Tokyo Metropolitan Institute of Technology
Tokyo Metropolitan University
Tokyo Metropolitan University
Tokyo Metropolitan University
Tokyo Metropolitan University
Tokyo Metropolitan University
Mitsubishi Heavy Industries Ltd.
Mitsubishi Heavy Industries Ltd.
Mitsubishi Heavy Industries Ltd.
出版者
宇宙航空研究開発機構宇宙科学研究本部
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
雑誌名
第27回宇宙エネルギーシンポジウム 平成19年度
雑誌名(英)
The Twenty-seventh Space Energy Symposium
ページ
97 - 101
発行年
2008-05
抄録（英）
This paper studies attitude and vibration control of tethered Space Solar Power Satellite (SSPS), which is the concept of a manned lunar landing to establish the lunar base. The purpose is to launch SSPS on the moon circular orbit and to build a system for supplying electric power. The large flexible panel is excited on its vibration according to change of attitude. The input torque for changing attitude is analyzed by Optimal-Control Theory and secondly, excited vibration of the panel is analyzed and then, control algorithm is studied for the system. The method of control uses the tether tension of the Mission-Function Control algorithm.
月探査衛星に適用させるテザー型SSPSの姿勢制御とパネル振動制御
