大气湍流和损耗条件下激光地星上行通信系统的误码率性能

L. Stotts, L. Andrews
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引用次数: 1

摘要

分析了地空激光上行通信系统在大气湍流和大气损耗作用下的误码率性能。波束漂移引起的效应,如闪烁和接收机噪声方差,对通信系统性能的影响比以前所评估的要大。提出了一种考虑大气损耗、强度波动、波束漂移和强度噪声方差的新信噪比模型。这种模式可以很容易地修改到其他通信系统,例如,差分相移键。因此,闪烁指数和误码率很容易用前向错误编码(FEC)来评估,以补偿大气湍流的影响。具体来说,在两种具体基准下,比较了10gb / s、不归零开关键、掺铒光纤放大器通信系统的10 - 12误码率性能与Hufnagle-Valley 5/7和hufnagle - andrew - phillips折射率结构参数模型的链路天顶角的关系。这些模型是用一个圆地球模型来评估的。这些模型基本上与Hufnagel-Valley 5/7模型的乘法版本相称,这似乎是更现实的模型比较方式。结果表明,在最后一种情况下,高天顶角的误码率性能有渐近极限。结论是,在高天顶角条件下,需要采用除FEC外的其他方法来实现10-12的误码率。文中给出了一个实例,说明了在减小湍流时增大FEC的一种方法
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Bit Error Rate Performance of a Laser Ground-to-Satellite Uplink Communications Systems in the Presence of Atmospheric Turbulence and Loss
The Bit Error Rate (BER) performance of a ground-to-space laser uplink communications systems subject to atmospheric turbulence and loss is analyzed. Beam wander-induced effects like scintillation and receiver noise variance have a greater effects on communications system performance than has previously been assessed. A new model for the signal-to-noise ratio is presented that includes atmospheric loss, intensity fluctuations, beam wander, and intensity noise variance. This model easily can be modified to other communications systems, e.g., Differential Phase Shift Key. The scintillation index and the BER hence readily evaluated with Forward Error Coding (FEC) to compensate for atmospheric turbulence effects. Specifically, comparisons in 10–12 BER performance for 10 Gigabit per second, Non-Return to Zero On-Off Key, Erbium-Doped-Fiber Amplifier communications systems as a function of link zenith angle are given for the Hufnagle-Valley 5/7 and Hufnagle-Andrews-Phillips refractive index structure parameter models under two specifics benchmarks. These models were evaluated using a round-earth model. These models essentially are commensurate with the multiplicative version of the Hufnagel-Valley 5/7 model, which appears to the more realistic way of model comparison. Results show that in this last situation, BER performance has an asymptotic limit for high zenith angles. The conclusion is that other means in addition to a FEC are needed to achieve a 10–12 BER for high zenith angle. Example is given that shows an approach for augmenting a FEC in mitigating turbulence
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