CN111207744B - Pipeline geographical position information measuring method based on thick tail robust filtering - Google Patents
Pipeline geographical position information measuring method based on thick tail robust filtering Download PDFInfo
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- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
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- G01C21/165—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation combined with non-inertial navigation instruments
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Abstract
The invention discloses a pipeline geographical position information measuring method based on thick tail robust filtering, and relates to a technology for measuring geographical position information of a pipeline. Specifically, an inertia/mileage wheel combined positioning system is formed by the MSINS and the mileage wheel, the system power device drives the system power device to run in a pipeline to acquire sensor data related to the pipeline trend, and strapdown inertia calculation and dead reckoning are respectively carried out; the difference value of the strapdown inertial calculation position and the dead reckoning position is used as measurement information, position measurement outlier information caused by the slip of a mileage wheel, the sliding fault and the failure of a pipeline motion constraint condition is filtered by a thick tail robust filter, meanwhile, a strapdown inertial calculation error is estimated, and the pipeline geographic position information is corrected and output, so that the system provides continuous and high-precision pipeline geographic position information.
Description
Technical Field
The invention relates to a method for measuring pipeline geographical position information, in particular to a method for measuring pipeline geographical position information based on thick tail robust filtering.
Background
Underground pipelines are important components of urban infrastructure, and pipelines for water supply, drainage, gas, heat supply and the like convey substances and energy for daily life of people, so that the underground pipelines are life lines for guaranteeing normal and orderly life of cities. However, as the operation time of the pipeline increases and the local geological structure changes, various environmental factors such as settlement, frost heaving and the like easily cause displacement and deformation of the in-service pipeline, so that a local pipe body generates large bending strain, and the pipeline failure problems such as pipeline instability or material damage and the like are caused in serious conditions, so that the structural integrity and the operation safety of the pipeline cannot be guaranteed. In addition, pipeline corrosion, failure of welding seam material and the like can also cause safety accidents such as pipeline leakage, explosion and the like. Therefore, the method has great significance for regularly detecting the running state of the pipeline and effectively preventing and maintaining accidents to guarantee the life and property safety of people. The measurement of the geographical position information of the pipeline is one of the key technologies for realizing the detection of the running state of the pipeline. The effects mainly comprise: 1. accurately measuring the relative displacement and deformation of the pipeline so as to determine whether the structural mechanics is normal or not; 2. the position of the pipeline defect part is accurately determined, so that maintenance operation is facilitated, and waste of manpower, material resources and financial resources caused by blind excavation is avoided.
The traditional underground pipeline positioning method mainly comprises an electromagnetic pipeline detector, a ground penetrating radar and the like. However, these methods often fail to accurately obtain the geographic location information of existing trenchless pipelines due to the influence of pipeline depth or pipeline material. Based on the outstanding measurement capability of the inertial navigation system and the completely autonomous and independent measurement principle, the micro inertial strapdown measurement system (MSINS) is used for measuring the geographic position information of the urban underground pipelines, so that the defects of the existing pipeline positioning method can be overcome, and the requirements of the geographic position information measurement of the urban underground pipelines on low cost, small size, universality and the like can be met. However, since MSINS uses miniature inertial measurement components, micro-mechanical (MEMS) gyroscopes and accelerometers, as its inertial measurement unit, and micro-mechanical gyroscope errors and stability are inferior to other types of gyroscopes, it is generally not suitable for use alone and needs external sensor assistance. In consideration of the special underground application environment of the pipeline, the combination positioning system formed by the MSINS and the mileage wheel is a feasible combination positioning mode. The position information provided by the mileage wheel is used as measurement information, and strapdown inertial calculation errors are estimated and corrected by using a filtering technology, so that the measurement precision of the geographical position information of the pipeline is effectively improved. However, when the odometer wheel runs in a pipeline, problems such as slipping or sliding faults often occur, and factors such as pipeline defects also cause the odometer wheel to generate non-pipeline motion model constraint actions such as jumping, and the above problems cause wild values in the position measurement information of the odometer wheel, so that the measurement noise distribution presents an obvious thick tail phenomenon. In the existing inertia/mileage wheel combined positioning system, the traditional kalman filtering technology is usually used to realize the filtering state estimation. However, the processing of the system noise and the measurement noise by the traditional kalman filtering algorithm is usually assumed to be white gaussian noise, which has obvious modeling error with the thick tail noise in the actual system, thereby reducing the measurement accuracy of the pipeline geographical position information. Therefore, a filtering method capable of processing the thick tail measurement noise is needed to solve the problems of slipping or jumping of the mileage wheel and the like, and further accurate measurement of the geographical position information of the pipeline is achieved.
There are 5 main articles related to the inertia/mileage wheel pipeline combination positioning technology in CNKI, which are:
the pipeline defect positioning technology based on the volume Kalman smoothing filtering is mainly used for researching that an MEMS strapdown inertial measurement system and a mile wheel form a pipeline defect positioning system, wherein a used filtering algorithm is a volume Kalman filter, and a used filtering algorithm in the invention is a thick tail robust filter, so the method is inconsistent with the used filtering algorithm in the invention.
The feasibility research of the detection and positioning scheme in the small-caliber pipeline adopting MEMS inertial navigation mainly researches a pipeline combined positioning technology based on an MEMS strapdown inertial measurement system, a pipeline odometer, a ground marker and pipeline motion constraint, wherein the used filtering algorithm is an extended Kalman filter, and is inconsistent with a combined device and the filtering algorithm used in the invention.
The application of the integrated navigation technology in the oil and gas pipeline surveying and mapping system mainly researches and utilizes a fiber-optic gyroscope strapdown inertial navigation system, a mileage recorder and a fixed-distance magnetic scale signal to form the long-distance oil and gas pipeline surveying and mapping system, wherein the used filtering algorithm is an L-D improved Kalman filter, and is inconsistent with a combined device and the filtering algorithm used in the invention.
The invention relates to a pipeline central line measuring method based on inertial navigation, which mainly researches a pipeline central line measuring system consisting of a laser gyro strapdown inertial navigation system, a mileage meter and a GPS (global position system).
A high-precision positioning method for pipeline detection based on reverse solution mainly researches a pipeline positioning method based on a strapdown inertial navigation system, a speedometer and position mark points, wherein a filter algorithm used by both forward solution and reverse solution is a Kalman filter and is inconsistent with the filter algorithm used by the invention.
Disclosure of Invention
Aiming at the prior art, the technical problem to be solved by the invention is to provide a pipeline geographical position information measuring method based on thick tail robust filtering, which can filter position measuring wild values when non-Gaussian thick tail measuring noise is caused by the slippage of a mileage wheel, sliding fault or damage of a pipeline motion constraint condition, so as to effectively improve the accuracy and stability of the pipeline geographical position information measurement.
In order to solve the technical problem, the invention provides a pipeline geographical position information measuring method based on thick tail robust filtering, which comprises the following steps:
step 1: fixedly mounting a micro-inertia strapdown measuring system and a mileage wheel on a pipeline geographical position information measuring instrument, and placing the pipeline geographical position information measuring instrument at an inlet of a measured pipeline;
step 2: manually binding the position information of the inlet of the pipeline to be measured to a navigation computer of a micro-inertia strapdown measurement system, wherein the initial position information comprises an initial latitudeInitial longitude λ 0 And an initial height h 0 ;
And step 3: preheating and initially aligning the micro-inertia strapdown measurement system;
and 4, step 4: starting a pipeline geographic position information measuring instrument, and driving the instrument to run in a pipeline by using a power device on the measuring instrument so as to acquire sensor data related to the pipeline trend, wherein the sensor data comprises a gyroscope angular speed outputSpecific force output f of accelerometer b And thereinOutputting delta S by mileage increment of the travel wheel;
and 5: strapdown inertial calculation is carried out by utilizing real-time output data of a gyroscope and an accelerometer to obtain a strapdown attitude matrixEast, north and sky speed along a geographic coordinate systemAnd location informationThe position information comprises latitudeLongitude (G)And height
And 6: utilizing the strapdown attitude matrix obtained in the step 5 based on the motion constraint conditions of the pipelineConverting the mileage increment information Δ S of the mileage wheel to a geographic coordinate system, i.e.
And 7: carrying out dead reckoning by using the mileage increment information of the geographic coordinate system obtained in the step 6 to obtain dead reckoning position informationThe dead reckoning position information comprises latitudeLongitude (longitude)And height
And 8: solving the strapdown inertial calculation position information obtained in the step 5Andand the dead reckoning position information obtained in the step 7Anddifferencing to obtain system measurement information Z, i.e.
And step 9: establishing a state equation and a measurement equation of a pipeline geographic position information measurement system;
step 10: starting a thick tail robust filter, and estimating speed errors delta V of the micro-inertia strapdown measurement system along the east direction, the north direction and the sky direction of a geographic coordinate system E ,δV N ,δV U And position errorδλ SINS ,δh SINS ;
Step 11: utilizing the velocity error delta V of the micro inertia strapdown measuring system obtained by estimation in the step 10 along the east direction, the north direction and the sky direction of the geographic coordinate system E ,δV N ,δV U Feeding back to the navigation computer of the micro inertial strapdown measurement system and correcting the measurements made by the micro inertial strapdown measurement systemEast, north and sky speed along a geographic coordinate systemNamely, it is
Using the micro-inertia strapdown measurement system position error estimated in step 10δλ SINS And δ h SINS The latitude of the calculation position information of the micro inertia strapdown measuring system is corrected by feeding back the navigation computer of the micro inertia strapdown measuring systemLongitude (G)And heightNamely, it is
Corrected positionλ SINS And h SINS And outputting the information as the pipeline geographic position information.
The invention also includes:
1. the establishment of the state equation of the pipeline geographical position information measurement system in the step 9 specifically comprises the following steps:
the state variable of the system is
Wherein:
φ=[φ E φ N φ U ] T measuring the attitude angle error of the system for micro-inertia strapdown;
δV n =[δV E δV N δV U ] T measuring the system speed error for the micro-inertia strapdown;
ε b =[ε x ε y ε z ] T the carrier system is the drift of an x, y and z triaxial gyroscope;
κ D =[α θ δK α ψ ] T is a milewheel error, where α θ For pitch setting of declination angle, alpha ψ Setting a deflection angle for the azimuth, wherein delta K is a scale coefficient error;
f is a system state transfer array, gamma is a system noise driving array, W is system noise, and the specific form is as follows:
wherein v is DR The heading speed measured by the mileage wheel can be obtained by the mileage increment measured by the mileage wheel and the time t, namely
For the projection of the odometer wheel speed in the geographical coordinate system, the strapdown attitude matrix obtained in step 5 may be utilizedThe stem-coupled speed v measured by the mileage wheel DR Projection to a geographic coordinate system:
f E ,f N ,f U for the accelerometer specific force output projection in the geographic coordinate system, the strapdown attitude matrix obtained in step 5 may be utilizedOutputting the specific force of the accelerometer obtained in the step 4Projected to a geographical coordinate system
Besides, ω is ie The rotational angular velocity of the earth; 0 m×n Is an m multiplied by n order zero matrix; c ij For the strapdown attitude matrix obtained in step 5Ith row and j column elements; r Mh ,R Nh Measuring the main curvature radius of the meridian and the prime unit circle calculated for the geographic position by using a micro-inertia strapdown measurement system; r MhD ,R NhD The radius of curvature of the prime circle and prime circle calculated by using the dead reckoning geographic position.
The establishment of the measurement equation of the pipeline geographical position information measurement system in the step 9 specifically comprises the following steps:
Z=HX+V
the measurement information Z of the system is obtained in step 8, V is the measurement noise, and H is the measurement matrix
2. The design of the thick tail robust filter in step 10 is as follows:
firstly, discretizing the state equation and the measurement equation of the pipeline geographical position information measurement system obtained in the step 9 respectively to obtain:
X k =F k-1 X k-1 +Γ k-1 W k-1
Z k =H k X k +V k
wherein, F k-1 ,H k ,Γ k-1 The discretized system state transition array, the discretized measurement array and the discretized system noise driving array are adopted; system noise W k-1 And measuring the noise V k Student's t thick tail noise, both with a degree of freedom parameter of γ, i.e.
P(W k )=St(0,Q k ,γ)
P(V k )=St(0,R k ,γ)
Wherein Q is k ,R k Respectively a system noise variance matrix and a measured noise variance matrix;
next, the filter starts to work and starts iterative computation, wherein the k filtering iterative computation step is as follows:
s10.1: update degree of freedom parameter eta' k-1 And calculating a degree of freedom update factor c by using a moment matching method:
S10.3, updating time and calculating the predicted value of the state variableAnd scale matrix prediction:
s10.4: updating the measurement, and calculating the state variable estimation valueAnd scale matrix estimation
Wherein n is dz Measuring dimension for quantity, i.e. n dz =3;
S10.5: updating the parameter η of degree of freedom k :
η k =η k-1 +n dz
The invention has the beneficial effects that:
the invention provides a combined positioning system formed by a micro inertial strapdown measurement system (MSINS) and a low-cost mileage wheel, and a technology for measuring geographical position information of a pipeline. Specifically, the MSINS and the mileage wheel are used to form an inertia/mileage wheel combination positioning system to provide the geographical location information for the pipeline. When the position measurement outlier information appears due to the fact that the mileage wheel slips or the pipeline motion constraint condition is damaged, the position measurement outlier information is filtered by the thick tail robust filter, and therefore the system provides continuous and high-precision pipeline geographic position information.
Compared with the prior art, the method has the following advantages: and the low-cost micro-inertia strapdown measurement system and the odometer are combined to measure the geographical position information of the pipeline. Meanwhile, the odometer wheel position measurement information noise is modeled as Student's t thick tail noise instead of traditional white gaussian noise. In the process of measuring the geographical position information of the pipeline, when position measurement outlier information occurs due to the fact that a mile wheel slips, a sliding fault and a pipeline motion constraint condition fails, a thick-tail robust filter is used for estimating strapdown inertial resolving errors, meanwhile, the position measurement outlier information can be effectively filtered, the problems that a traditional Kalman filtering algorithm is poor in robustness and unstable in an inertial/mile wheel combined system are solved, and therefore continuous and high-precision geographical position information of the pipeline can be provided.
The beneficial effects of the invention are further illustrated by the following steps: comparing simulation results of the micro inertia strapdown measurement system/odometer combined pipeline geographical position information measurement method based on the thick tail robust filtering (STKF) and the combined positioning method based on the conventional Kalman Filtering (KF).
Drawings
FIG. 1 is a flow chart of a micro inertial strapdown measurement system/odometer wheel combination pipeline geographical location information measurement system work based on thick tail robust filtering;
FIG. 2 is a schematic diagram of a movement track of a pipeline geographical position information measuring system;
FIG. 3 is a comparison of position errors after combined inertial/odometer positioning based on conventional Kalman filtering and based on thick-tailed robust filtering;
FIG. 4 is the results of 20 simulation experiments RMSE;
Detailed Description
The following further describes the embodiments of the present invention with reference to the drawings.
The system power device drives the system power device to operate in the pipeline to acquire sensor data related to the pipeline trend, and strapdown inertial resolution and dead reckoning are respectively carried out; and the difference value between the strapdown inertial calculation position and the dead reckoning position is used as measurement information, position measurement outlier information caused by the slip of a mileage wheel, the sliding fault and the failure of a pipeline motion constraint condition is filtered by a thick tail robust filter, and meanwhile, a strapdown inertial calculation error is estimated and the geographic position information of a pipeline is corrected and output.
The invention is described in more detail below by way of example with reference to fig. 1. A pipeline geographical position information measuring method based on thick tail robust filtering comprises the following specific implementation steps:
and 4, starting the pipeline geographic position information measuring instrument, and driving the measuring instrument to run in the pipeline by using a power device on the measuring instrument so as to acquire information related to the pipeline trendThe sensor data including a gyroscope angular velocity outputSpecific force output f of accelerometer b And outputting the mileage increment Delta S of the mileage wheel;
step 5, performing strapdown inertial calculation by utilizing real-time output data of the gyroscope and the accelerometer to obtain a strapdown attitude matrixEast, north and sky speed along a geographic coordinate systemAnd location informationThe position information comprises latitudeLongitude (G)And height
Step 7, carrying out dead reckoning by using the geographical coordinate system mileage increment information obtained in the step 6 to obtain dead reckoning position informationThe dead reckoning position information comprises latitudeLongitude (longitude)And height
Step 9, establishing a state equation and a measurement equation of the pipeline geographical position information measurement system;
Step 11, utilizing the micro inertia strapdown measurement system estimated in the step 10Velocity error delta V of system along east, north and sky directions of geographic coordinate system E ,δV N ,δV U Feeding back to the navigation computer of the micro inertial strapdown measurement system and correcting the speed of the micro inertial strapdown measurement system measured along the east, north and sky directions of the geographic coordinate systemNamely, it is
Using the micro inertial strapdown measurement system position error estimated in step 10δλ SINS And δ h SINS Feeding back to the navigation computer of the micro-inertia strapdown measurement system and correcting the calculated position information latitude of the micro-inertia strapdown measurement systemLongitude (G)And heightNamely, it is
Corrected positionλ SINS And h SINS And outputting the information as the pipeline geographic position information.
The invention also includes:
(1) The system state equation in step 9 is established as follows:
the state variable of the system is
Wherein:
φ=[φ E φ N φ U ] T -measuring the system attitude angle error for a micro inertial strapdown;
δV n =[δV E δV N δV U ] T -measuring the system velocity error for a micro inertial strapdown;
ε b =[ε x ε y ε z ] T -shifting for a carrier system x, y, z triaxial gyro;
κ D =[α θ δK α ψ ] T -as odometer wheel error, where α θ For pitch mounting of declination angle, alpha ψ Setting a deflection angle for the azimuth, wherein delta K is a scale coefficient error;
f is a system state transfer array, gamma is a system noise driving array, W is system noise, and the specific form is as follows:
wherein v is DR The heading speed measured by the mileage wheel can be obtained by the mileage increment measured by the mileage wheel and the time t, namely
For the projection of the odometer wheel speed in the geographical coordinate system, the strapdown attitude matrix obtained in step 5 may be utilizedThe stem-coupled speed v measured by the mileage wheel DR Projected to a geographic coordinate system
f E ,f N ,f U For the projection of the accelerometer specific force output on the geographic coordinate system, the strapdown attitude matrix obtained in step 5 may be utilizedOutputting the specific force of the accelerometer obtained in the step 4Projected to a geographical coordinate system
In addition to this, ω ie The rotational angular velocity of the earth; 0 m×n Is an m multiplied by n order zero matrix; c ij For the strapdown attitude matrix obtained in step 5Ith row and j column elements; r Mh ,R Nh Measuring the main curvature radius of the meridian and the prime unit circle calculated for the geographic position by using a micro-inertia strapdown measurement system; r is MhD ,R NhD The radius of curvature of the prime circle and prime circle calculated by using the dead reckoning geographic position.
(2) The measurement equation in step 9 is established as follows:
Z=HX+V
the measurement information Z of the system is obtained in step 8, V is the measurement noise, and H is the measurement matrix
(3) The thick tail robust filter in step 10 is designed as follows:
firstly, discretizing the state equation and the measurement equation of the pipeline geographical position information measurement system obtained in the step 9 respectively to obtain
X k =F k-1 X k-1 +Γ k-1 W k-1
Z k =H k X k +V k
Wherein, F k-1 ,H k ,Γ k-1 The discretized system state transition array, the discretized measurement array and the discretized system noise driving array are adopted; system noise W k-1 And measuring the noise V k Student's t thick tail noise, both with a degree of freedom parameter of γ, i.e.
P(W k )=St(0,Q k ,γ)
P(V k )=St(0,R k ,γ)
Wherein Q is k ,R k Respectively, a system noise variance matrix and a measured noise variance matrix.
Next, the filter start-up operation starts iterative computation. Wherein, the k filtering iterative computation step is as follows:
(1) updating a degree of freedom parameter eta' k-1 And a degree of freedom update factor c is calculated by using a moment matching method.
(3) Updating time and calculating the predicted value of the state variableAnd a scale matrix predictor.
(4) Performing measurement update to calculate state variable estimation valueAnd scale matrix estimation
Wherein n is dz Measuring the dimension number, i.e. n dz =3。
(5) Updating the degree of freedom parameter eta k 。
η k =η k-1 +n dz
Details not described in the present specification are well within the skill of those in the art.
Simulation verification:
(1) The main sensor parameters in the micro-inertia strapdown measurement system are as follows:
zero bias stability of the MEMS gyroscope: 1 degree/h;
zero offset stability of the MEMS accelerometer: 10 -4 g (g is gravitational acceleration);
error parameters of the mileage wheel device: the pitching installation declination angle is 0.5 degrees, the azimuth installation declination angle is 0.7 degrees, and the scale coefficient error is 0.002;
(2) In order to simulate the position measurement wild value caused by the slippage of the mileage wheel, the sliding fault and the failure of the pipeline motion constraint condition, the measurement noise V is set as follows:
wherein w.p. represents that noise appears with a certain probability, 0.10 represents the probability of appearance of the position measurement field value, and the measurement noise variance matrix R = (diag [10m/Re 10 m)]) 2 And Re is the earth radius.
(3) In the thick-tail robust filter, the filter parameters are set as follows:
degree of freedom eta 0 =5, scale matrix Σ 0 = R, number of iterations N =4.
(4) And (5) carrying out 20 simulation tests, wherein the time length of each simulation test is 1000 seconds. After the initial alignment is completed, the pipeline geographic position information measuring system is set to respectively perform the following movements: firstly, accelerating for 10s along the north direction and then running at a constant speed for 290s; then, the turning (50 s) runs for 100s at a constant speed along the course direction of 90 degrees; is connected withThen, turning again (50 s) and running at constant speed for 490s along the course direction of 180 degrees; finally, the speed is reduced to zero. The acceleration in the operation process is 0.1m/s respectively 2 、-0.1m/s 2 The schematic diagram of the movement track of the pipeline geographical position information measuring system is shown in fig. 2. Evaluating the measurement accuracy of the pipeline geographical position information by using the performance indexes shown in the formulas (2), (3) and (4):
wherein p is k For filtering the corrected position information, mu k For the real position information, M represents the number of simulation steps, and the superscript T represents the matrix transposition.
The invention utilizes the micro inertia strapdown measurement system/odometer combined pipeline geographical position information measurement method based on the thick tail robust filtering (STKF) and the combined positioning method based on the conventional Kalman Filtering (KF) to carry out simulation comparison. The simulation result of the northeast position error corrected by the graph in fig. 3 shows that: the inertia/mileage wheel combination positioning precision based on the conventional Kalman filtering is obviously lower than that of the micro inertia strapdown measurement system/mileage wheel combination pipeline geographical position information measurement method based on the thick tail robust filtering (STKF) provided by the invention. Through 20 times of simulation test results as shown in fig. 4 and table 1, in a 1-kilometer pipeline measurement simulation test, the average measurement error of the pipeline geographical position information provided by the invention is 1.67 meters, and the measurement precision is improved by 49.08% compared with that of the conventional method, so that the precision requirement of the urban underground pipeline geographical position information measurement can be met.
TABLE 1 EMAX and ARMSE results of 120 simulation tests
The invention relates to a pipeline geographical position information measuring method based on a thick tail robust filtering micro-inertia strapdown measuring system/mile wheel combination. The output position of the mileage wheel is used as measurement information to assist a micro-inertia strapdown measurement system, and strapdown inertia calculation errors are estimated and corrected through a thick tail robust filter, so that continuous and high-precision pipeline geographical position information is provided. Meanwhile, when a thick tail robust filter is designed, measurement noise is modeled into Student's t thick tail noise distribution, so that a position measurement wild value can be filtered when the position measurement noise is not Gaussian thick tail noise caused by the fact that a mileage wheel slips, a sliding fault or a pipeline motion constraint condition is damaged, and the accuracy and the stability of pipeline geographic position information measurement are effectively improved.
Claims (3)
1. A pipeline geographical position information measuring method based on thick tail robust filtering is characterized by comprising the following steps:
step 1: fixedly mounting a micro-inertia strapdown measuring system and a mileage wheel on a pipeline geographical position information measuring instrument, and placing the pipeline geographical position information measuring instrument at an inlet of a measured pipeline;
step 2: manually binding the position information of the inlet of the pipeline to be measured to a navigation computer of a micro-inertia strapdown measurement system, wherein the initial position information comprises an initial latitudeInitial longitude λ 0 And an initial height h 0 ;
And step 3: preheating and initially aligning the micro-inertia strapdown measurement system;
and 4, step 4: starting a pipeline geographic position information measuring instrument, and driving the instrument to run in a pipeline by using a power device on the measuring instrument so as to acquire sensor data related to the pipeline trend, wherein the sensor data comprises a gyroscope angular speed outputSpecific force output f of accelerometer b And mileage wheel mileage increment output Δ S;
and 5: strapdown inertial calculation is carried out by utilizing real-time output data of a gyroscope and an accelerometer to obtain a strapdown attitude matrixEast, north and sky speed along a geographic coordinate systemAnd location informationThe position information comprises latitudeLongitude (G)And height
Step 6: utilizing the strapdown attitude matrix obtained in the step 5 based on the constraint condition of the pipeline motionConverting the mileage increment information Δ S of the mileage wheel to a geographical coordinate system, i.e.
And 7: carrying out dead reckoning by using the mileage increment information of the geographic coordinate system obtained in the step 6 to obtain dead reckoning position informationThe dead reckoning position information comprises latitudeLongitude (G)And height
And 8: solving the strapdown inertial calculation position information obtained in the step 5Andand the dead reckoning position information obtained in the step 7Anddifferencing to obtain system measurement information Z, i.e.
And step 9: establishing a state equation and a measurement equation of a pipeline geographic position information measurement system;
step 10: starting a thick tail robust filter, and estimating speed errors delta V of the micro-inertia strapdown measurement system along the east direction, the north direction and the sky direction of a geographic coordinate system E ,δV N ,δV U And position errorδλ SINS ,δh SINS ;
Step 11: utilizing the velocity error delta V of the micro inertia strapdown measuring system obtained by estimation in the step 10 along the east direction, the north direction and the sky direction of the geographic coordinate system E ,δV N ,δV U Feeding back to the navigation computer of the micro inertial strapdown measurement system and correcting the speed of the micro inertial strapdown measurement system measured along the east, north and sky directions of the geographic coordinate systemNamely, it is
Using the micro inertial strapdown measurement system position error estimated in step 10δλ SINS And δ h SINS The latitude of the calculation position information of the micro inertia strapdown measuring system is corrected by feeding back the navigation computer of the micro inertia strapdown measuring systemLongitude (G)And heightNamely, it is
2. The pipeline geographical position information measuring method based on the thick tail robust filtering as claimed in claim 1, wherein: step 9, establishing a state equation of the pipeline geographical position information measurement system specifically comprises:
the state variable of the system is
Wherein:
φ=[φ E φ N φ U ] T measuring the attitude angle error of the system for micro-inertia strapdown;
δV n =[δV E δV N δV U ] T measuring the system speed error for the micro-inertia strapdown;
ε b =[ε x ε y ε z ] T the carrier system is the drift of an x, y and z triaxial gyroscope;
κ D =[α θ δK α ψ ] T is a milewheel error, where α θ For pitch setting of declination angle, alpha ψ Mounting a deflection angle for the azimuth, wherein delta K is a scale coefficient error;
f is a system state transfer array, gamma is a system noise driving array, W is system noise, and the specific form is as follows:
wherein v is DR The heading speed measured by the mileage wheel can be obtained by the mileage increment measured by the mileage wheel and the time t, namely
For the projection of the odometer wheel speed in the geographical coordinate system, the strapdown attitude matrix obtained in step 5 may be utilizedThe stem-coupled speed v measured by the mileage wheel DR Projection onto a geographic coordinate system:
f E ,f N ,f U for the projection of the accelerometer specific force output on the geographic coordinate system, the strapdown attitude matrix obtained in step 5 may be utilizedOutputting the specific force of the accelerometer obtained in the step 4Projected to a geographical coordinate system
Besides, ω is ie The rotational angular velocity of the earth; 0 m×n Is an m multiplied by n order zero matrix; c ij For the strapdown attitude matrix obtained in step 5Row i and column j; r Mh ,R Nh Measuring the main curvature radius of the meridian and the prime unit circle calculated for the geographic position by using a micro-inertia strapdown measurement system; r MhD ,R NhD Calculating the main curvature radius of a meridian circle and a prime circle by using the dead reckoning geographic position;
step 9, the establishment of the measurement equation of the pipeline geographical location information measurement system specifically comprises:
Z=HX+V
the measurement information Z of the system is obtained in step 8, V is the measurement noise, and H is the measurement matrix
3. The pipeline geographical position information measurement method based on the thick tail robust filtering as claimed in claim 1 or 2, wherein: step 10, the design of the thick tail robust filter is as follows:
firstly, discretizing the state equation and the measurement equation of the pipeline geographical position information measurement system obtained in the step 9 respectively to obtain:
X k =F k-1 X k-1 +Γ k-1 W k-1
Z k =H k X k +V k
wherein, F k-1 ,H k ,Γ k-1 The discretized system state transition array, the discretized measurement array and the discretized system noise driving array are obtained; system noise W k-1 And measuring the noise V k Student's t thick tail noise, both with a degree of freedom parameter of γ, i.e.
P(W k )=St(0,Q k ,γ)
P(V k )=St(0,R k ,γ)
Wherein,Q k ,R k Respectively a system noise variance matrix and a measured noise variance matrix;
next, the filter starts to work and starts iterative computation, wherein the k filtering iterative computation step is as follows:
s10.1: updating a degree of freedom parameter eta' k-1 And calculating a degree of freedom update factor c by using a moment matching method:
S10.3, updating time and calculating the predicted value of the state variableAnd scale matrix prediction:
s10.4: updating the measurement, and calculating the state variable estimation valueAnd scale matrix estimation
Wherein n is dz Measuring the dimension number, i.e. n dz =3;
S10.5: updating the degree of freedom parameter eta k :
η k =η k-1 +n dz
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