首页> 外文会议>Instrumentation and Measurement Technology Conference, 1994. IMTC/94. Conference Proceedings. 10th Anniversary. Advanced Technologies in I amp; M., 1994 IEEE >Bias of a resonator fiber optic gyro composed of apolarization-maintaining fiber ring resonator with the photoinducedbirefringent grating
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Bias of a resonator fiber optic gyro composed of apolarization-maintaining fiber ring resonator with the photoinducedbirefringent grating

机译:谐振器光纤陀螺仪的偏置由光诱导的保偏光纤环形谐振器双折射光栅

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A theoretical study of the polarization-fluctuation induced biasof an resonator fiber optic gyro (R-FOG), which employs apolarization-maintaining fiber ring resonator with a photoinducedbirefringent grating, is presented. The polarization conversion due tothe photoinduced birefringent grating can stabilize the resonatoroutput, which result in the reduction of the bias in the R-FOG output.The influences of the parameters, such as the fluctuation of the inputpolarization, the resonator finesse, and the photoinduced index changeof the dielectric tensor, on the bias of the gyro-output have beeninvestigated. Our results show that with the help of a photoinducedbirefringent grating the bias of the gyro-output can be limited in theorder of 10-7 rad/s, a typical specification for theaircraft-navigation
机译:偏振波动偏差的理论研究 阳光光纤陀螺仪(R-FOG),雇用了 用光诱导保持偏振纤维环谐振器 提出了双折射光栅。极化转换导致 光抑制的双折射光栅可以稳定谐振器 输出,导致R-FOG输出中的偏差减少。 参数的影响,例如输入的波动 极化,谐振器精细性和光诱导指数变化 在介电张量的情况下,在陀螺仪的偏差上已经存在 调查。我们的结果表明,借助光线诱导 双折射光栅陀螺仪的偏差可以限制在 10 -7 rad / s,典型规格 飞机导航

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