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Noise and Bias Error Due to Polarization Coupling in a Fiber Optic Gyroscope

机译:光纤陀螺仪中偏振耦合引起的噪声和偏置误差

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摘要

This paper reports a comprehensive model of the noise and drift induced by polarization coupling in a fiber optic gyroscope (FOG) interrogated with a laser of arbitrary linewidth. It includes the effects of dynamic phase biasing, a realistic description of the laser phase noise and polarization-dependent loss. This model yields concise analytical expressions for the noise and drift dependencies on the laser linewidth, the fiber length and holding parameter , and the fractional power launched into the unwanted polarization at the input to the sensing coil. For all realistic FOG parameter sets, the polarization-coupling noise is found to be insignificant. For a 1-km coil, a typical holding parameter () and push–pull modulation, the drift is only ∼1 μ rad up to a linewidth of ∼100 MHz, which is far lower than previously believed. The drift decreases to even lower values for larger linewidths. Experimental measurements of the noise and drift in a 150-m FOG and their dependence on laser linewidth support these predictions. Birefringence modulation can be brought to bear to reduce this residual drift enough to meet the requirement for aircraft inertial navigation. Ultimately, this analysis shows that low-polarization coupling error can be obtained without the use of a broadband source.
机译:本文报告了一个由光纤陀螺仪(FOG)偏振耦合引起的噪声和漂移的综合模型,该陀螺仪受到任意线宽激光器的询问。它包括动态相位偏置的影响,对激光相位噪声和偏振相关损耗的现实描述。该模型针对噪声和漂移与激光线宽,光纤长度和保持参数以及在感应线圈输入端发射到不想要的偏振中的分数功率产生了简洁的解析表达式。对于所有现实的FOG参数集,偏振耦合噪声均不明显。对于1 km的线圈,典型的保持参数()和推挽调制,直到线宽为〜100 MHz时,漂移仅为〜1μrad,远低于以前的估计。对于较大的线宽,漂移减小到更低的值。 150 m FOG中噪声和漂移的实验测量及其对激光线宽的依赖性支持了这些预测。可以承担双折射调制,以减少此残余漂移,足以满足飞机惯性导航的要求。最终,该分析表明,无需使用宽带源就可以获得低极化耦合误差。

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