@inproceedings{oai:jaxa.repo.nii.ac.jp:00007355,
 author = {樋口, 和也 and 市川, 朗 and Higuchi, Kazuya and Ichikawa, Akira},
 book = {アストロダイナミクスシンポジウム講演後刷り集, Proceedings of 19th workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部)), Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan, 摘要: 目標姿勢運動と現在の姿勢運動との相対運動方程式を導出し､その安定化制御を行うことにより､軸対称スピン衛星の姿勢制御を行う｡原点周りの線形化方程式に基づく線形制御を非線形システムに適用し､その挙動を考察する｡主に入力トルクのL(sub 1)ノルムに基づいて評価を行う｡, In this paper, we discuss attitude control of a satellite from the minimum fuel point of view. We derive equations of relative motion between a desired attitude motion and the present attitiude motion, and consider its stabilization. We design a linear feedback controller based on the linearizied equations of relative motion around the origin. The main perforamance index is the L(sub 1) norm of the feedback controller., 資料番号: AA0064734050},
 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)},
 title = {Attitude Control of an Axisymmetric Spinning Satellite},
 volume = {2009},
 year = {2010}
}