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arXiv 2401.09577gr-qcastro-ph.HE
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参数化绝热旋进的黑洞轨道

Parameterizing black hole orbits for adiabatic inspiral

Scott A. Hughes

AI总结:

本文开发了从运动积分(E, L_z, Q)到轨道几何参数(p, e, x_I)的通用反向映射,解决了赤道及一般轨道的高效计算问题,消除了接近最后稳定轨道时的雅可比奇异性,从而更精确地计算绝热旋进。

摘要:

小质量比极限下的绝热双星旋进将小天体视为沿大Kerr黑洞的测地线运动,该测地线因辐射反作用而缓慢演化。除初始条件外,测地线通常有两种参数化方式:使用运动积分能量$E$、轴向角动量$L_z$和Carter常数$Q$;或使用轨道几何参数半通径$p$、偏心率$e$和倾角(的余弦)$x_I \equiv \cos I$。学界早已掌握如何将轨道积分计算为轨道几何参数的函数,即表示为$E(p, e, x_I)$的函数,$L_z$和$Q$同理。反向映射——即函数$p(E, L_z, Q)$,$e$和$x_I$同理——尚未得到普遍开发。在本文中,我们开发了从($E$, $L_z$, $Q$)到($p$, $e$, $x_I$)的通用映射。该映射对于赤道轨道($Q = 0$, $x_I = \pm1$)特别简单,并且对于一般情况可以高效计算。这些结果使得更精确地计算绝热旋进成为可能,因为消除了使用在旋进接近最后稳定轨道时变得奇异的雅可比行列式的需要。

英文摘要:

Adiabatic binary inspiral in the small mass ratio limit treats the small body as moving along a geodesic of a large Kerr black hole, with the geodesic slowly evolving due to radiative backreaction. Up to initial conditions, geodesics are typically parameterized in two ways: using the integrals of motion energy $E$, axial angular momentum $L_z$, and Carter constant $Q$; or, using orbit geometry parameters semi-latus rectum $p$, eccentricity $e$, and (cosine of ) inclination $x_I \equiv \cos I$. The community has long known how to compute orbit integrals as functions of the orbit geometry parameters, i.e., as functions expressing $E(p, e, x_I)$, and likewise for $L_z$ and $Q$. Mappings in the other direction -- functions $p(E, L_z, Q)$, and likewise for $e$ and $x_I$ -- have not yet been developed in general. In this note, we develop generic mappings from ($E$, $L_z$, $Q$) to ($p$, $e$, $x_I$). The mappings are particularly simple for equatorial orbits ($Q = 0$, $x_I = \pm1$), and can be evaluated efficiently for generic cases. These results make it possible to more accurately compute adiabatic inspirals by eliminating the need to use a Jacobian which becomes singular as inspiral approaches the last stable orbit.

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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