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Experimental comparison of tracking algorithms in the presence of aircraft boundary-layer distortions for emulated free-space laser communication links

机译:仿真自由空间激光通信链路存在飞机边界层失真时跟踪算法的实验比较

摘要

We report experiments comparing different focal plane array (FPA) tracking algorithms for emulated laser communication links between an aircraft and spacecraft. The links include look-angle-dependent phase disturbances caused by boundary-layer turbulence replicated by using a deformable mirror. Impairments from platform jitter, atmospheric scintillation, and propagation delay are also included. We study a hyperhemispherical dome geometry that provides a large field of regard but generates boundary-layer turbulence. Results from experiments comparing peak and centroid FPA tracking algorithms in various environments show that power delivered to the optical fiber varies with algorithm and look angle. An improvement in steady-state fiber-coupled power of up to 1.0 dB can be achieved through appropriate choice of algorithm. In a real system, this advantage could be realized by implementing a tracking processor that dynamically changes its tracking algorithm depending on look angle and other parameters correlated to boundary-layer turbulence.
机译:我们报告的实验比较了飞机和航天器之间模拟激光通信链路的不同焦平面阵列(FPA)跟踪算法。链接包括由使用可变形反射镜复制的边界层湍流引起的与视场角相关的相位干扰。还包括平台抖动,大气闪烁和传播延迟造成的损害。我们研究了一个超半球形的圆顶几何形状,该几何形状提供了广阔的视野,但会产生边界层湍流。在各种环境下比较峰和质心FPA跟踪算法的实验结果表明,传递到光纤的功率随算法和视角而变化。通过适当选择算法,可以将稳态光纤耦合功率提高高达1.0 dB。在实际系统中,可以通过实现跟踪处理器来实现此优势,该跟踪处理器根据视角和与边界层湍流相关的其他参数动态更改其跟踪算法。

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