@inproceedings{oai:jaxa.repo.nii.ac.jp:00007468,
 author = {Simanjuntak, Triwanto and 津田, 雄一 and 森本, 睦子 and 川口, 淳一郎 and 澤田, 弘崇 and Simanjuntak, Triwanto and Tsuda, Yuichi and Morimoto, Mutsuko Y. and Kawaguchi, Junichiro and Sawada, Hirotaka},
 book = {第17回アストロダイナミクスシンポジウム講演後刷り集　2007, Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {Here at L2, introduced a satellite formation flying consists of two satellites powered by solar sail, the Mirror SpaceCraft (MSC) and the Detector SpaceCraft (DSC). The two satellites are separated such that the operational detector is at the focus of the mirror. Due to the instability of the collinear Lagrangian points, the desired distance between the two satellites need to be maintained. This paper addresses the control design scheme for formation keeping control. The equation of motion is derived in Hill's frame and inertial frame and then control law formulated mathematically. Halo and Lissajous orbit are considered as options for reference orbit., 資料番号: AA0063718031},
 pages = {190--193},
 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/ISAS)},
 title = {Preliminary study on satellite formation flying control around L(sub 2) using solar sail propulsion},
 year = {2008}
}