@inproceedings{oai:jaxa.repo.nii.ac.jp:00007282,
 author = {中宮, 賢樹 and 津田, 雄一 and 川勝, 康弘 and Nakamiya, Masaki and Tsuda, Yuichi and Kawakatsu, Yasuhiro},
 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, We present the guidance approach for the Small Solar Power Sail Demonstrator, IKAROS. This approach will be used for future solar power sail missions. First, we show the range of orbital controllability, which is severely restricted by the attitude constraint due to the power and communication. Second, we also show the adaptive guidance method, in which guidance parameters are updated based on the estimation of the spacecraft's parameters such as the area and reflectivity coefficient of the sail., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065115035},
 pages = {211--214},
 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 = {A study of the guidance approach for the Small Solar Power Sail Demonstrator (IKAROS)},
 volume = {20},
 year = {2011}
}