大质量旋转天体场中双曲线运动的后开普勒扰动

Lorenzo Iorio
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摘要

在牛顿后第一层次上,分析计算了大质量旋转体引力场的广义相对论引力-电磁-施瓦兹柴尔德分量和伦斯-特林分量对测试粒子双曲线运动的扰动。在牛顿阶,还计算了源的四极质量力矩的影响。由此得出的分析表达式对探测器轨道平面和主旋轴在空间的一般方向以及任意偏心率值都有效。我们首先将它们应用于'Oumuamua',这是一颗星际小行星,最近沿着一条非束缚日心轨道造访了我们的太阳系。虽然它在飞越太阳时发生的重力位移小于几十毫微秒,但在整个轨道上因太阳扁平和角动量而发生的位移却达到了微微秒数量级。近地小行星会合(NEAR)航天器在飞越地球期间的牛顿后偏移也有类似的数值,而后者的扁平造成的偏移名义上要大几个数量级。目前地球位势四极质量矩的不确定性(形式上的)将使这种经典效应的错误模型低于预测相对论扰动的标称值。双曲过量速度不会因所考虑的任何开普勒后加速度而改变。所开发的计算方法也可以直接扩展到任何其他重力模型。
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Post-Keplerian perturbations of the hyperbolic motion in the field of a massive, rotating object
The perturbations of the hyperbolic motion of a test particle due to the general relativistic gravitoelectromagnetic Schwarzschild and Lense-Thirring components of the gravitational field of a massive, rotating body are analytically worked out to the first post-Newtonian level. To the Newtonian order, the impact of the quadrupole mass moment of the source is calculated as well. The resulting analytical expressions are valid for a generic orientation in space of both the orbital plane of the probe and the spin axis of the primary, and for arbitrary values of the eccentricity. They are applied first to 'Oumuamua, an interstellar asteroid which recently visited our solar system along an unbound heliocentric orbit. While its gravitoelectric shifts occurred close to the Sun's flyby are less than some tens of milliarcseconds, those due to the solar oblateness and angular momentum are of the order of microarcseconds throughout the whole trajectory. Comparable values occur for the post-Newtonian shifts of the Near Earth Asteroid Rendezvous (NEAR) spacecraft during its flyby of the Earth, while those due to the oblateness of the latter are nominally several orders of magnitude larger. The current (formal) uncertainty in the quadrupole mass moment of the geopotential would bring the mismodeling of such classical effects below the nominal value of the predicted relativistic disturbances. The hyperbolic excess velocity is not changed by any of the post--Keplerian accelerations considered. The calculational approach developed can be straightforwardly extended to any alternative models of gravity as well.
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