High-order resonant orbit manifold expansions for mission design in the planar circular restricted 3-body problem
In recent years, stable and unstable manifolds of invariant objects (such as libration points and periodic orbits) have been increasingly recognized as an efficient tool for designing transfer trajectories in space missions. However, most methods currently used in mission design rely on using eigenv...
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| Published in: | Communications in nonlinear science & numerical simulation Vol. 97; p. 105691 |
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| Main Authors: | , , |
| Format: | Journal Article |
| Language: | English |
| Published: |
Amsterdam
Elsevier B.V
01.06.2021
Elsevier Science Ltd |
| Subjects: | |
| ISSN: | 1007-5704, 1878-7274 |
| Online Access: | Get full text |
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