@inproceedings{oai:jaxa.repo.nii.ac.jp:00007783,
 author = {松永, 三郎 and 宇井, 恭一 and 中谷, 幸司 and 宮下, 直己 and Matsunaga, Saburo and Ui, Kyoichi and Nakaya, Koji and Miyashita, Naoki},
 book = {平成14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 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers},
 month = {Feb},
 note = {本研究室では次世代親子衛星用のドッキング機構を提案し、その試作モデルを製作してきた。そしてその把持、引込、放出の各機能について、本研究既存の2次元衛星シミュレータを用いた実験、および地下無重力実験センター(JAMIC)の落下棟を用いた実験を行い、評価を行ったので、それらの結果について報告する。, A docking method and mechanism for mothership-daughtership nano-satellite in the near future have been proposed and a functional test model based on proposed method has been made. And 2-dimensional microgravity experiments were conducted using air floating test bed in the laboratory and 3-dimensional microgravity experiments were conducted using a drop shaft at Japan Microgravity Center (JAMIC). This paper reports the results of the experiments to verify and evaluate grasp, guide and release functions., 資料番号: AA0045497021},
 pages = {120--125},
 publisher = {宇宙科学研究所, The Institute of Space and Astronautical Science (ISAS)},
 title = {Docking mechanism for mothership-daughtership nano-satellite: Microgravity experiments to verify grasping and guiding functions},
 year = {2003}
}