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首页> 外文期刊>International journal of modern physics, D. Gravitation, astrophysics, cosmology >CONSTRAINING THE PREFERRED-FRAME α_1, α_2 PARAMETERS FROM SOLAR SYSTEM PLANETARY PRECESSIONS
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CONSTRAINING THE PREFERRED-FRAME α_1, α_2 PARAMETERS FROM SOLAR SYSTEM PLANETARY PRECESSIONS

机译:从太阳系行星偏向中构造优选框架α_1,α_2参数

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Analytical expressions for the orbital precessions affecting the relative motion of the components of a local binary system induced by Lorentz-violating Preferred Frame Effects (PFE) are explicitly computed in terms of the Parametrized Post- Newtonian (PPN) parameters α_1, α_2. Preliminary constraints on α_1, α_2 are inferred from the latest determinations of the observationally admitted ranges ?ω for any anomalous Solar System planetary perihelion precessions. Other bounds existing in the literature are critically reviewed, with particular emphasis on the constraint |α_2| ≤ 10~(-7) based on an interpretation of the current close alignment of the Sun's equator with the invariable plane of the Solar System in terms of the action of a α_2-induced torque throughout the entire Solar System's existence. Taken individually, the supplementary precessions ?ω of Earth and Mercury, recently determined with the INPOPlOa ephemerides without modeling PFE, yield α_1 = (0.8 ± 4) X 10~(-6) and α_2 = (4 ± 6) X 10~(-6), respectively. A linear combination of the supplementary perihelion precessions of all the inner planets of the Solar System, able to remove the a priori bias of unmodeled/mismodeled standard effects such as the general relativistic Lense-Thirring precessions and the classical rates due to the Sun's oblateness J_2, allows to infer α_1 = (-1 ± 6) X 10~(-6), α_2 = (-0.9 ± 3.5) x 10~(-5). Such figures are obtained by assuming that the ranges of values for the anomalous perihelion precessions are entirely due to the unmodeled effects of α_1 and α_2. Our bounds should be improved in the near-mid future with the MESSENGER and, especially, BepiColombo spacecrafts. Nonetheless, it is worthwhile noticing that our constraints are close to those predicted for BepiColombo in two independent studies. In further dedicated planetary analyses, PFE may be explicitly modeled to estimate α_1, α_2 simultaneously with the other PPN parameters as well.
机译:根据参数化后牛顿(PPN)参数α_1,α_2明确计算了影响洛伦兹违规优先帧效应(PFE)引起的影响本地二元系统组件相对运动的轨道运动的解析表达式。根据对任何异常太阳系行星近日点进动的观测允许范围ωω的最新确定,可以得出对α_1,α_2的初步约束。严格审查文献中存在的其他界限,特别强调约束条件|α_2|。 ≤10〜(-7),是根据整个太阳系存在期间由α_2引起的转矩作用对太阳赤道与太阳系不变平面的当前紧密对准的一种解释。单独计算,最近用INPOP10a星历表确定的地球和水银的补充旋进量ωω,未对PFE进行建模,得出α_1=(0.8±4)X 10〜(-6)和α_2=(4±6)X 10〜( -6)。太阳系所有内行星的辅助近日点进动的线性组合,能够消除未建模/建模错误的标准效果的先验偏差,例如一般相对论的Lense-Thirring进动和由于太阳扁率J_2而产生的经典速率,可以推断出α_1=(-1±6)X 10〜(-6),α_2=(-0.9±3.5)x 10〜(-5)。通过假设异常近日点进动的值范围完全是由于α_1和α_2的非模型效应而获得的。在不久的将来,我们应该借助MESSENGER(尤其是BepiColombo航天器)改善我们的飞行范围。尽管如此,值得注意的是,我们的限制条件接近于两项独立研究中对BepiColombo预测的条件。在进一步的专用行星分析中,PFE可以显式建模以与其他PPN参数同时估算α_1,α_2。

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