@inproceedings{oai:jaxa.repo.nii.ac.jp:00007417,
 author = {中宮, 賢樹 and 山川, 宏 and 吉川, 真 and Nakamiya, Masaki and Scheeres, Daniel and Yamakawa, Hiroshi and Yoshikawa, Makoto},
 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, We investigate spacecraft capture trajectories to the periodic orbits of the L1 and L2 points from interplanetary trajectories in the planar restricted Hill three-body problem are studied. 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 reduced relative to direct capture into a parabolic orbit. However, the time of flight for capture trajectories is increased. Therefore, the way of reducing of the time of flight for capture trajectories is discussed based on using stable manifolds., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064733043},
 pages = {270--274},
 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 = {Analysis of Time of Flight for Capture Trajectories to the Periodic Orbit of Libration Points},
 volume = {2008},
 year = {2009}
}