Abstract
We explore two ways of gravity assists concerning three-body energy and twobody energy in the planar restricted four-body problem. The first is concerned with changing dynamical objects of the restricted three-body problem such as energy of orbits and energetically forbidden region via gravity assists within the framework of the restricted four-body problem. As an application, we propose a method of finding nominal transfer trajectories between Lyapunov orbits of different energies without fuel consumption. The second is concerned with revealing time-dependent analogues of invariant manifolds of resonant orbits directly in the restricted four-body problem. For this purpose, we employ the method of Lagrangian coherent structures as a visual aid. We then identify homoclinic and heteroclinic connections of resonant orbits in the restricted four-body problem, which could be applicable to the low-energy exploration of the moons of Jupiter.
Original language | English |
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Title of host publication | Advances in the Astronautical Sciences |
Publisher | Univelt Inc. |
Pages | 503-522 |
Number of pages | 20 |
Volume | 152 |
ISBN (Print) | 9780877036111 |
Publication status | Published - 2014 |
Event | 24th AAS/AIAA Space Flight Mechanics Meeting, 2014 - Mexico, United States Duration: 2014 Jan 26 → 2014 Jan 30 |
Other
Other | 24th AAS/AIAA Space Flight Mechanics Meeting, 2014 |
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Country/Territory | United States |
City | Mexico |
Period | 14/1/26 → 14/1/30 |
ASJC Scopus subject areas
- Aerospace Engineering
- Space and Planetary Science