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Perspectives in measuring the PPN parameters beta and gamma in the Earth's gravitational fields with the CHAMP/GRACE models

机译:关于测量ppN参数β和γ的观点   地球的引力场与CHamp / GRaCE模型

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摘要

The current bounds on the PPN parameters gamma and beta are of the order of10^-4-10^-5. Various missions aimed at improving such limits by several ordersof magnitude have more or less recently been proposed like LATOR, ASTROD,BepiColombo and GAIA. They involve the use of various spacecraft, to belaunched along interplanetary trajectories, for measuring the effects of thesolar gravity on the propagation of electromagnetic waves. In this paper weinvestigate what is needed to measure the combination nu=(2+2gamma-beta)/3 ofthe post-Newtonian gravitoelectric Einstein perigee precession of a testparticle to an accuracy of about 10^-5 with a pair of drag-free spacecraft inthe Earth's gravitational field. It turns out that the latest gravity modelsfrom the dedicated CHAMP and GRACE missions would allow to reduce thesystematic error of gravitational origin just to this demanding level ofaccuracy. In regard to the non-gravitational errors, the spectral noise densityof the drag-free sensors required to reach such level of accuracy would amountsto 10^-8-10^-9 cm s^-2 Hz^-1/2 over very low frequencies. Although not yetobtainable with the present technologies, such level of compensation is muchless demanding than those required for, e.g., LISA. As a by-product, anindependent measurement of the post-Newtonian gravitomagnetic Lense-Thirringeffect with a 0.9% accuracy would be possible as well. The forthcoming Earthgravity models from CHAMP and GRACE will further reduce the systematicgravitational errors in both of such tests.
机译:PPN参数gamma和beta的当前范围为10 ^ -4-10 ^ -5。最近提出了各种旨在将这种限制提高几个数量级的任务,例如LATOR,ASTROD,BepiColombo和GAIA。它们涉及沿行星际轨迹发射的各种航天器的使用,用于测量太阳重力对电磁波传播的影响。在本文中,我们研究了使用一对无阻力航天器将牛顿后重电爱因斯坦近地点进动测试粒子的nu =(2 + 2gamma-beta)/ 3的组合测量到大约10 ^ -5的精度时所需要的在地球的引力场中。事实证明,来自专用CHAMP和GRACE任务的最新重力模型将可以将引力起源的系统误差降低到这种要求的精度水平。关于非重力误差,要达到这样的精度水平,无阻力传感器的频谱噪声密度在非常低的条件下将达到10 ^ -8-10 ^ -9 cm s ^ -2 Hz ^ -1 / 2频率。尽管目前的技术尚无法获得,但是这种补偿水平比例如LISA所需的补偿水平要高得多。作为副产品,也可以以0.9%的准确度独立地测量牛顿后重力Lense-Thirring效应。来自CHAMP和GRACE的即将出现的Earthgravity模型将进一步减少这两种测试中的系统重力误差。

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    Iorio, Lorenzo;

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  • 年度 2007
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