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Low-energy weak stability boundary transfers to Pluto's moons: Preliminary trajectory design via triangular libration point

  • Published:2019-03 Issue: Volume:156 Page:219-233
  • ISSN:0094-5765
  • Container-title:Acta Astronautica
  • language:en
  • Short-container-title:Acta Astronautica

Author:

Liang Yuying,Xu Ming,Xu Shijie

Funder

National Natural Science Foundations of China

Central Universities

Academic Excellence Foundation of BUAA

Space Science Foundation of China

Shanghai Space Science and Technology Innovation Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference50 articles.

1. Sun-perturbed Earth-to-Moon transfers with ballistic capture;Belbruno;J. Guid. Contr. Dynam.,1993

2. Resonance transition associated to weak capture in the restricted three- body problem;Belbruno;Adv. Space Res.,2008

3. Resonant motion, ballistic escape, and their applications in astrodynamics;Topputo;Adv. Space Res.,2008

4. Calculation of weak stability boundary ballistic lunar transfer trajectories;Belbruno,2000

5. On optimal two-impulse Earth–Moon transfers in a four-body model;Topputo;Celestial Mech. Dyn. Astron.,2013

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Leveraging L3 to transfer to L4 in the Sun-perturbed Earth-Moon system;Acta Astronautica;2021-12

2. The role of the mass ratio in ballistic capture;Monthly Notices of the Royal Astronomical Society;2020-08-24

3. Capturing an Asteroid via Triangular Libration Points;Journal of Guidance, Control, and Dynamics;2020-06

4. Potential Launch Opportunities for a SmallSat Mission around the Moon Injected during a Lunar Flyby En Route to Mars;Mathematical Problems in Engineering;2019-09-24
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