@inproceedings{oai:jaxa.repo.nii.ac.jp:00007276,
 author = {中宮, 賢樹 and 川勝, 康弘 and Simanjuntak, Triwanto and Nakamiya, Masaki and Kawakatsu, Yasuhiro},
 book = {アストロダイナミクスシンポジウム講演後刷り集, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {第20回アストロダイナミクスシンポジウム (2010年7月26-27日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, In this paper we address natural formation flying around L2 point of the Sun-Earth Circular Restricted Three-Body Problem (CR3BP) systems. Halo orbit is choosen as the reference orbit for the leader and the follower is conceived to follow loosely. This type of formation will be useful in future for constructing space based ports, long-baseline space telescope, sun-shielded astronomical spacecraft, etc. We approach this problem by utilizing Dynamical System Theory (DST)., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065115029},
 pages = {175--183},
 publisher = {宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS), Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {Design of Loose Formation Flying in the Vicinity of Halo Orbits Based on Initial Set Values},
 volume = {20},
 year = {2011}
}