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LATOR: Its science product and orbital considerations

机译:主持人:其科学成果和轨道方面的考虑

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摘要

In a LATOR mission to measure the non-Euclidean relationship between three sides and one angle of a light triangle near the Sun, the primary science parameter, to be measured to part-in-10(9) precision, is shown to include not only the key parametrized post-Newtonian (PPN) gamma, but also the Sun's additional mass parameter, MG, which appears in the spatial metric field potential. MG may deviate from the Sun's well-measured gravitational mass due to post-Newtonian features of gravitational theory not previously measured in relativistic gravity observations. Under plausible assumptions, M-Gamma is a linear combination of the Sun's gravitational and inertial masses. If LATOR's two spacecraft lines of sight are kept close to equal and opposite relative to the Sun during the mission's key measurements of the light triangle, it is found that the navigational requirements for the spacecraft positions are greatly relaxed, eliminating the need for on-board drag-free systems. Spacecraft orbits from the Earth to achieve the equal and opposite passages by the Sun's, line of sight are illustrated.
机译:在一次LATOR任务中,它测量三边和太阳附近的一个轻三角形的一个角度之间的非欧几里得关系,主要科学参数被测量为十分之一(9)的精度,它不仅包括关键参数化后牛顿(PPN)伽玛参数,还有太阳的附加质量参数MG,它出现在空间度量场势中。由于相对论引力观测中以前没有测量到的牛顿后引力理论特征,MG可能会偏离太阳测得的引力质量。在合理的假设下,M-Gamma是太阳的重力质量和惯性质量的线性组合。如果在执行任务关键的光三角形测量期间,LATOR的两个航天器视线相对于太阳保持相等且相对,则发现该航天器位置的导航要求得到了极大的放松,从而无需在机上进行飞行无阻力系统。图解说明了从地球到地球的航天器轨道,以实现太阳视线的相等和相反的通过。

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