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The SIM Astrometric Grid

机译:SIM星状网格

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摘要

The Space Interferometry Mission (SIM) is fundamentally a one-dimensional instrument with a 15-degree field-of-regard. Mission objectives require a global reference grid of thousands of well-understood stars with positions known to 4 mi-croarcseconds which will be used to establish the instrument baseline vector during scientific observations. This accuracy will be achieved by frequently observing a set of stars throughout the mission and performing a global fit of the observations to determine position, proper motion and parallax for each star. Each star will be observed approximately 200 times with about 6.5 stars per single instrument field on the sky. We describe the nature of the reference grid, the candidate objects, and the results of simulations demonstrating grid performance, including estimates of the grid robustness when including effects such as instrument drift and possible contamination of the grid star sample by undetected binaries.
机译:空间干涉测量任务(SIM)基本上是一维具有15度视场的一维仪器。任务目标需要一个由数千颗易于理解的恒星组成的全球参考网格,其位置已知为4毫秒,这将用于在科学观测期间建立仪器基线向量。通过在整个任务过程中经常观察一组恒星并进行观测的全局拟合以确定每个恒星的位置,适当的运动和视差,可以实现这种精度。每颗恒星将被观测约200次,而天空中的每个仪器场将观测到约6.5颗恒星。我们描述了参考网格的性质,候选对象以及演示网格性能的模拟结果,包括当包括诸如仪器漂移和未检测到的二进制文件可能对网格星样本造成污染等影响时对网格鲁棒性的估计。

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