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LSST Telescope Guider Loop Requirements Analysis, and predictedPerformance

机译:LSST望远镜导向器回路需求分析和预测 r n性能

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The LSST Telescope has critical requirements on tracking error to meet image quality specifications, and will require closing a guiding loop, with the telescope servo control, to meet its mission. The guider subsystem consists of eight guiding sensors located inside the science focal plane at the edge of the 3.5deg field of view. All eight sensors will be read simultaneously at a high rate, and a centroid average will be fed to the telescope and rotator servo controls, for tracking error correction. A detailed model was developed to estimate the sensors centroid noise and the resulting telescope tracking error for a given frame rate and telescope servo control system.rnThe centroid noise depends on the photo-electron flux, seeing conditions, and guide sensor specifications. The model for the photo-electron flux takes into consideration the guide star availability at different galactic latitudes, the atmospheric extinction, the optical losses at different filter bands, the detector quantum efficiency, the integration time and the number of stars sampled. A 7-layer atmospheric model was also developed to estimate the atmospheric decorrelation between the different guide sensors due to the 3.5deg field of view, to predict both correlated and decorrelated atmospheric tip/tilt components, and to determine the trade-offs of the guider servo loop.
机译:LSST望远镜对跟踪误差有严格的要求,以满足图像质量规格,并且需要通过望远镜伺服控制闭合导向环才能完成其任务。导向器子系统由位于科学焦平面内3.5deg视场边缘的八个导向传感器组成。高速读取所有八个传感器,并且质心平均值将被馈送到望远镜和旋转伺服控制装置,以进行跟踪误差校正。针对给定的帧频和望远镜伺服控制系统,开发了一个详细的模型来估计传感器的质心噪声以及由此产生的望远镜跟踪误差。质心噪声取决于光电子通量,视线条件和引导传感器的规格。光电子通量模型考虑了不同银河纬度下的引导星可用性,大气消光,不同滤光带上的光损耗,探测器量子效率,积分时间和采样星数。还开发了一个7层大气模型来估计由于3.5度视场而导致的不同导向传感器之间的大气去相关,预测相关和去相关的大气尖端/倾斜组件以及确定导向器的权衡伺服回路。

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