@techreport{oai:jaxa.repo.nii.ac.jp:00006054,
 author = {内田, 英樹 and 清水, 隆三 and 遠藤, 達也 and 小松, 敬治 and Uchida, Hideki and Shimizu, Ryuzo and Endo, Tatsuya and Komatsu, Keiji},
 month = {Nov},
 note = {Pointing Accuracy of sensors and stability of attitude control of spacecraft are influenced by micro-vibration transmitted from components, for example, reaction wheels and coolers, which are regarded as internal disturbance sources. Such micro-vibration should be controlled and managed on early design phase. In order to establish the control method, characteristics of the micro-vibration transmissibility have to be measured and evaluated. Thus, the measurement and testing methods of the micro-vibration are investigated., 資料番号: AA0049500070, レポート番号: JAXA-SP-06-006},
 title = {擾乱伝達計測技術の研究:構造技術の研究},
 year = {2006}
}