@inproceedings{oai:jaxa.repo.nii.ac.jp:00007713,
 author = {吉河, 章二 and 山田, 克彦 and Yoshikawa, Shoji and Yamada, Katsuhiko},
 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 = {外部から繰り返しインパルスを入力することでタンブリング衛星の角運動量を減衰させる制御において、接触モデルにゲイン不確定性がある場合に角運動量が0収束する条件について考察する。, An angular momentum control of a tumbling spacecraft is discussed. The proposed control method is to apply an impulse by a space robot arm, to measure and control the relative position and attitude between the target spacecraft, and then to apply another impulse until the rotational motion of the target spacecraft is well damped. A discrete controller is designed using the simplified equations of rotational motion through appropriate coordinate transformation. The stationary response under contact model uncertainty is investigated and stability condition is analytically derived. Numerical simulations are given to validate the proposed approach., 資料番号: AA0046652012},
 pages = {76--83},
 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 momentum control of tumbling spacecraft by repetitive impulse inputs},
 year = {2004}
}