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The low-energy planetary flyby orbit could be temporarily captured by the planet and earn at least one more close encounter chance for the planet exploration. We propose a concept of effective planetary flyby to investigate the dynamical mechanism of low-energy flyby orbits in the Sun-planet planar circular restricted three-body problem.

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This page is a summary of: Low-Energy Planetary Flyby in the Sun-Planet Restricted Three-Body Problem, Journal of Guidance Control and Dynamics, July 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g008137.
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