A novel ephemeris model for Martian moons incorporating their free rotation
Yongzhang Yang, Kai Huang, Jianguo Yan, Yuqiang Li

TL;DR
This paper develops a high-precision coupled orbit-rotation model for Martian moons Phobos and Deimos, improving ephemeris accuracy and providing insights into their rotational dynamics and orbital differences.
Contribution
It introduces a novel coupled orbit-rotation model for Martian moons, integrating rotational equations with orbital dynamics for the first time.
Findings
Orbital differences between models are within 300 meters for Phobos and 125 meters for Deimos.
Orientation parameters align well with IAU standards.
Perturbations from main asteroids and mutual torques are negligible in orbital effects.
Abstract
High precision ephemerides not only support space missions, but can also be used to study the origin and future of celestial bodies. In this paper, a coupled orbit rotation dynamics model that fully takes into account the rotation of the Martian moons is developed. Phobos and Deimos rotation are firstly described by Eulerian rotational equations, and integrated simultaneously with the orbital motion equations. Orbital and orientational parameters of Mars satellites were simultaneously obtained by numerical integration for the first time. In order to compare the differences between our newly developed model and the one now used in the ephemerides, we first reproduced and simulated the current model using our own parameters, and then fit it to the IMCCE ephemerides using least square procedures. The adjustment test simulations show Phobos and Deimos orbital differences between the refined…
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