@inproceedings{oai:jaxa.repo.nii.ac.jp:00008164,
 author = {関川, 和馬 and 藤井, 裕矩 and 小島, 広久 and 渡部, 武夫 and Sekikawa, Kazuma and Fujii, Hironori and Kojima, Hirohisa and Watanabe, Takeo},
 book = {第22回宇宙エネルギーシンポジウム　平成14年度, The 22nd ISAS Space Energy Symposium March 12, 2003},
 month = {May},
 note = {Active control to suppress vibration of large solar panel is studied for a space solar power satellite employing tether tension. The solar panel is connected to a bus system through at the corners by four tethers and tether tension is used to suppress the vibration of the panel. The mission function control algorithm is employed for the control and results of numerical analysis show excellent controlled behavior. Also attitude control of a space solar power satellite is studied by actuating the movement of a tethered bus system. Actuating the length of tethers, which is employed to attain the gravity-gradient stability of the satellite, controls the movement of the bus system. The linear quadratic regulator is designed for the control and results of numerical analysis show excellent controlled behavior except for yaw attitude motion., 資料番号: AA0045915014},
 pages = {66--70},
 publisher = {宇宙科学研究所, The Institute of Space and Astronautical Science (ISAS)},
 title = {テザーの張力による太陽電池パネルの振動制御},
 year = {2003}
}