@inproceedings{oai:jaxa.repo.nii.ac.jp:00007654,
 author = {中村, 英之 and 升谷, 保博 and 宮崎, 文夫 and Nakamura, Hideyuki and Masutani, Yasuhiro and Miyazaki, Fumio},
 book = {平成16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 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers},
 month = {Mar},
 note = {This paper proposes a control method of resting a tumbling uncooperative satellite by continuously applying forces to a fixed point on the satellite. A simple feedback control law, which does not require excessive thrust, is derived using Lyapunov theory. Several simulation results show that the proposed control law makes the angular velocity converge to 0 even if there are observation errors in the angular velocity of the satellite or identification error in the location of thrust., 資料番号: AA0047897021},
 pages = {115--120},
 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 = {Angular velocity control of tumbling uncooperative satellite based on Lyapunov theory},
 year = {2005}
}