@inproceedings{oai:jaxa.repo.nii.ac.jp:00007413,
 author = {川口, 淳一郎 and 森本, 睦子 and Simanjuntak, Triwanto and Kawaguchi, Junichiro and Morimoto, Mutsuko Y.},
 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 18th workshop on JAXA Astrodynamics and flight mechanics},
 month = {Mar},
 note = {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, 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., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064733039},
 pages = {248--252},
 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 = {Formation Control of Sailcfrats around Collinear Lagrangian Points},
 volume = {2008},
 year = {2009}
}