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.
Authors
- M. Javed Idrisi (ORCID: https://orcid.org/0000-0003-1435-6780)
- Sergey V. Ershkov (ORCID: https://orcid.org/0000-0002-6826-1691)
- Md Sanam Suraj (ORCID: https://orcid.org/0000-0003-4630-3181)
- Elbaz I. Abouelmagd (ORCID: https://orcid.org/0000-0002-2800-4527)
- Dawit Beza
Institutions
- 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)
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