CN103697879A - Fiber-optic gyroscope light path - Google Patents
Fiber-optic gyroscope light path Download PDFInfo
- Publication number
- CN103697879A CN103697879A CN201310715026.XA CN201310715026A CN103697879A CN 103697879 A CN103697879 A CN 103697879A CN 201310715026 A CN201310715026 A CN 201310715026A CN 103697879 A CN103697879 A CN 103697879A
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- Prior art keywords
- fiber
- light path
- optical fibre
- fibre gyro
- coupled
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/58—Turn-sensitive devices without moving masses
- G01C19/64—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
- G01C19/72—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams with counter-rotating light beams in a passive ring, e.g. fibre laser gyrometers
- G01C19/725—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams with counter-rotating light beams in a passive ring, e.g. fibre laser gyrometers using nxn optical couplers, e.g. 3x3 couplers
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/58—Turn-sensitive devices without moving masses
- G01C19/64—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
- G01C19/72—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams with counter-rotating light beams in a passive ring, e.g. fibre laser gyrometers
- G01C19/728—Assemblies for measuring along different axes, e.g. triads
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- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Optics & Photonics (AREA)
- Electromagnetism (AREA)
- Power Engineering (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Gyroscopes (AREA)
Abstract
The invention relates to a fiber-optic gyroscope light path. The fiber-optic gyroscope light path is characterized in that a superfluorescence light source is coupled into a 1*3 optical fiber coupler after passing through an isolator, output superfluorescence is divided into three paths, each path of the output superfluorescence is coupled into first, second and third detectors and first, second and third Y waveguides by virtue of first, second and third 2*2 optical fiber couplers, and the two optical fiber emergent end surfaces of the first, second and third Y waveguides are coupled with two tail fibers of first, second and third optical fiber rings. The fiber-optic gyroscope light path provided by the invention has the advantages that the stability is good, the precision is high, and a fiber-optic gyroscope inertial navigation system has a miniaturization property.
Description
Technical field
The light path that the present invention relates to a kind of optical fibre gyro, is applied to three axis optical fibre gyro.
Background technology
Development along with optical fibre gyro inertial navigation system, optical fibre gyro is widely used, but three single axis fiber gyros that three directions are mutually orthogonal in inertial navigation system, have been used, make like this cost of inertial navigation system higher, size is larger, and in each optical fibre gyro, super-fluorescence light source exists inevitable difference and makes the precision of each optical fibre gyro different, and then has limited the overall precision of optical fibre gyro inertial navigation system.
Summary of the invention
In order to overcome the shortcoming of prior art, the invention provides a kind of optical fibre gyro light path, its good stability, precision is high, can make the miniaturization of optical fibre gyro inertial navigation system.
The present invention solves the technical scheme that its technical matters takes: super-fluorescence light source is coupled into 1 * 3 fiber coupler by isolator, the superfluorescence of output is divided into three tunnels, each road is coupled with first, second, third detector and first, second, third Y waveguide respectively through 2 * 2 first, second, third fiber couplers, two optical fiber outgoing end faces of first, second, third Y waveguide and first, second, third fiber optic loop two pigtail couplings.
The invention enables three mutually orthogonal fiber optic loop to share a super-fluorescence light source, and after super-fluorescence light source, add an isolator, to improve stability and the precision of optical fibre gyro, thereby make the miniaturization of optical fibre gyro inertial navigation system.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the present invention is further described.
Fig. 1 is index path of the present invention.
Embodiment
As shown in Figure 1, super-fluorescence light source 1 is coupled into 1 * 3 fiber coupler 2 by isolator 14, the superfluorescence of output is divided into three tunnels, each road is coupled with first, second, third detector 3,12,13 and first, second, third Y waveguide 5,9,10 respectively through 2 * 2 first, second, third fiber couplers 4,11,15, two optical fiber outgoing end faces of first, second, third Y waveguide 5,9,10 and 6,7,8 liang of pigtail couplings of first, second, third fiber optic loop.
The light emitting tail fiber of described isolator 14 should with 1 * 3 fiber coupler 2 coupled fiber pattern match.
First, second, third 2 * 2 described fiber coupler 4,11,15 residue fiber end faces are cut oblique 45 °, in case swash, penetrate.
First, second, third 2 * 2 described fiber coupler 4,11,15 should enter fine pattern match with first, second, third Y waveguide 5,9,10.
First, second, third described Y waveguide 5,9,10 tail optical fibers should with fiber optic loop first, second, third 6,7,8 tail optical fiber pattern match.
Claims (5)
1. an optical fibre gyro light path, it is characterized in that: super-fluorescence light source (1) is coupled into 1 * 3 fiber coupler (2) by isolator (14), the superfluorescence of output is divided into three tunnels, each road is coupled with first, second, third detector (3,12,13) and first, second, third Y waveguide (5,9,10) respectively through 2 * 2 first, second, third fiber couplers (4,11,15), two optical fiber outgoing end faces of first, second, third Y waveguide (5,9,10) and first, second, third fiber optic loop (6,7,8), two pigtail couplings.
2. optical fibre gyro light path according to claim 1, is characterized in that: the light emitting tail fiber of described isolator (14) should with 1 * 3 fiber coupler (2) coupled fiber pattern match.
3. optical fibre gyro light path according to claim 1, is characterized in that: first, second, third 2 * 2 described fiber coupler (4,11,15) residue fiber end face is cut oblique 45 °.
4. optical fibre gyro light path according to claim 1, is characterized in that: first, second, third 2 * 2 described fiber coupler (4,11,15) should enter fine pattern match with first, second, third Y waveguide (5,9,1) 0.
5. optical fibre gyro light path according to claim 1, is characterized in that: first, second, third described Y waveguide (5,9,10) tail optical fiber should with fiber optic loop first, second, third (6,7,8) tail optical fiber pattern match.
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CN201310715026.XA CN103697879A (en) | 2013-12-20 | 2013-12-20 | Fiber-optic gyroscope light path |
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CN201310715026.XA CN103697879A (en) | 2013-12-20 | 2013-12-20 | Fiber-optic gyroscope light path |
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CN103697879A true CN103697879A (en) | 2014-04-02 |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106596075A (en) * | 2016-12-29 | 2017-04-26 | 北京航天时代光电科技有限公司 | Interferometer assembling quality detection system |
CN110579204A (en) * | 2019-08-20 | 2019-12-17 | 北京航空航天大学 | Optical fiber coupler array for triaxial integrated optical fiber gyroscope |
CN112781579A (en) * | 2021-01-29 | 2021-05-11 | 湖北三江航天红峰控制有限公司 | Six-axis integrated optical fiber gyroscope light path structure |
CN113804178A (en) * | 2021-08-20 | 2021-12-17 | 北京航天时代光电科技有限公司 | High-precision and miniaturized triaxial integrated optical fiber gyroscope based on double erbium source redundancy design |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102207387A (en) * | 2011-04-12 | 2011-10-05 | 浙江大学 | Triaxial integration all-optical fiber inertia sensing device |
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2013
- 2013-12-20 CN CN201310715026.XA patent/CN103697879A/en active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102207387A (en) * | 2011-04-12 | 2011-10-05 | 浙江大学 | Triaxial integration all-optical fiber inertia sensing device |
Non-Patent Citations (2)
Title |
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吴军伟等: "微小型三轴光纤陀螺技术", 《红外与激光工程》 * |
翁炬等: "向高精度发展的干涉型光纤陀螺仪技术", 《中国惯性技术学报》 * |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106596075A (en) * | 2016-12-29 | 2017-04-26 | 北京航天时代光电科技有限公司 | Interferometer assembling quality detection system |
CN110579204A (en) * | 2019-08-20 | 2019-12-17 | 北京航空航天大学 | Optical fiber coupler array for triaxial integrated optical fiber gyroscope |
CN112781579A (en) * | 2021-01-29 | 2021-05-11 | 湖北三江航天红峰控制有限公司 | Six-axis integrated optical fiber gyroscope light path structure |
CN112781579B (en) * | 2021-01-29 | 2022-03-08 | 湖北三江航天红峰控制有限公司 | Six-axis integrated optical fiber gyroscope light path structure |
CN113804178A (en) * | 2021-08-20 | 2021-12-17 | 北京航天时代光电科技有限公司 | High-precision and miniaturized triaxial integrated optical fiber gyroscope based on double erbium source redundancy design |
CN113804178B (en) * | 2021-08-20 | 2023-02-24 | 北京航天时代光电科技有限公司 | High-precision miniaturized triaxial integrated optical fiber gyroscope based on double erbium source redundancy design |
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Application publication date: 20140402 |