JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

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Other TitleAttitude and vibration control of solar panel for tethered SSPS applied for lunar exploration
Author(jpn)中野 美琴; 藤井 裕矩; 草谷 大郎; 渡部 武夫; 皆川 洋平; 小島 幸高; 布施 嘉春; 新津 真行; 安間 健一
Author(eng)Nakano, Mikoto; Fujii, Hironori; Kusagaya, Tairo; Watanabe, Takeo; Minagawa, Yohei; Kojima, Yukitaka; Fuse, Yoshiharu; Niitsu, Mayuki; Anma, Kenichi
Author Affiliation(jpn)東京都立科学技術大学; 首都大学東京; 首都大学東京; 首都大学東京; 首都大学東京; 首都大学東京; 三菱重工業; 三菱重工業; 三菱重工業
Author Affiliation(eng)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.
Issue Date2008-05
PublisherInstitute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
Publication title第27回宇宙エネルギーシンポジウム 平成19年度
The Twenty-seventh Space Energy Symposium
Start page97
End page101
Publication date2008-05
AbstractThis 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.
Keywordssolar power satellite; tethered satellite; lunar exploration; electric power supply; lunar base; lunar orbit; rectenna; satellite attitude control; vibration damping; numerical analysis; structural vibration; 太陽発電衛星; テザー衛星; 月探査; 電力供給; 月面基地; 月周回軌道; レクテナ; 衛星姿勢制御; 振動減衰; 数値解析; 構造振動
Document TypeConference Paper
JAXA Categoryシンポジウム・研究会

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