@inproceedings{oai:jaxa.repo.nii.ac.jp:00038616,
 author = {笹田, 武志 and 嶋根, 愛理 and 西田, 宏 and 森口, 孝文 and 内納, 亮平 and 孫崎, 太 and Sasada, Takeshi and Shimane, Eri and Nishida, Hiroshi and Moriguchi, Takafumi and Uchino, Ryouhei and Magosaki, Futoshi},
 book = {第57回宇宙科学技術連合講演会講演集, Proceedings of 57th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第57回宇宙科学技術連合講演会（2013年10月9日-11日. 米子コンベンションセンター（BiG SHiP）), 米子市, 鳥取県, The development of high-accuracy Micro Electro Mecanical Systems (MEMS) gyroscopes for space applications havebeen started under the framework of the JAXA Aerospace Open Laboratory program in 2012. Taking advantage ofMEMS capabilities such as small, lightweight, low power consumption, and low cost, to modify the existing gyroproducts for navigation-grade. Two approaches; (1) advanced digital compensation for temperature variation, and (2)improvements of characteristics for MEMS sensor head, are adopted to accomplish the ten times better than theperformance of existing gyros (0.1 or less degrees per hours of bias instability). This paper reports a research outline,interim results, and revealed technical issues for high-accuracy., 資料番号: AC1400032000, レポート番号: JSASS-2013-4365},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences(JSASS)},
 title = {宇宙用高精度MEMS ジャイロ開発の中間報告},
 year = {2013}
}