Small jitter frequency stabilization method of four-frequency laser gyro
Patent Information
- Authority / Receiving Office
- CN Β· China
- Current Assignee / Owner
- NAT UNIV OF DEFENSE TECH
- Publication Date
- 2011-02-16
- Estimated Expiration
- Not applicable Β· inactive patent
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Abstract
Description
technical field
[0001] The invention relates to a four-frequency laser gyro, in particular to a frequency stabilization method for a four-frequency laser gyro. Background technique
[0002] The laser gyroscope has the advantages of large dynamic range, no acceleration effect, simple structure, and small size. It is an ideal component for inertial systems, especially strapdown inertial systems, and has been widely used in military and civilian fields. The principle of the laser gyroscope is the Sagnac effect, and at least one pair of counterpropagating light waves run in its optical resonant cavity. When it rotates around the sensitive axis relative to the inertial space, the frequency of the opposite traveling waves splits to form a beat frequency proportional to the rotation rate, so the rotation information of the laser gyroscope relative to the inertial space can be obtained by measuring the beat frequency.
[0003] Due to the energy coupling between opposing traveling w...