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Stellar Imager: Wavefront Control

机译:恒星成像仪:波前控制

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Stellar Imager (SI) is a proposed 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 sensing and control is required to maintain alignment during science observations and after array reconfigurations. The Fizeau Interferometry Testbed (FIT), developed at the NASA/Goddard Space Flight Center, is being used to study wavefront sensing and control methodologies for Stellar Imager and other large, sparse aperture telescope systems. FIT initially consists of 7 articulated spherical mirrors in a Golay pattern, and is currently undergoing expansion to 18 elements. FIT currently uses in-focus whitelight sparse aperture PSFs and a direct solve broadband phase retrieval algorithm to sense and control its wavefront. Ultimately it will use extended scene wavelength, with a sequential diversity algorithm that modulates a subset of aperture pistons to jointly estimate the wavefront and the reconstructed image from extended scenes. The recovered wavefront is decomposed into the eigenmodes of the control matrix and actuators are moved to minimize the wavefront piston, tip and tilt in closed-loop. We discuss the testbed, wavefront control methodology and ongoing work to increase its bandwidth from 1 per 11 seconds to a few 10's of Hertz and show ongoing results.
机译:恒星成像仪(SI)是一种拟议的NASA天基紫外成像干涉仪,用于解析附近恒星的恒星盘。 SI将由20到30个在地球太阳L2解放点编队飞行的独立航天器组成。在科学观测期间和阵列重新配置后,需要板载波前传感和控制来保持对准。由NASA /戈达德太空飞行中心开发的Fizeau干涉测量试验台(FIT)被用于研究Stellar Imager和其他大型稀疏孔径望远镜系统的波前传感和控制方法。 FIT最初由7个呈Golay图案的铰接球面反射镜组成,目前正扩展到18个元件。 FIT当前使用焦点对准的白光稀疏孔径PSF和直接求解宽带相位检索算法来感测和控制其波前。最终,它将使用扩展的场景波长,并通过顺序分集算法对孔径活塞的子集进行调制,以共同估计波前和扩展场景中的重建图像。恢复的波前分解为控制矩阵的本征模式,并移动致动器以使闭环中的波前活塞,尖端和倾斜最小化。我们讨论了测试平台,波前控制方法和正在进行的工作,以将其带宽从每11秒1个增加到几十赫兹,并显示正在进行的结果。

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