首页> 外文会议>New Frontiers in Stellar Interferometry pt.2 >The Fizeau Interferometer Testbed (FIT): Developing and Testing the Technologies Needed for Space-Based Interferometric Imaging Systems
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The Fizeau Interferometer Testbed (FIT): Developing and Testing the Technologies Needed for Space-Based Interferometric Imaging Systems

机译:Fizeau干涉仪测试平台(FIT):开发和测试天基干涉成像系统所需的技术

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The Fizeau Interferometer Testbed (FIT) is a ground-based laboratory experiment at Goddard Space Flight Center (GSFC) designed to develop and test technologies that will be needed for future interferometric spacecraft missions. Specifically, the research from this experiment is a proof-of-concept for optical accuracy and stability, closed-loop control algorithms, optimal sampling methodology of the Fourier UV-plane, computational models for system performance, and image synthesis techniques for a sparse array of 7 to 30 mirrors. It will assess and refine the technical requirements on hardware, control, and imaging algorithms for the Stellar Imager (SI), its pathfinder mission, and other sparse aperture and interferometric imaging mission concepts. This ground-based optical system is a collaborative effort between NASA's GSFC, Sigma Space Corporation, the Naval Research Laboratory, and the University of Maryland. We present an overview of the FIT design goals and explain their associated validation methods. We further document the design requirements and provide a status on their completion. Next, we show the overall FIT design, including the optics and data acquisition process. We discuss the technologies needed to insure success of the testbed as well as for an entire class of future mission concepts. Finally, we compare the expected performance to the actual performance of the testbed using the initial array of seven spherical mirrors. Currently, we have aligned and phased all seven mirrors, demonstrated excellent system stability for extended periods of time, and begun open-loop operations using "pinhole" light sources. Extended scenes and calibration masks are being fabricated and will shortly be installed in the source module. Installation of all the different phase retrieval/diversity algorithms and control software is well on the way to completion, in preparation for future tests of closed-loop operations.
机译:Fizeau干涉仪试验台(FIT)是戈达德太空飞行中心(GSFC)的地面实验室实验,旨在开发和测试未来干涉式航天器飞行所需的技术。具体而言,该实验的研究是光学精度和稳定性的概念证明,闭环控制算法,傅立叶紫外平面的最佳采样方法,系统性能的计算模型以及稀疏阵列的图像合成技术7至30面镜子。它将评估和完善对Stellar Imager(SI),其探路者任务以及其他稀疏孔径和干涉成像任务概念的硬件,控制和成像算法的技术要求。这种基于地面的光学系统是NASA GSFC,Sigma Space Corporation,海军研究实验室和马里兰大学之间的共同努力。我们提供FIT设计目标的概述,并解释其相关的验证方法。我们进一步记录设计要求并提供完成状态。接下来,我们展示整个FIT设计,包括光学和数据采集过程。我们将讨论确保测试平台以及整个未来任务概念成功所需的技术。最后,我们使用七个球面镜的初始阵列将预期性能与测试台的实际性能进行比较。目前,我们已经对所有七个反射镜进行了对准和定相,在长时间内展示了出色的系统稳定性,并开始使用“针孔”光源进行开环操作。扩展的场景和校准遮罩正在制造中,并将很快安装在源模块中。所有不同的相位检索/分集算法和控制软件的安装都快要完成了,为将来的闭环操作测试做准备。

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