@inproceedings{oai:jaxa.repo.nii.ac.jp:00003677,
 author = {大里, 優一郎 and 新谷, 昌人 and 東尾, 奈々 and 渡邉, 力夫 and Osato, Yuichiro and Araya, Akito and Higashio, Nana and Watanabe, Rikio},
 book = {宇宙航空研究開発機構特別資料: 第12回宇宙環境シンポジウム講演論文集, JAXA Special Publication: Proceedings of the 12th Spacecraft Environment Symposium},
 month = {Mar},
 note = {第12回 宇宙環境シンポジウム（2015年11月16日-18日. 北九州国際会議場　国際会議室）, 北九州市, 福岡県, The 12th Spacecraft Environment Symposium (November 16-18, 2015. International Conference Room, Kitakyushu International Conference Center), Kitakyushu, Fukuoka, Japan, To estimate neutral atmospheric density in the super low earth orbit by measuring drag of a spacecraft, a highly sensitive and wide-range accelerometer is required. Thus a new type of the accelerometer which consists of 6 sets of contactless optical displacement sensors and magnetic actuators is proposed. The breadboard model of the accelerometer achieved 6-DOF control with detectable acceleration of 1.0×10(exp -2)m/s(exp 2) and the measurement accuracy improved by the proposed calibration method for the magnetic actuators., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630004022, レポート番号: JAXA-SP-15-012},
 pages = {259--263},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {中性大気密度計測用6自由度加速度計の制御結果及び較正方法について},
 volume = {JAXA-SP-15-012},
 year = {2016}
}