哈勃空间望远镜精细制导传感器的光学校准

L. Abramowicz-Reed, H. L. Hallock, W. Jefferys, G. Welter
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引用次数: 1

摘要

哈勃太空望远镜(HST)任务的重要目标是在科学仪器孔径内放置目标,精度为10毫弧秒,并进行天体测量,精度为均方根2.7毫弧秒。为了实现这些目标,必须对三种精细制导传感器(FGS)的放大倍数和光学畸变的地轨变化进行表征。本文中没有介绍的另一个步骤是,通过FGS-to-FGS校准,将三个fgs对准一个共同的参考框架。本文确定了畸变的来源,描述了校准原理和发射前可行性研究,最后讨论了与10毫角秒指向要求相关的在轨性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Optical Calibration of the Hubble Space Telescope Fine Guidance Sensors
Important objectives of the Hubble Space Telescope (HST) mission are to place targets within a science instrument aperture to an accuracy of 10 milliarcseconds and to perform astrometric measurements to an accuracy of 2.7 milliarcseconds, rms. In order to achieve these goals, ground-to-orbit changes in magnification and optical distortion must be characterized for each erf the three Fine Guidance Sensors (FGS). An additional step, not presented in this paper, aligns the three FGSs to a common reference frame via the FGS-to-FGS alignment calibration. This paper identifies the sources of distortion, describes the calibration philosophy and pre-launch feasibility studies and finally, discusses on-orbit performance pertaining to the 10 milliarcsecond pointing requirement.
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