@inproceedings{oai:jaxa.repo.nii.ac.jp:00007368,
 author = {菅原, 佳城 and 小林, 信之 and Shinohara, Ken and Sugawara, Yoshiki and Kobayashi, Nobuyuki},
 book = {アストロダイナミクスシンポジウム講演後刷り集, Proceedings of 19th workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部)), Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan, 摘要: 紐や膜などの柔軟な要素を有する衛星の挙動は，剛体運動を伴った大変形を生じる．そのような挙動に対して，近年Absolute Nodal Coordinate Formulation (ANCF)が注目されているが，その解析精度についての実験的な検証は数少ない．本研究では基礎的な検証として，大変形を伴って大回転する柔軟はりの動的スティフニング効果に注目し，解析結果と実験結果を比較することにより，柔軟要素を有する衛星の解析手法としてのANCFを検証する., Satellites which have flexible structures such as tethers or membranes undergo rigid body motion with their large deformation. Absolute Nodal Coordinate Formulation (ANCF) is attracting a lot of attention as a method for dealing with such behaviors. However, there are not enough researches which validate the method by comparison with experimental data. In this investigation, dynamic stiffening effect of flexible beam undergoing large rotation is focused on and ANCF is validated by comparison of numerical results and experimental results to construct an analysis method for the behaviors of the satellites with flexible elements., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064734063},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {Experimental Validation on Analysis Method of Behaviors of Satellites with Flexible Elements},
 volume = {2009},
 year = {2010}
}