@inproceedings{oai:jaxa.repo.nii.ac.jp:00007449,
 author = {中宮, 賢樹 and Scheeres, Daniel and 山川, 宏 and 吉川, 真 and Nakamiya, Masaki and Scheeres, Daniel and Yamakawa, Hiroshi and Yoshikawa, Makoto},
 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 = {We investigate spacecraft capture trajectories to the periodic orbits of the L1 and L2 points in the planar restricted Hill three-body problem are studied. The specific focus is on transfer to these vicinities from interplanetary trajectories. This application is motivated by future plan to use the Sun-Earth and Sun-Mars collinear libration points as space hub for Mars Mission. We utilize stable manifolds for capture trajectories to periodic orbits around the libration points. As a result, the cost of capture into a periodic orbit is also reduced relative to direct capture into a parabolic orbit. The way of linking between interplanetary transfer trajectories and the stable manifold is also discussed., 資料番号: AA0063718012},
 pages = {63--68},
 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 = {A study of capture trajectories to the vicinity of L1 and L2 points},
 year = {2008}
}