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arXiv 1904.02253astro-ph.EPastro-ph.SR
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开普勒要素的潮汐演化

Tidal evolution of the Keplerian elements

Gwenaël Boué, Michael Efroimsky

摘要:

我们解决的开普勒轨道要素的速率在两个合作伙伴的潮汐扰动的两体问题的表达式。这些比率的公式在文献中以各种形式出现,有时有错误。我们从头开始重新考虑这些速率的推导,并得出拉格朗日型方程,它在某些细节上不同于考拉(1964)以前得到的相应方程。我们还列出了$da/dt$、$de/dt$和$di/dt$的详细表达式,以订购$e^4$。它们不同于Kaula的表达式,Kaula的表达式包含冗余因子$M/(M+M^{\prime}),$,其中$M$和$M^{\prime}$是初级和次级的质量。由于考拉对地月系统感兴趣,这个多余的因素接近统一,对他的发展并不重要。这个因素,但是,必须恢复时,考拉的理论是适用于一个二进制组成的合作伙伴的可比质量。我们已经发现,虽然在$da/dt$或$de/dt$中简单地对初级和次级的输入求和是合法的,但是对于$di/dt$来说情况并非如此。因此,我们对$di/dt$的表达式在两个方面不同于Kaula的表达式。第一,当拱点进动是均匀的时,由于二次耗散的贡献是平均的。第二,我们得到了一个由于角动量守恒而出现的附加项:轨道倾角的变化引起主星赤道面的变化。

英文摘要:

We address the expressions for the rates of the Keplerian orbital elements within a two-body problem perturbed by the tides in both partners. The formulae for these rates have appeared in the literature in various forms, at times with errors. We reconsider, from scratch, the derivation of these rates and arrive at the Lagrange-type equations which, in some details, differ from the corresponding equations obtained previously by Kaula (1964). We also write down detailed expressions for $da/dt$, $de/dt$ and $di/dt$, to order $e^4$. They differ from Kaula's expressions which contain a redundant factor of $M/(M+M^{\prime}),$ with $M$ and $M^{\prime}$ being the masses of the primary and the secondary. As Kaula was interested in the Earth-Moon system, this redundant factor was close to unity and was unimportant in his developments. This factor, however, must be reinstated when Kaula's theory is applied to a binary composed of partners of comparable masses. We have found that, while it is legitimate to simply sum the primary's and secondary's inputs in $da/dt$ or $de/dt$, this is not the case for $di/dt$. So our expression for $di/dt$ differs from that of Kaula in two regards. First, the contribution due to the dissipation in the secondary averages out when the apsidal precession is uniform. Second, we have obtained an additional term which emerges owing to the conservation of the angular momentum: a change in the inclination of the orbit causes a change of the primary's plane of equator.

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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