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arXiv 2204.05047gr-qc
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第四后闵可夫斯基阶引力两体系统的能量学与散射

Energetics and scattering of gravitational two-body systems at fourth post-Minkowskian order

Mohammed Khalil, Alessandra Buonanno, Jan Steinhoff, Justin Vines

AI总结:

本文通过与数值相对论比较圆轨道结合能和散射角,评估并将4PM保守动力学纳入EOB框架,显著提升了等质量双星近并合阶段的预测精度。

摘要:

LIGO-Virgo-KAGRA合作组织即将开展的观测运行,以及未来地面和空间引力波(GW)探测器,都需要比现有模型更精确的波形模型。通过改进对致密双星动力学的解析描述,并用数值相对论(NR)信息加以完善,可以发展高精度波形模型。在此,我们通过与圆轨道结合能及散射角的NR模拟进行比较,评估了近期第四后闵可夫斯基(4PM)保守动力学结果的准确性。我们发现,4PM动力学比3PM动力学与NR符合得更好;尽管对于束缚轨道,4PM近似给出与第三后牛顿(PN)近似相当的结果,但在散射相遇中其表现更佳。此外,我们将4PM结果纳入有效一体(EOB)哈密顿量中;对于等质量双星,在并合前两个GW周期时,这使相对于4PM展开哈密顿量与NR的不符程度从约40%改善至约10%,或依据EOB规范不同而改善至约3%。最后,我们推导了适用于双曲线轨道的4PN-EOB哈密顿量,并将其对散射角的预测与NR以及为椭圆轨道计算的4PN-EOB哈密顿量的散射角进行了比较。

英文摘要:

Upcoming observational runs of the LIGO-Virgo-KAGRA collaboration, and future gravitational-wave (GW) detectors on the ground and in space, require waveform models more accurate than currently available. High-precision waveform models can be developed by improving the analytical description of compact binary dynamics and completing it with numerical-relativity (NR) information. Here, we assess the accuracy of the recent results for the fourth post-Minkowskian (PM) conservative dynamics through comparisons with NR simulations for the circular-orbit binding energy and for the scattering angle. We obtain that the 4PM dynamics gives better agreement with NR than the 3PM dynamics, and that while the 4PM approximation gives comparable results to the third post-Newtonian (PN) approximation for bound orbits, it performs better for scattering encounters. Furthermore, we incorporate the 4PM results in effective-one-body (EOB) Hamiltonians, which improves the disagreement with NR over the 4PM-expanded Hamiltonian from $\sim 40\%$ to $\sim 10\%$, or $\sim 3\%$ depending on the EOB gauge, for an equal-mass binary, two GW cycles before merger. Finally, we derive a 4PN-EOB Hamiltonian for hyperbolic orbits, and compare its predictions for the scattering angle to NR, and to the scattering angle of a 4PN-EOB Hamiltonian computed for elliptic orbits.

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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