Hierarchical three-body problem at high eccentricities = simple pendulum II: octupole including Brown’s Hamiltonian

ABSTRACT The very long-term evolution of the hierarchical restricted three-body problem with a massive perturber is analysed analytically in the high eccentricity regime. Perturbations on the time-scale of the outer orbit can accumulate over long time-scales and be comparable to the effect of the octupole term. These perturbations are described by Brown’s Hamiltonian – having different forms in the literature. We show that at the high eccentricity regime – the effect of Brown’s Hamiltonian is an azimuthal precession of the eccentricity vector and can be solved analytically. In fact, the dynamics are equivalent to a simple pendulum model allowing an explicit flip criterion.

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Publication Details

Journal
Monthly Notices of the Royal Astronomical Society Letters
Published
2024-09-18
DOI
https://doi.org/10.1093/mnrasl/slae089
Citations
11
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
14.29
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article

Hierarchical three-body problem at high eccentricities = simple pendulum II: octupole including Brown’s Hamiltonian

Boaz Katz, Ygal Klein
11 citations
Monthly Notices of the Royal Astronomical Society Letters
Spacecraft Dynamics and Control
14.29
article

Hierarchical three-body problem at high eccentricities = simple pendulum II: octupole including Brown’s Hamiltonian

Boaz Katz, Ygal Klein
article en
11 citations

Abstract

ABSTRACT The very long-term evolution of the hierarchical restricted three-body problem with a massive perturber is analysed analytically in the high eccentricity regime. Perturbations on the time-scale of the outer orbit can accumulate over long time-scales and be comparable to the effect of the octupole term. These perturbations are described by Brown’s Hamiltonian – having different forms in the literature. We show that at the high eccentricity regime – the effect of Brown’s Hamiltonian is an azimuthal precession of the eccentricity vector and can be solved analytically. In fact, the dynamics are equivalent to a simple pendulum model allowing an explicit flip criterion.

Monthly Notices of the Royal Astronomical Society LettersVol. 535(1)
Weizmann Institute of Science (IL)
Openalex Percentile: Top 2%
Spacecraft Dynamics and Control
14.29
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