| Issue |
A&A
Volume 702, October 2025
|
|
|---|---|---|
| Article Number | A161 | |
| Number of page(s) | 13 | |
| Section | Planets, planetary systems, and small bodies | |
| DOI | https://doi.org/10.1051/0004-6361/202453589 | |
| Published online | 16 October 2025 | |
Resonance capture and stability analysis for planet pairs under Type I disk migration
1
Institute for Astronomy, School of Physics, Zhejiang University,
Hangzhou
310027,
PR
China
2
Department of Physics, National University of Singapore,
Singapore
117542,
Singapore
★ Corresponding authors: llh_astro@zju.edu.cn; bbliu@zju.edu.cn; zekai77@u.nus.edu
Received:
23
December
2024
Accepted:
1
September
2025
We present a theoretical framework for investigating a two-planet system undergoing convergent type I migration in a protoplanetary disk. Our study identifies the conditions for resonant capture and subsequent dynamical stability. By deriving analytical criteria for general j:j − 1 first-order mean-motion resonances (MMRs) applicable to planet pairs with arbitrary mass ratios, we validate these predictions through N-body simulations. The key results are demonstrated in τm−τm/τe plots, where τm and τe are the timescales of the angular momentum and eccentricity damping, respectively. Specifically, we determine which combinations of orbital damping timescales allow for capture into resonance, showing that too fast migration or too strong eccentricity damping inhibit successful capture. After capture, the subsequent evolution can be classified into three regimes: stable trap, overstable trap and escape. Importantly, resonant capture always remains stable when the inner planet significantly outweighs the outer one. In contrast, when the mass of the inner planet is lower than or comparable to that of the outer planet, the system transitions from the stable to overstable trap, and eventually escapes the resonance, as the relative strength of eccentricity damping to migration (τm/τe) decreases.
Key words: methods: analytical / celestial mechanics / planets and satellites: dynamical evolution and stability
© The Authors 2025
Open Access article, published by EDP Sciences, under the terms of the Creative Commons Attribution License (https://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
This article is published in open access under the Subscribe to Open model. Subscribe to A&A to support open access publication.
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.