@inproceedings{oai:jaxa.repo.nii.ac.jp:00007751,
 author = {尾曲, 邦之 and 岡田, 英人 and 松永, 三郎 and Omagari, Kuniyuki and Okada, Hideto and Matsunaga, Saburo},
 book = {平成15年度アストロダイナミクスシンポジウム:講演後刷り集, ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers},
 month = {Feb},
 note = {軌道上サービスを行う宇宙機は、衛星や構造物の検査、アームによる修理、組立作業をしつつ通信を行うなど、状況に応じて多様な制御を必要とする。本研究では、リアクション・ホイールとコントロール・モーメント・ジャイロ(CMG)の双方の機能を併せ持ち、必要に応じてこれらの機能を切り替えて使用できるVS-CMGに注目し、その試験モデルを製作した。また、2次元衛星シミュレータ装置を用いて、基本性能データを取得した。本稿ではその概要と結果について報告する。, A spacecraft for in-orbit servicing needs various attitude control tasks. For example, there are repair or building using robotic arm, rapid maneuvering for inspection or antenna to be pointed to the ground station, and so on. For such situations, Variable Speed Control Moment Gyro (VS-CMG) is suitable. VS-CMG is a kind of CMG that can control its rotational speed like a reaction wheel. Therefore, VS-CMG control logic can be changed from reaction wheel (RW) based logic to CMG based logic or the contrary of that. By using VS-CMC, a satellite for in-orbit servicing can generate high torque in CMG based control logic when torquing the robotic arm and can stabilize its attitude to the Earth in RW based control logic to save energy consumption. In this study, an experimental model of VS-CMG was made and 2-dimentional ground experiment was conducted in which a satellite simulator equipped with the VS-CMG is floating by air pressure and can move using air thrusters., 資料番号: AA0046652050},
 pages = {310--315},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {Test model and ground experiment of VS-CMG for in-orbit servicing},
 year = {2004}
}