@inproceedings{oai:jaxa.repo.nii.ac.jp:00007302,
 author = {中宮, 賢樹 and 川勝, 康弘 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, Transfers from the Earth to the Halo orbits by exploiting the stable manifolds, which are the characteristic of the dynamical system in the three-body problem are investigated. First, the conditions for the transfer to the Halo orbits such as the altitude of perigee and the orbital inclination are shown. Next, the launch window for the lift-off to the Halo orbit using stable manifold at the Japanese launch site is discussed., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065115055},
 pages = {347--350},
 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 = {A study of the transfer trajectories to Halo orbits using stable manifolds},
 volume = {20},
 year = {2011}
}