@inproceedings{oai:jaxa.repo.nii.ac.jp:00007598,
 author = {宇井, 恭一 and 松永, 三郎 and Ui, Kyoichi and Matsunaga, Saburo},
 book = {第15回アストロダイナミクスシンポジウム講演後刷り集　2005, Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {超小型衛星を繰り返し回収・結合・放出する機能を持つ把持引込型ドッキング技術に関連し、試作した機能実証モデルを対象とした把持制御則を提案して、把持機能実証実験を行った。具体的には、ドッキング機構が有する把持空間内で制御誤差を有する超小型衛星を確実に把持することを目的として、把持機能を最小限の構成で実現するための機構・制御システムを構築し、微小重力実験によって衛星に対する制御精度要求を抽出し、その妥当性を評価した。, Laboratory for Space Systems researches a grasping/guiding type docking mechanism. The mechanism has a grasping function to fix relative position and attitude between a nano-satellite and the mechanism and a guiding function to dock a nano-satellite. In the paper, a grasping function is explained in detail. The function has a large grasping space to permit control errors of a nano-satellite, grasps it into the space. A grasping control algorithm consists of three routines which check the approach of a nano-satellite and the beginning/end of the grasping. This paper discusses feasibility of the grasping function including practical mechanisms and control algorithms through microgravity experiments., 資料番号: AA0063480033},
 pages = {210--215},
 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 = {Grasping control of grasping/guiding-type docking mechanism for nano-satellite},
 year = {2006}
}