@inproceedings{oai:jaxa.repo.nii.ac.jp:00008035,
 author = {小島, 幸高 and 藤井, 裕矩 and 草谷, 大郎 and 渡部, 武夫 and 皆川, 洋平 and 中野, 美琴 and Kojima, Yukitaka and Fujii, Hironori A. and Kusagaya, Tairo and Watanabe, Takeo and Minagawa, Yohei and Nakano, Mikoto},
 book = {第27回宇宙エネルギーシンポジウム　平成19年度, The Twenty-seventh Space Energy Symposium},
 month = {May},
 note = {In this paper, the effectiveness of vibration control is examined by employing tether on the flexible space structures like SSPS (Space Solar Power System). The vibration control is analyzed numerically to simulate the behavior of flexible space structure in a flexible panel-tether system with mathematical description in the partial differential equation, and the effectiveness is shown for the tether tension control. Vibration control experiment is also examined on an experiment model and the result is compared with that of numerical analysis. An actuator is analyzed in its performance to generate a very low tension employed for the experiment of vibration control experiment of this model. It aimed to make a numeric model about the actuator used when the vibration was controlled, to compare with an actual performance, and to optimize it to the control experiment., 資料番号: AA0063965022},
 pages = {107--111},
 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/ISAS)},
 title = {微小張力アクチュエータを用いた柔軟宇宙構造物の振動制御の実験的研究},
 year = {2008}
}