@inproceedings{oai:jaxa.repo.nii.ac.jp:00007248,
 author = {羽染, 円絵 and 白澤, 洋次 and 森, 治 and 川口, 淳一郎 and Hasome, Mitsue and Shirasawa, Yoji and Mori, Osamu and Kawaguchi, Junichiro},
 book = {アストロダイナミクスシンポジウム講演後刷り集, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {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, 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, 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．, 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., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065115001},
 pages = {1--6},
 publisher = {宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS), Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {Refining Membrane Model via Multi Particle Method combined with Vibration Experiment in Vacuum Chamber},
 volume = {20},
 year = {2011}
}