Geometry of transit orbits in the periodically-perturbed restricted three-body problem
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DOI: 10.1016/j.asr.2022.04.029
Abstract: In the circular restricted three-body problem, low energy transit orbits are revealed by linearizing the governing dif-ferential equations about the collinear Lagrange points. This procedure fails when time-periodic perturbations are considered, such as perturbation due… read more here.
Keywords: time; problem; geometry; restricted three ... See more keywords