Low-energy escape from the Sun-Earth L2 halo orbit utilizing unstable manifolds and lunar gravity assist

Hongru Chen, Yasuhiro Kawakatsu, Toshiya Hanada

研究成果: 著書/レポートタイプへの貢献会議での発言

抄録

The paper investigates the escape strategy using the unstable manifolds of the Sun-Earth L2 halo orbit and lunar gravity assist. There are four cases of intersection of the manifold tubes associated with halo orbits and the orbit of the Moon. The four intersections have different V with respect to the Moon. The corresponding lunar gravity assists can result in a range of escape trajectories, granting choices for the extended mission of halo orbits. In order to satisfy the lunar encounter requirements, the strategy and ΔV costs of phasing maneuvers are presented as well.

元の言語英語
ホスト出版物のタイトルAdvances In The Astronautical Sciences
出版者Univelt Inc.
ページ3679-3691
ページ数13
152
ISBN(電子版)9780877036111
出版物ステータス出版済み - 2014
イベント24th AAS/AIAA Space Flight Mechanics Meeting, 2014 - Mexico, 米国
継続期間: 1 26 20141 30 2014

その他

その他24th AAS/AIAA Space Flight Mechanics Meeting, 2014
米国
Mexico
期間1/26/141/30/14

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Sun
escape
Moon
halos
Gravitation
sun
Orbits
Earth (planet)
gravity
gravitation
orbits
moon
intersections
energy
trajectory
maneuvers
cost
encounters
Trajectories
trajectories

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

これを引用

Chen, H., Kawakatsu, Y., & Hanada, T. (2014). Low-energy escape from the Sun-Earth L2 halo orbit utilizing unstable manifolds and lunar gravity assist. : Advances In The Astronautical Sciences (巻 152, pp. 3679-3691). Univelt Inc..

Low-energy escape from the Sun-Earth L2 halo orbit utilizing unstable manifolds and lunar gravity assist. / Chen, Hongru; Kawakatsu, Yasuhiro; Hanada, Toshiya.

Advances In The Astronautical Sciences. 巻 152 Univelt Inc., 2014. p. 3679-3691.

研究成果: 著書/レポートタイプへの貢献会議での発言

Chen, H, Kawakatsu, Y & Hanada, T 2014, Low-energy escape from the Sun-Earth L2 halo orbit utilizing unstable manifolds and lunar gravity assist. : Advances In The Astronautical Sciences. 巻. 152, Univelt Inc., pp. 3679-3691, 24th AAS/AIAA Space Flight Mechanics Meeting, 2014, Mexico, 米国, 1/26/14.
Chen H, Kawakatsu Y, Hanada T. Low-energy escape from the Sun-Earth L2 halo orbit utilizing unstable manifolds and lunar gravity assist. : Advances In The Astronautical Sciences. 巻 152. Univelt Inc. 2014. p. 3679-3691
Chen, Hongru ; Kawakatsu, Yasuhiro ; Hanada, Toshiya. / Low-energy escape from the Sun-Earth L2 halo orbit utilizing unstable manifolds and lunar gravity assist. Advances In The Astronautical Sciences. 巻 152 Univelt Inc., 2014. pp. 3679-3691
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