@inproceedings{oai:jaxa.repo.nii.ac.jp:00007252,
 author = {津田, 雄一 and 佐伯, 孝尚 and 船瀬, 龍 and 三桝, 裕也 and 白澤, 洋次 and 卯尾, 匡史 and 河内, 宏道 and 石橋, 史朗 and 谷口, 正 and Tsuda, Yuichi and Saiki, Takanao and Funase, Ryu and Mimasu, Yuya and Shirasawa, Yoji and Uo, Masahi and Kawauchi, Hiromichi and Ishibashi, Shiro and Taniguchi, Sho},
 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, This paper describes the attitude determination and control system and an analysis for the initial on-orbit attitude determination and control operation of IKAROS solar power sail demonstration spacecraft. IKAROS is a spin stabilized spacecraft equipped with a solar sail, which works as a very large flexible structure. The attitude control is realized by the newly developed gas-liquid equilibrium thruster system. IKAROS uses a sun sensor and a downlink Doppler modulation for the attitude determination. This paper focuses on these distinctive aspects of the IKAROS attitude system, and shows an initial flight result with some discussions., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065115005},
 pages = {26--30},
 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 = {Attitude Determination and Control Operation of IKAROS in Initial On-Orbit Phase},
 volume = {20},
 year = {2011}
}