@inproceedings{oai:jaxa.repo.nii.ac.jp:00038696,
 author = {関口, 毅 and 松本, 秀一 and 神澤, 拓也 and 野口, 一秀 and 佐藤, 康志 and 東野, 勇 and Sekiguchi, Takeshi and Matsumoto, Shuichi and Kanzawa, Takuya and Noguchi, Kazuhide and Sato, Koshi and Higashino, Isamu},
 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, Star Tracker (STT) has come into wide use as main attitude sensor instead of the Earth sensor for its accurate and autonomous characteristics. Meanwhile there are a lot of STT manufacturers and they have define the performances and functions of STT in different ways, so it's difficult to compare the performances of STT appropriately. This paper presents the results of study for the Error provision of STT., 資料番号: AC1500056000, レポート番号: JSASS-2014-4454},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {スタートラッカの誤差規定に関する検討},
 year = {2014}
}