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首页> 外文期刊>Advances in space research >Dynamical orbital effects of general relativity on the satellite-to-satellite range and range-rate in the GRACE mission:A sensitivity analysis
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Dynamical orbital effects of general relativity on the satellite-to-satellite range and range-rate in the GRACE mission:A sensitivity analysis

机译:广义相对论对GRACE任务中卫星到卫星的射程和射程速率的动态轨道影响:敏感性分析

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We numerically investigate the impact of the General Theory of Relativity (GTR) on the orbital part of the satellite-to-satellite range p and range-rate p of the twin GRACE A/B spacecrafts through their post-Newtonian (PN) dynamical equations of motion integrated in an Earth-centered frame over a time span AP = 1 d. The present-day accuracies in measuring the GRACE biased range and range-rate are s_p~ 1- 10 rn, s_p~ 0.1 - 1 m s~(-1). The GTR range and range-rate effects turn out to be Ap = 80 m and Ap = 0.012 m s~(-1) (1PN gravitomagnetic), and Ap = 6000 m and Ap = 10 m s~(-1) (1PN gravitoelectric). It turns out that the range shifts Ap corresponding to the GTR-induced time delays At on the propagation of the electromagnetic waves linking the GRACE spacecrafts are either negligible (1PN gravitomagnetic) or smaller (1PN gravitoelectric) than the orbital effects by about 1 order of magnitude over AP = 1 d. We also compute the dynamical range and range-rate perturbations caused by the first six zonal harmonic coefficients J_lt, = 2,3,4, 5,6, 7 of the classical multipolar expansion of the geopotential to evaluate their aliasing impact on the relativistic effects. Conversely, we quantitatively, and preliminarily, assess the possible a-priori "imprinting" of GTR itself, not solved-for in all the GRACE-based Earth's gravity models produced so far, on the low degree zonals of the geopotential. The present sensitivity analysis can also be extended, in principle, to different orbital configurations in order to design a suitable dedicated mission able to accurately measure GTR. Moreover, it may be the starting point for more refined numerical investigations concerning the actual measurability of the relativistic effects involving, e.g., a simulation of full GRACE data, including GTR itself, and the consequent parameters' estimation. Finally, also other non-classical dynamical features of motion, caused by, e.g., modified models of gravity, may be considered in further studies.
机译:我们通过其后牛顿(PN)动力学方程,通过数值研究广义相对论(GTR)对双GRACE A / B航天器的卫星到卫星范围p和范围速率p的轨道部分的影响在AP = 1 d的时间跨度内集成在以地球为中心的帧中的运动量。目前测量GRACE偏置范围和范围速率的精度为s_p〜1-10 rn,s_p〜0.1-1 m s〜(-1)。 GTR范围和范围速率效应分别为Ap = 80 m和Ap = 0.012 ms〜(-1)(1PN重力),Ap = 6000 m和Ap = 10 ms〜(-1)(1PN重力) 。事实证明,对应于GTR引起的时间延迟At的距离偏移Ap在与GRACE航天器相连的电磁波传播时,可以忽略不计(1PN重力电磁)或比轨道效应小(1PN重力电磁)约1个数量级。 AP上的强度= 1 d。我们还计算了由经典的多极地势扩展的前六个纬向谐波系数J_lt = 2,3,4,5,6,7引起的动态范围和范围速率摄动,以评估其混叠效应对相对论效应的影响。相反,我们定量地,初步地评估了GTR本身可能存在的先验性“印记”,但到目前为止,并没有解决所有基于GRACE的地球重力模型在地势低纬度带上解决的问题。原则上,本敏感性分析还可以扩展到不同的轨道配置,以便设计能够精确测量GTR的合适的专用任务。此外,它可能是对相对论效应的实际可测量性进行更精细的数值研究的起点,例如,对包括GRTR本身在内的完整GRACE数据进行仿真,以及随后对参数进行估计。最后,还可以在进一步研究中考虑由例如修改的重力模型引起的运动的其他非经典动力学特征。

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