@inproceedings{oai:jaxa.repo.nii.ac.jp:00007301,
 author = {田中, 啓太 and 川口, 淳一郎 and Tanaka, Keita and Kawaguchi, Junichiro},
 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, Invariant manifolds theory is useful to design low delta-V trajectories using planet's gravity as much as possible. Many of the previous studies on trajectory design using invariant manifolds assumed Poincare sections being parallel to x or y axes in (x, y) Cartesian coordinates and connected two manifolds on the sections. The way to define Poincare sections are, however, not have to be limited in (x, y) coordinates and you can assume them in various ways depending on problems you deal with. In case of S/C trajectory design, it is better to take Poincare sections in (r, theta) coordinates so that you can easily check apoapsis and periapsis of S/C. In this study, we propose a successful trajectory design method using invariant manifolds by having Poincare sections in new ways., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065115054},
 pages = {336--346},
 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 = {Trajectory Design between Jovian Moons Guided by Invariant Manifolds},
 volume = {20},
 year = {2011}
}