Equilibrium Dynamics in the CR3BP with Radiating Primary and Oblate Secondary Using the Rotating Mass Dipole Model

dc.contributor.authorPerdiou, E. Angela
dc.contributor.authorVincent, Ekele Aguda
dc.contributor.authorSingh, Jagadish
dc.contributor.authorKalantonis, S. Vassilis
dc.date.accessioned2026-01-28T21:48:56Z
dc.date.issued2025-10-03
dc.description.abstractIn this study, we numerically investigate the equilibrium dynamics of a rotating system consisting of two masses connected by a massless rod within the framework of the circular restricted three-body problem. The larger primary is modeled as a radiating body and the smaller as an oblate spheroid. We explore the influence of the involved parameters, i.e., mass ratio (µ), force ratio (k), radiation pressure factor (q1), and oblateness coefficient (A2), on the number, positions, and linear stability of equilibrium points. Zero velocity curves are presented in the equatorial plane for varying values of the Jacobi constant. Up to five equilibrium points are identified of which three are collinear (L1, L2, L3) and two are non-collinear (L4, L5). The positions of all equilibria shift under variations in the perturbing parameters. While the collinear points are generally unstable, L1 can exhibit stability for certain combinations of µ, k, and q1. The non-collinear points may also be stable under specific conditions with stability zones expanding with increased parameter values. The model is applied to the irregular, elongated asteroid 951 Gaspra, for which five equilibrium points are found. Despite positional dependence on oblateness and radiation, the perturbations do not significantly affect the equilibrium points’ stability and the motion near them remains linearly unstable. The Lyapunov families of periodic orbits emanating from the collinear equilibria of this particular system are also investigated.
dc.identifier.citationPerdiou, A.E.; Vincent, A.E.; Singh, J.; Kalantonis, V.S. Equilibrium Dynamics in the CR3BP with Radiating Primary and Oblate Secondary Using the Rotating Mass Dipole Model. Mathematics2025,13, 3179. https://doi.org/10.3390/ math13193179
dc.identifier.urihttps://doi.org/10.3390/ math13193179
dc.identifier.urihttps://repository.nmu.edu.ng/handle/123456789/74
dc.language.isoen
dc.publisherMDPI
dc.subjectCR3BP
dc.subjectequilibrium points
dc.subjectperiodic orbits
dc.subjectstability
dc.subjectrotating mass dipole
dc.subjectelongated asteroid
dc.subjectradiation pressure
dc.subjectoblateness
dc.titleEquilibrium Dynamics in the CR3BP with Radiating Primary and Oblate Secondary Using the Rotating Mass Dipole Model
dc.typeArticle

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