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arXiv 2602.08720gr-qcastro-ph.EPastro-ph.IM
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水星轨道器的后牛顿加速度

Post-Newtonian accelerations of a Mercury orbiter

University of Pisa(比萨大学);Dresden Technical University(德累斯顿工业大学)

Miriam Falletta, Gabriel Rodríguez-Moris, Sergei A. Klioner

AI总结:

本文提出了一种高精度相对论轨道模型的构建方法,用于水星轨道器,分析了后牛顿项的大小及影响。

摘要:

我们研究了水星后牛顿局部坐标系中航天器运动的相对论建模。这一研究受到启发,即水星的后牛顿引力场(以及任何其他行星的引力场)可以按多极矩展开,这些多极矩最适当地定义在局部参考系中。在以水星为中心的局部框架中,运动方程包括相对论性的局部扰动,由Schwarzschild项、Lense-Thirring进动和四极矩引起的加速度组成,以及相对论性的第三体扰动,即引力-电和引力-磁加速度,以及水星与其他太阳系天体之间的耦合项。相对论性的第三体扰动通常在所有实际应用中被忽略。在本研究中,我们分析了在水星中心框架中制定的运动方程的后牛顿项的大小,沿着两艘BepiColombo航天器的轨迹进行评估。基于此分析,我们提供了一种构建高精度相对论轨道模型的实用方法,适用于水星轨道器。

英文摘要:

We investigate the relativistic modeling of spacecraft motion in Mercury's post-Newtonian local coordinates. This investigation is motivated by the fact that Mercury's post-Newtonian gravitational field (as well as that of any other planet) admits an expansion in terms of multipole moments, which are most appropriately defined in the local reference system. The equations of motion in the Mercury-centric local frame include relativistic local perturbations, given by the Schwarzschild term, Lense-Thirring precession, and the acceleration due to the quadrupole moment, and relativistic third-body perturbations, which are the gravito-electric and gravito-magnetic accelerations, along with a coupling term between Mercury and other solar system bodies. The relativistic third-body perturbations are usually neglected in all practical applications. In this study, we analyze the magnitude of the post-Newtonian terms of the equations of motion formulated in the Mercury-centric frame, evaluating them along the trajectories of the two BepiColombo spacecrafts. Based on this analysis, we provide a practical approach for constructing a high-accuracy relativistic orbital model suitable for a Mercury orbiter.

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

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