@article{oai:jaxa.repo.nii.ac.jp:00022487,
 author = {山下, 哲生 and 濱田, 吉郎 and 山口, 功 and 長塩, 知之 and 木田, 隆 and Yamashita, Tetsuo and Hamada, Yoshiro and Yamaguchi, Isao and Nagashio, Tomoyuki and Kida, Takashi},
 issue = {802},
 journal = {日本機械学会論文集Ｃ編, Transactions of the Japan Society of Mechanical Engineers. C},
 month = {Jun},
 note = {This paper presents an application of the model predictive control to flexible spacecraft attitude maneuver. The objective of the study is to demonstrate an experimental feasibility of optimal attitude controllers suppressing the flexible appendage vibration under the actuator saturation. For the purpose, we study two approaches in the model predictive control framework. One is to use the frequency-shaped linear quadratic cost with finite horizon, and the other is to apply the robust control theory. Through ground experiments using a single axis air bearing table, as well as numerical studies for ETS-VIII spacecraft, their abilities are shown and compared., 資料番号: PA1420038000},
 pages = {1935--1948},
 title = {大型柔軟衛星のロバスト姿勢制御（入力拘束を考慮したモデル予測制御の適用）},
 volume = {79},
 year = {2013}
}