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Being the optical type resonator gyroscope, and the methodological null optical type gyroscope in order to decrease

机译:作为光学谐振器陀螺仪,以及方法上的空光学陀螺仪

摘要

PROBLEM TO BE SOLVED: To provide method for determining rotational speed of an optical gyroscope (10), while reducing the resonance asymmetric errors.;SOLUTION: The gyroscope (10) includes a ring resonator (25) equipped with a hollow core optical fiber coil (24), and optical elements selected and/or oriented so as to reduce stray light which can exist within incident ray that is being introduced into the ring resonator (25). The resonator has prescribed modes. A part of the optical elements partially transmits a part of the incident ray to a 1st end (41) of the optical fiber coil (24), while partially transmitting a part of the incident ray to a filter (20). A light having specific mode is received inside the 1st end (41) of the optical fiber coil (24), and the filter (20) receives the light of incident ray which has the corresponding mode. Transmission component of circulating light indicates resonance peak of counter-propagation direction of the ring resonator (25).;COPYRIGHT: (C)2008,JPO&INPIT
机译:要解决的问题:提供一种确定光学陀螺仪(10)转速的方法,同时减少共振不对称误差。;解决方案:陀螺仪(10)包括一个配备有空心光纤线圈的环形谐振器(25) (24),以及光学元件的选择和/或定向,以减少可能存在于引入环形谐振器(25)的入射光线中的杂散光。谐振器具有规定的模式。一部分光学元件将一部分入射光线部分地透射到光纤线圈(24)的第一端(41),同时将一部分入射光线部分地透射到滤光器(20)。在光纤线圈(24)的第一端(41)的内部接收具有特定模式的光,并且滤光器(20)接收具有对应模式的入射光。循环光的透射分量表示环形谐振器(25)反向传播的谐振峰值。;版权所有:(C)2008,JPO&INPIT

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