A generalized framework for the collinear restricted four-body problem with a central dominant mass

This study extends the classical circular restricted three-body problem (CR3BP) by introducing a dominant central primary, forming a collinear restricted four-body problem (CR4BP) that better reflects the dynamics of real planetary systems. The model remains dynamically consistent and non-degenerate when the central mass parameter μ<sub>0</sub> lies in (½, 1) and the peripheral mass μ satisfies 0 < μ < ½ (1 - μ<sub>0</sub>). It generalizes to the CR3BP by setting μ<sub>0</sub> = 0, recovering classical results. The system exhibits six libration points: four collinear and two symmetric non-collinear points forming an isosceles triangle with the peripheral primaries. Non-collinear points emerge via a saddle-node bifurcation at a critical μ = μ<sub>c</sub> and as μ increases further within the range μ<sub>c</sub> < μ < ½ (1 - μ<sub>0</sub>), these points move away from the x-axis and gradually align closer to the y-axis, while remaining symmetric with respect to the x-axis. The stability analysis reveals that collinear libration points L<sub>1</sub>, L<sub>3</sub> and L<sub>4</sub> are linearly unstable under all conditions while L<sub>2</sub> is stable in the interval 0 < μ < μ<sup>*</sup> where μ<sup>*</sup> is a critical threshold for L<sub>2</sub>. The non-collinear points are linearly stable within a defined interval μ<sub>c</sub> < μ < μ<sub>c1</sub>. Finally, these results are applied to the Saturn-Janus-Epimetheus system to illustrate the model's practical relevance.

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Publication Details

Journal
Scientific Reports
Published
2025-10-17
DOI
https://doi.org/10.1038/s41598-025-20510-y
Citations
2
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
9.99
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article

A generalized framework for the collinear restricted four-body problem with a central dominant mass

M. Javed Idrisi, Sergey V. Ershkov, Md Sanam Suraj, Elbaz I. Abouelmagd et al.
2 citations
Scientific Reports
Spacecraft Dynamics and Control
9.99
article

A generalized framework for the collinear restricted four-body problem with a central dominant mass

M. Javed Idrisi, Sergey V. Ershkov, Md Sanam Suraj, Elbaz I. Abouelmagd, Dawit Beza
article en
2 citations

Abstract

This study extends the classical circular restricted three-body problem (CR3BP) by introducing a dominant central primary, forming a collinear restricted four-body problem (CR4BP) that better reflects the dynamics of real planetary systems. The model remains dynamically consistent and non-degenerate when the central mass parameter μ<sub>0</sub> lies in (½, 1) and the peripheral mass μ satisfies 0 < μ < ½ (1 - μ<sub>0</sub>). It generalizes to the CR3BP by setting μ<sub>0</sub> = 0, recovering classical results. The system exhibits six libration points: four collinear and two symmetric non-collinear points forming an isosceles triangle with the peripheral primaries. Non-collinear points emerge via a saddle-node bifurcation at a critical μ = μ<sub>c</sub> and as μ increases further within the range μ<sub>c</sub> < μ < ½ (1 - μ<sub>0</sub>), these points move away from the x-axis and gradually align closer to the y-axis, while remaining symmetric with respect to the x-axis. The stability analysis reveals that collinear libration points L<sub>1</sub>, L<sub>3</sub> and L<sub>4</sub> are linearly unstable under all conditions while L<sub>2</sub> is stable in the interval 0 < μ < μ<sup>*</sup> where μ<sup>*</sup> is a critical threshold for L<sub>2</sub>. The non-collinear points are linearly stable within a defined interval μ<sub>c</sub> < μ < μ<sub>c1</sub>. Finally, these results are applied to the Saturn-Janus-Epimetheus system to illustrate the model's practical relevance.

Scientific ReportsVol. 15(1)
Plekhanov Russian University of Economics (RU), Sinai University (EG), Lomonosov Moscow State University (RU), Mizan Tepi University (ET), Government of India (IN), National Research Institute of Astronomy and Geophysics (EG), MIREA - Russian Technological University (RU), Manav Rachna International Institute of Research and Studies (IN)
Openalex Percentile: Top 2%
Spacecraft Dynamics and Control
9.99
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