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Fizeau interferometry testbed: wavefront control

机译:FIZEAU干涉测量试验台:波前控制

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Stellar Imager (SI) is a potential NASA space-based UV imaging interferometer to resolve the stellar disks of nearby stars. SI would consist of 20 - 30 separate spacecraft flying in formation at the Earth-Sun L2 libration point. Onboard wavefront control would be required to initially align the formation and maintain alignment during science observations and after array reconfiguration. The Fizeau Interferometry Testbed (FIT) is a testbed currently under development at the NASA/Goddard Space Flight Center to develop and study the wavefront control methodologies for Stellar Imager and other large, sparse aperture telescope systems. FIT consists of 7 articulated spherical mirrors in a Golay pattern, expandable up to 30 elements, and reconfigurable into multiple array patterns. FIT's purpose is to demonstrate image quality versus array configuration and to develop and advance the wavefront control for SI. FIT uses extended scene wavelength, focus and field diversity to estimate the wavefront across the set of apertures. The recovered wavefront is decomposed into the eigenmodes of the control matrix and actuators are moved to minimize the wavefront piston, tip and tilt. Each mirror's actuators are 3 degrees of freedom, however, they do not move each of the mirrors about a point on each mirrors surface, thus the mapping from wavefront piston, tip/tilt to mirror piston, tip/tilt is not diagonal. We initially estimate this mapping but update it as part of wavefront sensing and control process using system identification techniques. We discuss the FIT testbed, wavefront control methodology, and show initial results from FIT.
机译:Stellar Imager(SI)是一种基于NASA空间的UV成像干涉仪,用于解决附近恒星的恒星磁盘。 SI将包括在地球 - 太阳L2拉动点形成的20 - 30个独立的航天器飞行。在载上的波前控制将需要最初对齐形成并在科学观察期间和阵列重新配置后保持对齐。 Fizeau干涉测量测试用(FIT)是目前在美国宇航局/戈达德太空飞行中心开发的试验台,开发和研究了恒星成像仪和其他大型稀疏孔径望远镜系统的波前控制方法。 FIT由7个铰接式球形镜子组成的高底图案,可扩展至30个元件,并可重新配置为多个阵列图案。 FIT的目的是展示图像质量与阵列配置,并开发和推进SI的波前控制。 FIT使用扩展的场景波长,焦点和现场多样性来估计该组孔径的波前。回收的波前被分解到控制矩阵的特征模具中,移动器移动以使波前活塞,尖端和倾斜最小化。每个镜子的致动器是3度自由度,然而,它们不会将每个镜子上的每个镜子移动到每个镜子表面上的点,从而从波前活塞的映射,尖端/倾斜到镜子活塞,尖端/倾斜不是对角线。我们最初估计该映射,但是使用系统识别技术将其更新为Wavefront感应和控制过程的一部分。我们讨论拟合试验台,波前控制方法,并显示初始结果。

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