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A Digital Closed-Loop Fiber Optic Gyroscope with Dual Interferometer System

A fiber optic gyroscope, digital closed-loop technology, applied in Sagnac effect gyroscopes, gyroscopes/steering sensing equipment, instruments, etc., can solve problems such as large errors and insufficient accuracy of fiber optic gyroscopes

Active Publication Date: 2017-08-29
中航捷锐(西安)光电技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of the above analysis, the present invention aims to provide a digital closed-loop fiber optic gyroscope with a dual interferometer system to solve the problems of insufficient precision or relatively large errors in existing fiber optic gyroscopes

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  • A Digital Closed-Loop Fiber Optic Gyroscope with Dual Interferometer System
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  • A Digital Closed-Loop Fiber Optic Gyroscope with Dual Interferometer System

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Embodiment Construction

[0044] Preferred embodiments of the present invention will be specifically described below in conjunction with the accompanying drawings, wherein the accompanying drawings constitute a part of the application and are used together with the embodiments of the present invention to explain the principle of the present invention.

[0045] Such as figure 1 as shown, figure 1 It is a schematic structural diagram of the digital closed-loop fiber optic gyroscope according to the embodiment of the present invention, which mainly includes: a light generating module, a third beam splitter, a first angular velocity sensitive module, a second angular velocity sensitive module, an optical fiber ring and a logic circuit, wherein,

[0046] The light generating module includes: a light source and a light driver. The light emitted by the light source driven by the constant current source driven by the light source passes through the third beam splitter to form two beams of incident light, which...

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Abstract

The invention discloses a digital closed loop optical fiber gyroscope with a double-interferometer system. The digital closed loop optical fiber gyroscope comprises a light source driver, a light source, a third beam splitter, a first angular speed sensing module, a second angular speed sensing module, an optical fiber ring and a logic circuit, wherein light emitted by the light source is divided into two beams of incident light after passing through the third beam splitter, and the two beams of incident light respectively enter the first angular speed sensing module and the second angular speed sensing module; the two modules uses the same optical fiber ring, so that two different interferometers are formed in the polarization maintaining optical fiber ring and respectively output signals; the logic circuit receives the signals and performs differential calculation to obtain speed information sensed by the interferometers. The digital closed loop optical fiber gyroscope disclosed by the invention controls a polarization state through a polarization beam splitting / combing device through the same polarization maintaining optical fiber ring, so that the two interferometers in different polarization states are formed in the optical fiber ring; the two polarization states are separated, so that the light-based double-polarization double-interferometer system is implemented, and the precision of the digital closed loop optical fiber gyroscope can be obviously improved, and the intensity noise of the light source is suppressed.

Description

technical field [0001] The invention relates to the field of optoelectronic technology, in particular to a digital closed-loop fiber optic gyroscope with a double interferometer system. Background technique [0002] Fiber optic gyroscope is a new type of solid-state inertial instrument combined with inertial technology, optoelectronic technology and modern manufacturing technology. It is currently the only silent gyroscope that can cover high, medium and low precision. Fiber optic gyroscope is a new generation of angular rate and angular displacement sensors, used for navigation and attitude control in satellites, aircraft, missiles, ships, vehicles, surveying and exploration, robots and other fields. It is the third generation of gyroscopes after electromechanical gyroscopes and laser gyroscopes . It has the characteristics of simple structure, low cost, quick start (zero start can be realized), high reliability, strong shock and vibration resistance, and long service life...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C19/72
CPCG01C19/721G01C19/726
Inventor 曹阳赵平王夏霄
Owner 中航捷锐(西安)光电技术有限公司
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