@inproceedings{oai:jaxa.repo.nii.ac.jp:00007279,
 author = {地福, 亮 and 市川, 朗 and Jifuku, Ryo 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, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 本講演では､円軌道上の主衛星(Leader)に対する,従衛星(Follower)の相対軌道遷移を考察する.フォーメーション問題は,線形化された相対運動方程式であるHCW方程式の周期解で記述される.一定幅のパルス入力を用いて軌道遷移を行うとき,増速量には下限が存在するが,3回の入力で総速度変化量最小の軌道遷移が達成できる.さらに,最適レギュレータ理論を用いて準最適フィードバック制御を設計し,そのシミュレーション結果を紹介する., This paper considers formation flight along a circular orbit. The relative motion of one space craft (follower) with respect to another (leader) in a circular orbit is described by nonlinear autonomous diferential equations, and their linearized equations are known as Hill-Clohessy-Wiltshire (HCW) equations. Formation problems are formulated by the periodic solutions of HCW equations. Control inputs are assumed to be pulse inputs of a constant width, and their performance index is the total velocity change. It is shown that there exist optimal three pulse strategies. Using the optimal regulator theory, suboptimal feedback controls are designed and simulation results are given., 資料番号: AA0065115032},
 pages = {193--198},
 publisher = {宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS), Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {Formation Flight along a Circular Orbit with Pulse Input},
 volume = {20},
 year = {2011}
}