@techreport{oai:jaxa.repo.nii.ac.jp:00006301,
 author = {遠藤, 達也 and 川井, 洋志 and 関口, 毅 and 鈴木, 秀人 and Endo, Tatsuya and Kawai, Hiroshi and Sekiguchi, Takeshi and Suzuki, Hideto},
 month = {Jan},
 note = {This is the report of a study of high performance maneuver for artificial satellite. Especially, CMG (Control Moment Gyro) aiming to agile reorientation maneuver is discussed in this report. The number and the arrangement of the CMG cluster were examined, for Rest-to-Rest maneuvering. The performance presumption parameter to the first design estimate was derived. The CMG assembly design for agile maneuver is determined by requirement of angular momentum and the moment of inertia of satellite. The result of the CMG assembly arrangement should be discussed from the point of electrical energy consumption, precise weight estimation and cost., 資料番号: AA0049054045, レポート番号: JAXA-SP-05-008},
 title = {人工衛星の高性能姿勢制御の研究},
 year = {2006}
}