粒子法を用いた膜モデルの高精度化に関する研究 | |||||
著者 |
羽染, 円絵
× 羽染, 円絵× 白澤, 洋次× 森, 治× 川口, 淳一郎× Hasome, Mitsue× Shirasawa, Yoji× Mori, Osamu× Kawaguchi, Junichiro |
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著者所属 | ||||||
東海大学 | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS) | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | |||||
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 : The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 巻 20, p. 1-6, 発行日 2011-03 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県 | |||||
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 | the 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本研究ではゴッサマ構造物のダイナミクス計算に適したモデルを構築することで面外変形を考慮した大型柔軟膜について,膜面をばね・マス・ダンパに置換する多粒子法を用いた多粒子系膜モデルを用いて検討する.従来の多粒子系膜モデルでは面外の曲げを考慮してこなかったが,本研究において実験結果と比較することで,薄膜であろうと面外剛性が膜面の挙動に影響を与えている事が明らかになった.よって,多粒子系膜モデルに曲げ剛性を入れた新しいモデルを構築し,そのモデルと実験結果を比較することで,モデルの高精度化を試みた. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, behavior of flexible membrane is discussed. In recent years, there have been a lot of attentions given to the use of membranes for space structure applications. As for the solar sail of spinning type in Japan has no rigid structure supporting its membrane, this mechanism has the advantage in its simple and lightweight structure, however, the attitude control is difficult due to the flexible membrane. I verify behavior of flexible membrane by numerical simulations using multi particle model (MPM). The multi particle model is using multi particle method which replaces membrane by spring, damper and mass. Compare with result of MPM and experimental result, refining membrane structural MPM. | |||||
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: AA0065115001 |