@article{oai:kanazawa-u.repo.nii.ac.jp:00009718,
 author = {泉田, 啓 and 室津, 義定 and 長岡, 秀行 and 三ツ矢, 明},
 issue = {6},
 journal = {日本ロボット学会誌 = Journal of the Robotics Society of Japan},
 month = {Sep},
 note = {A hardware satellite model with thrusters and a control moment gyro (CMG) is constructed to discuss position/attitude control methods for a ground testbed simulating a space robot. A bang-bang position control and two attitude control methods, i.e., a Lyapunov-type controller and an exact-linearization-based controller, are designed. Hardware experiments as well as numerical simulations show the feasibility of the modeling and the controllers. It is also shown that the developed position/attitude control system has enough performance for the ground testbed.},
 pages = {824--831},
 title = {宇宙ロボット実験システムのための位置姿勢制御},
 volume = {16},
 year = {1998}
}