@inproceedings{oai:jaxa.repo.nii.ac.jp:00007249,
 author = {佐藤, 泰貴 and 古谷, 寛 and Sato, Yasutaka and Furuya, Hiroshi},
 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, 摘要: ソーラーセイル等の超大型膜を地上で簡易に折り畳むため，著者らは膜に折り目を形成させるガイドピンを用いた収納機構を提案してきた．提案した収納機構を用いて収納実験を行った結果，ガイドピンに対する膜の滑りが観察され，この滑りはガイドピン配置に依存することが示された．本研究では，収納機構を用いる際の折り畳みの精度を向上させるため，膜が滑る現象を一次元モデルを用いて表現し，滑りが生じにくいガイドピンの配置条件を明らかにする．, Guided-pin location of retraction mechanisms is examined to improve the fold precision of a large deployable space membrane. The guided-pin, which is introduced to the retraction mechanisms, generates the fold lines on the membrane. The retraction experiments with the guided-pins are performed to investigate the fold precision. In the course of the retraction, the fold precision is interfered by the slips between the guided-pin and the membrane. To investigate the non-slip condition, the mechanics of the slip is examined introducing a one-dimensional slip model for the guided-pin location. Finally, the non-slip condition, which is derived with the slip model, is evaluated by the results of the retraction experiments., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065115002},
 pages = {7--12},
 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 = {Location of Guided-Pin in Retraction Mechanisms for Large Deployable Space Membrane},
 volume = {20},
 year = {2011}
}