CN108168536A - The accurate measurement method of optical fibre gyro zero bias - Google Patents

The accurate measurement method of optical fibre gyro zero bias Download PDF

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Publication number
CN108168536A
CN108168536A CN201711324841.8A CN201711324841A CN108168536A CN 108168536 A CN108168536 A CN 108168536A CN 201711324841 A CN201711324841 A CN 201711324841A CN 108168536 A CN108168536 A CN 108168536A
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China
Prior art keywords
optical fibre
fibre gyro
zero bias
output
gyro
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CN201711324841.8A
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杨鹏
何虹锋
黄今纯
薛晓蕾
王君
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Shaanxi Baocheng Aviation Instrument Co Ltd
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Shaanxi Baocheng Aviation Instrument Co Ltd
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Priority to CN201711324841.8A priority Critical patent/CN108168536A/en
Publication of CN108168536A publication Critical patent/CN108168536A/en
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/58Turn-sensitive devices without moving masses
    • G01C19/64Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
    • G01C19/72Gyrometers 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
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C25/00Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Manufacturing & Machinery (AREA)
  • Optics & Photonics (AREA)
  • Electromagnetism (AREA)
  • Power Engineering (AREA)
  • Gyroscopes (AREA)

Abstract

A kind of accurate measurement method of optical fibre gyro zero bias is provided, by measuring output of the positive optical fibre gyro being installed on horizontal base within the t time cycles and obtaining output mean value, reversely the output within the t ¢ time cycles of the optical fibre gyro that is installed on horizontal base and obtain output mean value, byWithIt calculates and obtains optical fibre gyro zero bias B0.Corresponding output mean value when the present invention is installed on horizontal base by measuring and calculating optical fibre gyro forward and reverse, realize the accurate zero bias that optical fibre gyro is obtained by corresponding output mean value computation, so as to make optical fibre gyro sensitive axes that need not be directed toward East and West direction, thoroughly eliminate the influence of earth rotation, dependence of the optical fibre gyro to test condition is reduced, accurate zero reference is provided for measuring system resolving.

Description

The accurate measurement method of optical fibre gyro zero bias
Technical field
The invention belongs to inertia sensing technical fields, and in particular to a kind of accurate measurement method of optical fibre gyro zero bias.
Background technology
Optical fibre gyro is a kind of novel inertia device, using the Sagnac effects of light as theoretical foundation, for measuring carrier phase To the angle rate signal in space, belong to all solid state gyro, since with small, precision is high, and environmental suitability is strong, reliability is high The features such as, it is one of mainstream inertia device of developed recently, therefore, establishing the optical fibre gyro leading indicator measuring method of science is Very necessary, optical fibre gyro leading indicator is divided into two classes, and one kind is to assess fiber optic gyroscope performance index (such as:Bias instaility, Bias repeatability, scale factory non-linearity degree and random walk etc.), one kind is characterization optical fibre gyro ATTRIBUTE INDEX (such as zero bias, mark Spend factor).The measuring system formed using optical fibre gyro as inertia device, other than the performance indicator for meeting system requirements, more Accurate ATTRIBUTE INDEX is provided, the zero reference or proportionate relationship calculated and outputted as system.For optical fibre gyro zero bias B0 (English represents:Bias Bias Offset) test method, i.e., when input angle speed is zero, weigh optical fibre gyro output The size of mean value is measured, is represented with the corresponding equivalent inpnt angular speed of output quantity mean value in the stipulated time.According to《GJB2426A- 2004 method for testing optical fiber gyroscope》, optical fibre gyro is fixed on by installs fixture on horizontal reference, in order to eliminate earth rotation Caused angular speed is influenced (except earth south poles), it is desirable that optical fibre gyro sensitive axes are directed toward East and West direction, but are actually measuring Cheng Zhong, optical fibre gyro reference for installation axis are directed toward East and West direction, there are problems that alignment precision, unless there are special guiding calibration, test It is required that height, limitation are big, especially for middle high-precision optical fiber gyro, sensitivity is not more than 0.5 °/h, due to earth rotation Sensibility, zero bias test error bigger caused by sensitive axes are aligned, in summary, it is necessary to be improved.
Invention content
Present invention solves the technical problem that:A kind of accurate measurement method of optical fibre gyro zero bias is provided, by measuring and counting It calculates optical fibre gyro forward and reverse and is installed on corresponding output mean value during horizontal base, realize by corresponding output mean value computation The accurate zero bias of optical fibre gyro are obtained, so as to make optical fibre gyro sensitive axes that need not be directed toward East and West direction, thoroughly eliminate earth rotation It influences, reduces dependence of the optical fibre gyro to test condition, accurate zero reference is provided for measuring system resolving.
The technical solution adopted by the present invention:The accurate measurement method of optical fibre gyro zero bias is installed on water by measuring forward direction The output within the t time cycles of optical fibre gyro on flat pedestal simultaneously obtains output mean valueReversely it is installed on horizontal base Output of the optical fibre gyro within the t ' time cycles simultaneously obtains output mean valueByWithObtain optical fibre gyro zero bias B0Calculating Formula is as follows:
Wherein, K is optic fiber gyroscope graduation factor.
The accurate measurement method of optical fibre gyro zero bias, includes the following steps:
1) sensitive axes of optical fibre gyro are installed on horizontal base and optical fibre gyro remains stationary state straight up, when Between the output quantity F of optical fibre gyro is measured in period ti(i=1,2,3 ... n), passes through optical fibre gyro output quantity FiCalculate optical fiber top The output mean value of spiral shellFormula it is as follows:
Wherein K be optic fiber gyroscope graduation factor, B0For optical fibre gyro zero bias, ΩeFor Earth rotation angular speed,The latitude local for test;
2) sensitive axes of optical fibre gyro are installed on horizontal base and optical fibre gyro remains stationary state straight down, when Between period t ' it is interior measure optical fibre gyro output quantity Fi' (i=1,2,3 ... n), passes through optical fibre gyro output quantity Fi' calculating optical fiber The output mean value of gyroFormula it is as follows:
3) the corresponding earth rate component of local latitude is eliminated after step 1) is added with the formula in step 2), is obtained Optical fibre gyro zero biasDue to Therefore it obtains Optical fibre gyro zero bias
The present invention compared with prior art the advantages of:
1st, make optical fibre gyro sensitive axes that need not be directed toward East and West direction by this method, thoroughly eliminate earth rotation to optical fibre gyro Influence, reduce dependence of the optical fibre gyro to test condition, resolved for measuring system and accurate zero reference is provided;
2nd, test and computational methods are simple and effective, and practical, easily operated, and the optical fibre gyro zero bias precision calculated is high.
Specific embodiment
Embodiment
The accurate measurement method of optical fibre gyro zero bias, by measuring the positive optical fibre gyro being installed on horizontal base in t Output in time cycle simultaneously obtains output mean valueReversely the optical fibre gyro on horizontal base is installed within the t ' time cycles Output and obtain output mean valueByWithObtain optical fibre gyro zero bias B0Calculation formula it is as follows:
Wherein, K is optic fiber gyroscope graduation factor.
The accurate measurement method of optical fibre gyro zero bias, includes the following steps:
1) sensitive axes of optical fibre gyro are installed on horizontal base and optical fibre gyro remains stationary state straight up, when Between the output quantity F of optical fibre gyro is measured in period ti(i=1,2,3 ... n), passes through optical fibre gyro output quantity FiCalculate optical fiber top The output mean value of spiral shellFormula it is as follows:
Wherein K be optic fiber gyroscope graduation factor, B0For optical fibre gyro zero bias, ΩeFor Earth rotation angular speed,The latitude local for test;
2) sensitive axes of optical fibre gyro are installed on horizontal base and optical fibre gyro remains stationary state straight down, when Between period t ' it is interior measure optical fibre gyro output quantity Fi' (i=1,2,3 ... n), passes through optical fibre gyro output quantity Fi' calculating optical fiber The output mean value of gyroFormula it is as follows:
3) the corresponding earth rate component of local latitude is eliminated after step 1) is added with the formula in step 2), is obtained Optical fibre gyro zero biasDue to Therefore it obtains Optical fibre gyro zero bias
In step 1) and step 2), generally there is Geometrical Tolerance Principle to the mounting plane of optical fibre gyro and horizontal base, Therefore, optical fibre gyro installation error deviation pairWithInfluence it is smaller, meanwhile, optical fibre gyro installation error deviation is opposite In optical fibre gyro zero bias B0For earth rate component, error deviation value can be neglected, therefore by step 1) and step 2) the accurate optical fibre gyro zero bias B in step 3) is obtained0.Make optical fibre gyro sensitive axes that need not be directed toward thing by this method To thoroughly influence of the elimination earth rotation to optical fibre gyro reduces dependence of the optical fibre gyro to test condition, be measuring system solution It calculates and accurate zero reference is provided, test and computational methods are simple and effective, and practical, easily operated, the optical fibre gyro calculated Zero bias precision is high.
Above-described embodiment, only presently preferred embodiments of the present invention, is not used for limiting the scope of the present invention, therefore all with this The equivalence changes that content described in invention claim is done should all be included within scope of the invention as claimed.

Claims (2)

1. the accurate measurement method of optical fibre gyro zero bias, it is characterised in that:The light being installed on horizontal base by measuring forward direction Output of the fine gyro within the t time cycles simultaneously obtains output mean valueThe optical fibre gyro on horizontal base is reversely installed in t ' Output in time cycle simultaneously obtains output mean valueByWithObtain optical fibre gyro zero bias B0Calculation formula it is as follows:
Wherein, K is optic fiber gyroscope graduation factor.
2. the accurate measurement method of optical fibre gyro zero bias according to claim 1, it is characterised in that:Include the following steps:
1) sensitive axes of optical fibre gyro are installed on horizontal base and optical fibre gyro remains stationary state straight up, in week time The output quantity F of optical fibre gyro is measured in phase ti(i=1,2,3 ... n), passes through optical fibre gyro output quantity FiCalculate optical fibre gyro Export mean valueFormula it is as follows:
Wherein K be optic fiber gyroscope graduation factor, B0For optical fibre gyro zero bias, ΩeFor the earth Rotation angular speed,The latitude local for test;
2) sensitive axes of optical fibre gyro are installed on horizontal base and optical fibre gyro remains stationary state straight down, in week time The interior output quantity F for measuring optical fibre gyro of phase t 'i' (i=1,2,3 ... n), passes through optical fibre gyro output quantity Fi' calculating optical fibre gyro Output mean valueFormula it is as follows:
3) the corresponding earth rate component of local latitude is eliminated after step 1) is added with the formula in step 2), obtains optical fiber Gyro zero biasDue to Therefore optical fiber is obtained Gyro zero bias
CN201711324841.8A 2017-12-13 2017-12-13 The accurate measurement method of optical fibre gyro zero bias Pending CN108168536A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109813296A (en) * 2019-03-24 2019-05-28 浙江大学 A kind of angle measurement unit and method for eliminating optic fiber gyroscope graduation factor error
CN113267202A (en) * 2021-04-28 2021-08-17 广东国天时空科技有限公司 Optical fiber gyroscope scale factor nonlinear error compensation method
CN114061617A (en) * 2020-08-05 2022-02-18 上海傲世控制科技股份有限公司 Non-orthogonal dynamic calibration method for optical fiber gyroscope
CN115638807A (en) * 2022-12-21 2023-01-24 中国船舶集团有限公司第七〇七研究所 Optical fiber gyroscope precision testing method based on earth rotation

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CN105444777A (en) * 2015-11-06 2016-03-30 北京航天时代光电科技有限公司 Method for testing error of optical fiber gyro under swing condition

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CN102519487A (en) * 2011-12-14 2012-06-27 浙江大学 Method for evaluating resolution of fiber-optic gyroscope
CN103913168A (en) * 2014-03-06 2014-07-09 哈尔滨工程大学 Double-axis rotary strapdown inertial navigation system transposition method
CN104197957A (en) * 2014-08-25 2014-12-10 哈尔滨工业大学 Micro-gyroscope measurement system and method for measuring zero-bias stability by using system
CN105444777A (en) * 2015-11-06 2016-03-30 北京航天时代光电科技有限公司 Method for testing error of optical fiber gyro under swing condition

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109813296A (en) * 2019-03-24 2019-05-28 浙江大学 A kind of angle measurement unit and method for eliminating optic fiber gyroscope graduation factor error
CN109813296B (en) * 2019-03-24 2020-12-15 浙江大学 Angle measuring device and method for eliminating scale factor error of fiber-optic gyroscope
CN114061617A (en) * 2020-08-05 2022-02-18 上海傲世控制科技股份有限公司 Non-orthogonal dynamic calibration method for optical fiber gyroscope
CN114061617B (en) * 2020-08-05 2024-04-09 上海傲世控制科技股份有限公司 Non-orthogonal dynamic calibration method for fiber-optic gyroscope
CN113267202A (en) * 2021-04-28 2021-08-17 广东国天时空科技有限公司 Optical fiber gyroscope scale factor nonlinear error compensation method
CN113267202B (en) * 2021-04-28 2024-03-08 广东国天时空科技有限公司 Nonlinear error compensation method for scale factors of fiber-optic gyroscope
CN115638807A (en) * 2022-12-21 2023-01-24 中国船舶集团有限公司第七〇七研究所 Optical fiber gyroscope precision testing method based on earth rotation

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Application publication date: 20180615