@inproceedings{oai:jaxa.repo.nii.ac.jp:00007262,
 author = {榎原, 匡俊 and 大島, 武 and 石井, 信明 and 粟井, 俊弘 and 吉沢, 剛 and 松島, 幸太 and 川勝, 康弘 and 成田, 伸一郎 and Ebara, Masatoshi and Oshima, Takeshi and Ishii, Nobuaki and Kurii, Toshihiro and Yoshizawa, Takeshi and Matsushita, Kota and Kawakatsu, Yasuhiro and Narita, Shinichiro},
 book = {アストロダイナミクスシンポジウム講演後刷り集, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 摘要: 2010年5月21日に打ち上げられた､日本初の内惑星探査機｢あかつき｣について､システム設計の概要と共に､姿勢制御系の初期運用の結果を報告する｡, 具体的には､1 太陽光外乱測定結果､2 500Nスラスタ噴射時の外乱トルクから推定される推力軸と質量中心との間のズレ､について､現状を報告する｡, "AKATSUKI" is the first Japanese interplanetary explorer for inferior planets, launched in May 21st, 2010; now on its way to Venus. In this paper, the system design and some results of the initial operations of the Attitude Control System is described. In particular, 1) Results of the Solar pressure disturbance estimation, 2) Calculations of the misalignment between the spacecraft center of mass and 500N maneuver engine thrust axis, estimated from the measured disturbance during the test injection., 資料番号: AA0065115015},
 pages = {81--86},
 publisher = {宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS), Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {Initial Operation results of the Attitude Control System onboard "AKATSUKI" Venus Climate Orbiter},
 volume = {20},
 year = {2011}
}