@techreport{oai:jaxa.repo.nii.ac.jp:00006064,
 author = {大谷, 崇 and 巳谷, 真司 and 濱田, 吉郎 and 山口, 功 and 葛西, 時雄 and 井川, 寛隆 and Otani, Takashi and Mitani, Shinji and Hamada, Yoshiro and Yamaguchi, Isao and Kasai, Tokio and Igawa, Hirotaka},
 month = {Nov},
 note = {A case study on advanced attitude control experiments of ETS-8 is reported in this paper. ETS-8 is scheduled to be launched on a H2A launch vehicle in 2006. In this experiment, spacecraft attitude control techniques for MIMO (Multi Input Multi Output) parameter-varying system will be tested on-orbit using advanced control theory such as gain-scheduling control, and so on. The purpose of this experiment is to establish the control system design method for extremely precise attitude control of large scale flexible spacecraft., 資料番号: AA0049500080, レポート番号: JAXA-SP-06-006},
 title = {ETS-8軌道上制御実験},
 year = {2006}
}