@inproceedings{oai:jaxa.repo.nii.ac.jp:00007711,
 author = {卯尾, 匡史 and 白川, 健一 and 橋本, 樹明 and 久保田, 孝 and Uo, Masashi and Shirakawa, Kenichi and Hashimoto, Tatsuaki and Kubota, Takashi},
 book = {平成15年度アストロダイナミクスシンポジウム:講演後刷り集, ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers},
 month = {Feb},
 note = {2003年5月9日に打ち上げられた小惑星探査機MUSES-Cの初期姿勢捕捉制御、巡航時定常姿勢制御系の概要と、軌道上での制御性能評価結果を報告する。太陽電池パネルの柔軟特性との干渉のRCS制御への影響について、計算機シミュレーションと軌道上ダイナミクスとの対比を行なった結果についても触れる。, JAXA/Institute of Space and Astronautical Science launched an asteroid sample and return spacecraft MUSES-C on May 9th, 2003. The spacecraft, renamed as 'HAYABUSA' (falcon), is operating normally on the orbit toward the target asteroid 'ITOKAWA'. This paper describes the operation and evaluation result of the attitude control system onboard MUSES-C spacecraft. The on-orbit attitude dynamics is also discussed focusing on the interference of flexible solar panels on the RCS (Reaction Control System) attitude control performance, through the comparison of the computer simulation and the on-orbit behavior., 資料番号: AA0046652010},
 pages = {66--71},
 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 = {HAYABUSA, on-orbit behavior of attitude dynamics and evaluation of attitude control system},
 year = {2004}
}