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Bit error rate performance on passive alignment in free space optical links using large core fibers

机译:使用大型纤芯光纤的自由空间光链路中无源对准时的误码率性能

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A 20-meter free-space optical link (FSOL) is proposed for data transmission between external ISS payload sites and the main cabin at a target rate of 10 Gbps (gigabits per second). Motion between a payload site and the main cabin is predicted to cause up to 5 cm in lateral misalignment and 0.2 degrees of angular misalignment. Due to the harsh environment of space it is advantageous to locate the optical transceivers inside the spacecraft or in a controlled environment. With the optical components and transceivers in separate locations, a fiber optic cable will be required to carry light between the two. In our past work we found that the use of large-core fibers provide an increased misalignment tolerance for such systems and could eliminate the need for active control of the optics. In that work, it was shown that a 105 μm core diameter fiber optic cable offered a viable low SWaP (size, weight, and power) solution for the ISS application; however, the effects of modal dispersion were not investigated. This paper will present bit error rate performance of the FSOL using these large-core fibers.
机译:提出了20米的自由空间光链路(FSOL),用于以10 Gbps(千兆位/秒)的目标速率在外部ISS有效载荷站点和主机舱之间进行数据传输。预计有效载荷站点与主客舱之间的运动将导致最多5 cm的侧向未对准和0.2度的角度未对准。由于恶劣的空间环境,将光收发器放置在航天器内部或受控环境中是有利的。由于光学组件和收发器位于不同的位置,因此需要一根光缆在两者之间传输光。在我们过去的工作中,我们发现使用大芯光纤可以为此类系统提供更高的失准公差,并且可以消除对光学器件进行主动控制的需求。在这项工作中,表明芯径为105μm的光缆为ISS应用提供了可行的低SWaP(尺寸,重量和功率)解决方案。但是,没有研究模态色散的影响。本文将介绍使用这些大芯光纤的FSOL的误码率性能。

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