@inproceedings{oai:jaxa.repo.nii.ac.jp:00038674,
 author = {井澤, 克彦 and 山中, 浩二 and 松本, 政信 and 古幡, 智 and Izawa, Katsuhiko and Yamanaka, Koji and Matsumoto, Masanobu and Furuhata, Satoshi},
 book = {第58回宇宙科学技術連合講演会講演集, Proceedings of 58th Space Sciences and Technology Conference},
 month = {Nov},
 note = {第58回宇宙科学技術連合講演会（2014年11月12日-14日. 長崎ブリックホール), 長崎市, 長崎県, New two attitude control equipment, Reaction Wheel Assembly Type S and Inertial Reference Unit TypeⅢ-C will be launched and flight verified on SLATS (Super Low Altitude Test Satellite). These equipment had  co-developed by JAXA and Mitsubishi Precision Co., Ltd had been co-developed in the Development Program of Strategic Components and will expected to be a standard attitude control equipment of many domestic satellites.  This paper describes its specifications, design, and qualification test results. And the philosophy of space verification on SLATS for two equipment are shown., 資料番号: AC1500033000, レポート番号: JSASS-2014-4077},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {超低高度衛星搭載の姿勢制御機器（リアクションホイール,慣性基準装置）とその宇宙実証},
 year = {2014}
}