@inproceedings{oai:jaxa.repo.nii.ac.jp:00038752,
 author = {巳谷, 真司 and 茂渡, 修平 and 神澤, 拓也 and 山中, 浩二 and Mitani, Shinji and Shigeto, Shuhei and Kanzawa, Takuya and Yamanaka, Koji},
 book = {第59回宇宙科学技術連合講演会講演集, Proceedings of 59th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第59回宇宙科学技術連合講演会（2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島県, A three-axis attitude control function module was assembled into a highly integrated cubic package with 10 × 10 × 10 cm3 dimension (1U-sized). In this paper, A dynamic equations, conservation laws, sensing and control laws are described as a 3D inverted pendulum. Some demonstrations such as balancing and jumping are conducted., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600008000, レポート番号: JSASS-2015-4558},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {超小型三軸姿勢制御モジュールの研究},
 year = {2015}
}