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CONTROL OF FORMATION-FLYING MULTI-ELEMENT SPACE INTERFEROMETERS WITH DIRECT INTERFEROMETER-OUTPUT FEEDBACK

机译:具有直接干涉仪输出反馈的形成飞行多元素空间干涉仪

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The long-baseline space interferometer concept involving formation flying of multiple spacecraft holds great promise as future space missions for high-resolution imagery. A major challenge of obtaining high-quality interferometric synthesized images from long-baseline space interferometers is to accurately control these spacecraft and their optics payloads in the specified configuration. Our research focuses on the determination of the optical errors to achieve fine control of long-baseline space interferometers without resorting to additional sensing equipment. We present a suite of estimation tools that can effectively extract from the raw interferometric image relative x/y, piston translational and tip/tilt deviations at the exit pupil aperture. The use of these error estimates in achieving control of the interferometer elements is demonstrated using simulated as well as laboratory-collected interferometric stellar images.
机译:涉及多个航天器的形成飞行的长基线空间干涉仪概念作为高分辨率图像的未来空间任务具有很大的承诺。 从长基线空间干涉仪获得高质量干涉综合图像的主要挑战是在指定的配置中准确控制这些航天器及其光学有效载荷。 我们的研究侧重于测定光学误差,以实现长基线空间干涉仪的微量控制,而无需借助额外的传感设备。 我们提出了一套估计工具,可以有效地从出口瞳孔孔的原始干涉图像相对X / Y,活塞平移和尖端/倾斜偏差中提取。 使用模拟和实验室收集的干涉式恒星图像来证明在实现干涉仪元件的控制方面使用这些误差估计。

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