Geometry of transit orbits in the periodically-perturbed restricted three-body problem
Joshua Fitzgerald, Shane Ross

TL;DR
This paper explores the geometric structure of transit orbits in the periodically-perturbed restricted three-body problem, extending classical methods to time-periodic systems and analyzing the phase space dynamics around periodic orbits.
Contribution
It introduces a geometric framework for understanding transit orbits in periodically-perturbed three-body systems using symplectic maps and effective Hamiltonians, extending prior unperturbed analyses.
Findings
Transit and non-transit orbit structures are preserved under periodic perturbations.
The phase space geometry around periodic orbits remains consistent with the unperturbed case.
A local conservation of an effective Hamiltonian guides the orbit dynamics in the perturbed system.
Abstract
In the circular restricted three-body problem, low energy transit orbits are revealed by linearizing the governing differential equations about the collinear Lagrange points. This procedure fails when time-periodic perturbations are considered, such as perturbation due to the sun (i.e., the bicircular problem) or orbital eccentricity of the primaries. For the case of a time-periodic perturbation, the Lagrange point is replaced by a periodic orbit, equivalently viewed as a hyperbolic-elliptic fixed point of a symplectic map (the stroboscopic Poincar\'e map). Transit and non-transit orbits can be identified in the discrete map about the fixed point, in analogy with the geometric construction of Conley and McGehee about the index-1 saddle equilibrium point in the continuous dynamical system. Furthermore, though the continuous time system does not conserve the Hamiltonian energy (which is…
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Taxonomy
TopicsSpacecraft Dynamics and Control · Quantum chaos and dynamical systems · Space Satellite Systems and Control
