Exploring the Influence of Oblateness on Asymptotic Orbits in the Hill Three-Body Problem

We examine the modified Hill three-body problem by incorporating the oblateness of the primary body and focus on its asymptotic orbits. Specifically, we analyze and characterize homoclinic and heteroclinic connections associated with the collinear equilibrium points. By systematically varying the oblateness parameter, we determine conditions for the existence and location of these orbits. Our results confirm the presence of both homoclinic orbits, where trajectories asymptotically connect an equilibrium point to itself, and heteroclinic orbits, which establish connections between two distinct equilibrium points, via their stable and unstable invariant manifolds, which are computed both analytically and numerically. To achieve precise computations, we employ differential correction techniques and leverage the system’s inherent symmetries. Numerical calculations are carried out for orbit multiplicities up to twelve, ensuring a comprehensive exploration of the dynamical properties.

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Publication Details

Journal
AppliedMath
Published
2025-03-17
DOI
https://doi.org/10.3390/appliedmath5010030
Citations
3
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
14.98
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article

Exploring the Influence of Oblateness on Asymptotic Orbits in the Hill Three-Body Problem

V. S. Kalantonis
3 citations
AppliedMath
Spacecraft Dynamics and Control
14.98
article

Exploring the Influence of Oblateness on Asymptotic Orbits in the Hill Three-Body Problem

V. S. Kalantonis
article en
3 citations

Abstract

We examine the modified Hill three-body problem by incorporating the oblateness of the primary body and focus on its asymptotic orbits. Specifically, we analyze and characterize homoclinic and heteroclinic connections associated with the collinear equilibrium points. By systematically varying the oblateness parameter, we determine conditions for the existence and location of these orbits. Our results confirm the presence of both homoclinic orbits, where trajectories asymptotically connect an equilibrium point to itself, and heteroclinic orbits, which establish connections between two distinct equilibrium points, via their stable and unstable invariant manifolds, which are computed both analytically and numerically. To achieve precise computations, we employ differential correction techniques and leverage the system’s inherent symmetries. Numerical calculations are carried out for orbit multiplicities up to twelve, ensuring a comprehensive exploration of the dynamical properties.

AppliedMathVol. 5(1)
University of Patras (GR)
Openalex Percentile: Top 2%
Spacecraft Dynamics and Control
14.98
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