@inproceedings{oai:jaxa.repo.nii.ac.jp:00007390,
 author = {森, 治 and 船瀬, 龍 and 津田, 雄一 and 川口, 淳一郎 and 花岡, 史紀 and 杉田, 昌行 and Mori, Osamu and Funase, Ryu and Tsuda, Yuichi and Kawaguchi, Junichiro and Hanaoka, Fuminori and Sugita, Masayuki},
 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 18th workshop on JAXA Astrodynamics and flight mechanics},
 month = {Mar},
 note = {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, 摘要: JAXAでは，深宇宙探査のための新しい推進機関として，ソーラー電力セイルを検討している．これを踏まえ，本研究では剛構造による支持を持たない大面積薄膜を有するスピン衛星の姿勢ダイナミクスを明らかにするとともに，スピン型セイルに適した姿勢制御手法を提案する．, Spinning solar sail has no structure supporting membrane, therefore estimation of the effect of membrane flexibility is one of the problems to solve for the future validation flight. In this study, we established a dynamic model including membrane vibration to handle a coupled motion of a rigid spacecraft and a flexible membrane, and focus on the consideration of attitude control method., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064733016},
 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 = {Input Shaping を用いたソーラーセイルの姿勢制御},
 volume = {2008},
 year = {2009}
}