Department of Aeronautics and Astronautics, School of Engineering, University of Tokyo
JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC)
JAXA Space Exploration Center, Japan Aerospace Exploration Agency (JAXA)(JSPEC)
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)
雑誌名
アストロダイナミクスシンポジウム講演後刷り集
雑誌名(英)
Proceedings of 18th workshop on JAXA Astrodynamics and flight mechanics
巻
2008
ページ
248 - 252
発行年
2009-03
会議概要（会議名, 開催地, 会期, 主催者等）（英）
Symposium on Flight Mechanics and Astrodynamics 2008 (July 28-29, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan
抄録（英）
In this study a formation flying, consists of two sailcrafts, is proposed around Lagrangian points of Sun-Earth system. These Sailcrafts are ought to have constant distance to emulate a conceptual long baseline space telescope. Here, few strategies are proposed and shown relatively small required sail area for geometrical frozen fomation. Additionally, this study shows the succesful implementation of feedforward control in combination with proximity time-varrying feedback control to actively maintain the constant distance of the two satellites.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
Formation Control of Sailcfrats around Collinear Lagrangian Points
