CN104819703B - A kind of angle of inclination parameter fitness method that fulcrum is sensed for inclination angle - Google Patents

A kind of angle of inclination parameter fitness method that fulcrum is sensed for inclination angle Download PDF

Info

Publication number
CN104819703B
CN104819703B CN201510216445.8A CN201510216445A CN104819703B CN 104819703 B CN104819703 B CN 104819703B CN 201510216445 A CN201510216445 A CN 201510216445A CN 104819703 B CN104819703 B CN 104819703B
Authority
CN
China
Prior art keywords
inclination
angle
axis
fitting
fulcrum
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201510216445.8A
Other languages
Chinese (zh)
Other versions
CN104819703A (en
Inventor
张军
吴俨
时国坚
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
WUXI WUSHEN TECHNOLOGY Co Ltd
Original Assignee
WUXI WUSHEN TECHNOLOGY Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by WUXI WUSHEN TECHNOLOGY Co Ltd filed Critical WUXI WUSHEN TECHNOLOGY Co Ltd
Priority to CN201510216445.8A priority Critical patent/CN104819703B/en
Publication of CN104819703A publication Critical patent/CN104819703A/en
Application granted granted Critical
Publication of CN104819703B publication Critical patent/CN104819703B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C9/00Measuring inclination, e.g. by clinometers, by levels

Abstract

The invention discloses a kind of angle of inclination parameter fitness method for inclination angle fulcrum, including step:Obtain the actual measurement angle of inclination in X-axis and Y-axis;Degree of tilt parameter fitting model is built, is specifically included:Obtain some groups of Y-axis inclination angle values;Obtain the fitting data of X-axis and Y-axis;X-axis and Y-axis angle of inclination fitting function model are built respectively, and obtain the parameter of each model;Determine X-axis and Y-axis angle of inclination fitting function model;Step value set by step 1 is substituted into the X-axis and Y-axis angle of inclination fitting function model of the gained of step 24, X-axis and Y-axis angle of inclination is obtained;Actual measurement angle of inclination is corrected with reference to resulting X-axis and Y-axis angle of inclination.The present invention can have modified nonlinearity measured directly, allow angle of inclination to reach high accuracy with reference to fitting technique;Existing inclination angle fulcrum precision in measurement can effectively be solved not high, it is impossible to the problem of automatic correction, realize the fitting and correction of parameter.

Description

A kind of angle of inclination parameter fitness method that fulcrum is sensed for inclination angle
Technical field
The present invention relates to a kind of angle of inclination parameter fitness method that fulcrum is sensed for inclination angle, belong to communication and sensing skill The field of art.
Background technology
In the various fields of science and technology, it is often necessary to according to the volume of data obtained by actual test, obtain it Functional relation expression formula.Theoretically, polynomial of degree n f (x) can be constructed according to Interpolation Principle so that f (x) is each The functional value of test point is just by eyeball.
But, under many circumstances, many sample points are acquired in order to reflect truth as far as possible, cause interpolation many The number of times of item formula f (x) is very high, this increases not only the amount of calculation of function, and have impact on approximation ratio;Besides due to interpolation Multinomial can thus retain measurement error by each actual measurement sampling point, so as to influence the precision of fitting function, be difficult reflection real The functional relation of border data.
On this basis, people are improved, and typically take according to known actual test sampling point, find out between tested amount Functional relation so that the relation that the function curve that draws of fitting can fully reflect between actual test amount, here it is bent Line is fitted.As a result, curve fitting technique is in image procossing, reverse-engineering, CAD and test data It is obtained in the field such as treatment display and fault mode diagnosis and is widely applied.
Generally there is inclination angle to sense fulcrum in the communications field, in equipment, and to the angle of inclination of inclination angle sensing fulcrum In technology, thus the angle of inclination direct measurement at the angle of inclination of inclination angle sensing fulcrum is directly obtained using sensor often Inclination angle senses the angle of inclination of fulcrum, also, be analyzed on the basis of measured value obtain corresponding after measurements are taken Conclusion.This also brings some problems, due to the aging of equipment or between coordinate defective tightness, easily cause measurement inclination angle There is error in degree, reduce the precision of measurement, and the angle measured by inclination angle cannot be corrected, so that inclination angle senses Fulcrum is in actual running, and parameter is not accurate.
The content of the invention
The technical problems to be solved by the invention are to overcome the deficiencies in the prior art, there is provided one kind senses branch for inclination angle The angle of inclination parameter fitness method of point, solves existing inclination angle sensing fulcrum precision in measurement not high, it is impossible to automatic correction Problem, realize the fitting and correction of parameter.
It is of the invention specific using following technical scheme solution above-mentioned technical problem:
A kind of angle of inclination parameter fitness method that fulcrum is sensed for inclination angle, comprises the following steps:
Step 1, inclination angle sensing fulcrum is measured according to the step value of setting, obtain the actual measurement in X-axis and Y-axis Angle of inclination;
Step 2, structure degree of tilt parameter fitting model, specifically include following steps:
Step 2-1, the angle of inclination according to different step values to inclination angle sensing fulcrum in X-axis measure, if obtaining Dry group X-axis inclination angle value;Measured according to angle of inclination of the different step values to inclination angle sensing fulcrum in Y-axis, obtained Some groups of Y-axis inclination angle values;
Step 2-2, some groups of X-axis and Y-axis inclination angle value are respectively adopted by line fitting approach and are fitted, obtained The fitting data of X-axis and Y-axis;
Step 2-3, X-axis and Y-axis angle of inclination fitting function model are built respectively, and by the fitting of the X-axis of gained and Y-axis Data substitute into fitting X-axis and Y-axis angle of inclination fitting function model respectively, obtain the parameter of each model;
Step 2-4, each model parameter according to obtained by step 2-3, determine X-axis and Y-axis angle of inclination fitting function model;
Step 3, the step value set by step 1 is substituted into the X-axis angle of inclination fitting function model obtained by step 2-4, Obtain X-axis angle of inclination;And the step value set by step 1 substitutes into the Y-axis angle of inclination fitting function mould obtained by step 2-4 Type, obtains Y-axis angle of inclination;
Step 4, with reference to the X-axis angle of inclination obtained by step 3 to step 1 gained X-axis it is actual measure angle of inclination enter Row correction, and school is carried out to the actual measurement angle of inclination of Y-axis of step 1 gained with reference to the Y-axis angle of inclination obtained by step 3 Just.
Further, as a preferred technical solution of the present invention:The step 2-2 line fitting approach is to use zero point The method for being averaging translation curve carries out curve fitting.
Further, as a preferred technical solution of the present invention:The step 2-4 also includes inclining X-axis and Y-axis Angle fitting function model carries out quadratic fit step.
Further, as a preferred technical solution of the present invention:The step 2-1 is obtained by the two groups of step values for setting Obtain two groups of X-axis inclination angle values and Y-axis inclination angle value.
Further, as a preferred technical solution of the present invention:The step 1 obtains inclination angle using obliquity sensor Actual measurement angle of inclination of the sensing fulcrum in X-axis and Y-axis.
The present invention uses above-mentioned technical proposal, can produce following technique effect:
(1), the angle of inclination parameter fitness method that fulcrum is sensed for inclination angle of the present invention, by actual measurement Inclination angle sensing fulcrum obtains the actual measurement angle of inclination in X-axis and Y-axis, and builds degree of tilt parameter fitting model, and combines The data of measurement substitute into model, and X-axis and Y-axis angle of inclination fitting function model are obtained after obtaining model parameter, then will be corresponding Numerical value substitute into gained model and obtain angle of inclination, and combine and obtain axle angle of inclination the actual measurement angle of inclination of gained is entered Row correction, accurately angle of inclination is calculated by model of fit, it is possible thereby to the error for avoiding direct measurement from existing, school is carried out to it Just, by this fit approach, have modified nonlinearity measured directly so that based on being allowed with reference to fitting technique on the basis of measurement Angle of inclination reaches precision very high.It is high thereby, it is possible to effectively solve existing inclination angle sensing fulcrum precision in measurement, The problem that cannot be corrected automatically, realizes the fitting and correction of parameter.
(2), further, this method is in fit procedure, using the accuracy of line fitting method, further raising side The precision of method.
Brief description of the drawings
Fig. 1 is schematic flow sheet of the present invention for the angle of inclination parameter fitness method of inclination angle sensing fulcrum.
Specific embodiment
Embodiments of the present invention are described with reference to Figure of description.
As shown in figure 1, the present invention devises a kind of angle of inclination parameter fitness method that fulcrum is sensed for inclination angle, including Following steps:
Step 1, inclination angle sensing fulcrum is measured according to the step value of setting, obtain the actual measurement in X-axis and Y-axis Angle of inclination;
Step 2, structure degree of tilt parameter fitting model, specifically include following steps:
Step 2-1, the angle of inclination according to different step values to inclination angle sensing fulcrum in X-axis measure, if obtaining Dry group X-axis inclination angle value;Measured according to angle of inclination of the different step values to inclination angle sensing fulcrum in Y-axis, obtained Some groups of Y-axis inclination angle values;
Step 2-2, some groups of X-axis and Y-axis inclination angle value are respectively adopted by line fitting approach and are fitted, obtained The fitting data of X-axis and Y-axis;
Step 2-3, X-axis and Y-axis angle of inclination fitting function model are built respectively, and by the fitting of the X-axis of gained and Y-axis Data substitute into fitting X-axis and Y-axis angle of inclination fitting function model respectively, obtain the parameter of each model;
Step 2-4, each model parameter according to obtained by step 2-3, determine X-axis and Y-axis angle of inclination fitting function model;
Step 3, the step value set by step 1 is substituted into the X-axis angle of inclination fitting function model obtained by step 2-4, Obtain X-axis angle of inclination;And the step value set by step 1 substitutes into the Y-axis angle of inclination fitting function mould obtained by step 2-4 Type, obtains Y-axis angle of inclination;
Step 4, with reference to the X-axis angle of inclination obtained by step 3 to step 1 gained X-axis it is actual measure angle of inclination enter Row correction, and school is carried out to the actual measurement angle of inclination of Y-axis of step 1 gained with reference to the Y-axis angle of inclination obtained by step 3 Just.
The actual measurement angle of inclination in fulcrum acquisition X-axis and Y-axis is sensed by actual measurement inclination angle, and combination obtains axle Angle of inclination is corrected to the actual measurement angle of inclination of gained, and accurately angle of inclination is calculated by model of fit, thus may be used With the error for avoiding direct measurement from existing, it is corrected, by this fit approach, have modified measured directly non-linear Degree.
In order to verify that parameter fitness method of the invention can realize the correction at the angle of inclination of inclination angle sensing fulcrum, below Enumerate an embodiment to illustrate, embodiment is as follows:
The present embodiment uses SCA100T type obliquity sensors, and SCA100T series is the high-precision dual-axis based on 3D MEMS Obliquity sensor chip, it provides the other performance of horizontal survey instrument grade.The sensing of twin shaft high-precision tilt angle sensor chip Element needs to be mutually perpendicular to measuring table keeping parallelism, and sensor twin shaft in measurement.Weak temperature dependency, height Resolution ratio, low noise and sound sensing element design allow SCA100T-D01, SCA100T-D02 high-precision dual-axis inclination angle to sense Device chip turns into the only selection of Horizontal measuring apparatus.And the mechanical impact force of 20,000g can be withstood up to, it is possible thereby to very It is good in this method.Using inclination of the SCA100T types obliquity sensor measurement inclination angle sensing fulcrum in the case where step value is set, Obtain the actual measurement angle of inclination in X-axis and Y-axis.
Then, degree of tilt parameter fitting model is built.The X-axis angle of inclination fitting function model of structure, i.e. model of fit It is straight line, its formula is as follows:
P=A+BX (1)
Wherein, P is step value;A and B are model parameter, and X is X-axis angle of inclination.
Then, inclination angle sensing fixed pivot on the platform of school position.School position platform steps to+10 ° from -10 °, and step value is 0.2°.An X-axis angle of inclination is obtained in stepping one time.High-ranking officers position platform is set as other step values again, obtains second X-axis Angle of inclination.Thus, two groups of step values by setting obtain two groups of X-axis inclination angle values.
Two groups of X-axis inclination angle values are fitted using line fitting approach, the fitting data of X-axis is obtained.Wherein Fitting data is the correlation function of model parameter A and B.
Then the fitting data of the X-axis of gained substitutes into fitting X-axis angle of inclination fitting function model, obtains the parameter of model The concrete numerical value of number A and B.After being determined by the concrete numerical value of A and B, X-axis angle of inclination fitting function model is obtained.
Similarly, degree of tilt parameter fitting model is built.The Y-axis angle of inclination fitting function model of structure, i.e. model of fit It is straight line, its formula is as follows:
Q=C+BY (2)
Wherein, Q is step value;C and D are model parameter, and Y is Y-axis angle of inclination.
Then, inclination angle sensing fixed pivot on the platform of school position.School position platform steps to+10 ° from -10 °, and step value is 0.2°.A Y-axis angle of inclination is obtained in stepping one time.High-ranking officers position platform is set as other step values again, obtains second Y-axis Angle of inclination.Thus, two groups of step values by setting obtain two groups of Y-axis inclination angle values.
Two groups of Y-axis inclination angle values are fitted using line fitting approach, the fitting data of Y-axis is obtained.Wherein Fitting data is the correlation function of model parameter C and D.
Then the fitting data of the Y-axis of gained substitutes into fitting Y-axis angle of inclination fitting function model, obtains the parameter of model The concrete numerical value of number C and D.After being determined by the concrete numerical value of C and D, Y-axis angle of inclination fitting function model is obtained.
In order to further improve the precision of parameter fitting, the inventive method also includes pair X-axis for determining and Y-axis inclination angle Degree fitting function model carries out quadratic fit step.The quadratic fit process can use various fittings well known in the prior art Method carries out quadratic fit, obtains the model after quadratic fit.As a result, inclination angle value and reality that model of fit is obtained The quadratic sum of the difference between measured value is minimum, for minimum problems therein, can be using using negative gradient direction in gradient method As the direction of search of optimization.
Then, the X-axis angle of inclination fitting function model obtained by set step value is substituted into, obtains X-axis inclination angle Degree;And the Y-axis angle of inclination fitting function model obtained by set step value substitution, obtain Y-axis angle of inclination.
Finally, complete contrast and correct.Specially:With reference to X-axis angle of inclination resulting under model of fit to the X of gained The actual measurement angle of inclination of axle is corrected, and when angle of inclination of the X-axis angle of inclination for obtaining more than actual measurement, chooses it The average of difference increases on the angle of inclination of actual measurement as correction radix, obtains the X-axis angle of inclination of last correction Output.When angle of inclination of the X-axis angle of inclination for obtaining less than actual measurement, the average of its difference is chosen as correction base Number, reduces the correction radix on the actually angle of inclination of measurement, obtains the X-axis angle of inclination output of last correction.
Similarly, school is carried out to the actual measurement angle of inclination of Y-axis of gained to Y-axis angle of inclination resulting under model of fit Just.When angle of inclination of the Y-axis angle of inclination for obtaining more than actual measurement, the average of its difference is chosen as correction base Number, increases on the angle of inclination of actual measurement, obtains the Y-axis angle of inclination output of last correction.When the Y-axis inclination angle for obtaining When degree is less than the angle of inclination that reality is measured, the average of its difference is chosen as correction radix, at the inclination angle of actually measurement The correction radix is reduced on degree, the Y-axis angle of inclination output of last correction is obtained.
To sum up, the angle of inclination parameter fitness method that fulcrum is sensed for inclination angle of the present invention, by model of fit Accurately angle of inclination is calculated, it is possible thereby to the error for avoiding direct measurement from existing, is corrected, by this fitting side to it Formula, have modified nonlinearity measured directly so that based on allowing angle of inclination to reach very with reference to fitting technique on the basis of measurement Precision high.It is not high thereby, it is possible to effectively solve existing inclination angle sensing fulcrum precision in measurement, it is impossible to automatic correction Problem, realizes the fitting and correction of parameter.
Embodiments of the present invention are explained in detail above in conjunction with accompanying drawing, but the present invention is not limited to above-mentioned implementation Mode, in the ken that those of ordinary skill in the art possess, can also be on the premise of present inventive concept not be departed from Make a variety of changes.

Claims (4)

1. it is a kind of for inclination angle sense fulcrum angle of inclination parameter fitness method, it is characterised in that comprise the following steps:
Step 1, inclination angle sensing fulcrum is measured according to the step value of setting, the actual measurement obtained in X-axis and Y-axis is inclined Angle;
Step 2, structure angle of inclination parameter fitting model, specifically include following steps:
Step 2-1, the angle of inclination according to different step values to inclination angle sensing fulcrum in X-axis measure, and obtain some groups of X Axle inclination angle value;Measured according to angle of inclination of the different step values to inclination angle sensing fulcrum in Y-axis, obtain some groups Y-axis inclination angle value;
Step 2-2, some groups of X-axis and Y-axis inclination angle value are respectively adopted by line fitting approach and are fitted, obtain X-axis With the fitting data of Y-axis;
Step 2-3, X-axis and Y-axis angle of inclination fitting function model are built respectively, and by the X-axis of gained and the fitting data of Y-axis Fitting X-axis and Y-axis angle of inclination fitting function model are substituted into respectively, obtain the parameter of each model;
Step 2-4, each model parameter according to obtained by step 2-3, determine X-axis and Y-axis angle of inclination fitting function model;
Step 3, the step value set by step 1 is substituted into the X-axis angle of inclination fitting function model obtained by step 2-4, obtain X Axle angle of inclination;And the step value set by step 1 substitutes into the Y-axis angle of inclination fitting function model obtained by step 2-4, obtains Y-axis angle of inclination;
Step 4, with reference to the X-axis angle of inclination obtained by step 3 to step 1 gained X-axis it is actual measure angle of inclination carry out school Just, and with reference to the Y-axis angle of inclination obtained by step 3 the actual measurement angle of inclination of Y-axis of step 1 gained is corrected.
2. the angle of inclination parameter fitness method that inclination angle senses fulcrum is used for according to claim 1, it is characterised in that:It is described Step 2-4 also includes carrying out quadratic fit step to X-axis and Y-axis angle of inclination fitting function model.
3. the angle of inclination parameter fitness method that inclination angle senses fulcrum is used for according to claim 1, it is characterised in that:It is described Step 2-1 obtains two groups of X-axis inclination angle values and Y-axis inclination angle value by the two groups of step values for setting.
4. the angle of inclination parameter fitness method that inclination angle senses fulcrum is used for according to claim 1, it is characterised in that:It is described Step 1 obtains actual measurement angle of inclination of the inclination angle sensing fulcrum in X-axis and Y-axis using obliquity sensor.
CN201510216445.8A 2015-04-30 2015-04-30 A kind of angle of inclination parameter fitness method that fulcrum is sensed for inclination angle Active CN104819703B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510216445.8A CN104819703B (en) 2015-04-30 2015-04-30 A kind of angle of inclination parameter fitness method that fulcrum is sensed for inclination angle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510216445.8A CN104819703B (en) 2015-04-30 2015-04-30 A kind of angle of inclination parameter fitness method that fulcrum is sensed for inclination angle

Publications (2)

Publication Number Publication Date
CN104819703A CN104819703A (en) 2015-08-05
CN104819703B true CN104819703B (en) 2017-05-31

Family

ID=53730074

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510216445.8A Active CN104819703B (en) 2015-04-30 2015-04-30 A kind of angle of inclination parameter fitness method that fulcrum is sensed for inclination angle

Country Status (1)

Country Link
CN (1) CN104819703B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111043831A (en) * 2019-12-30 2020-04-21 大连民族大学 Space angle detection method based on integral method

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4580926A (en) * 1983-09-28 1986-04-08 Mobil Oil Corporation Foundation level and orientation tool
JP2006077725A (en) * 2004-09-13 2006-03-23 Honda Motor Co Ltd Angle adjustment device for inclination sensor in vehicle
CN101349559B (en) * 2008-09-04 2010-10-13 河北中博联创科技有限公司 Method for testing indication angle of accurate near sea-route indicator light fitting
CN102288162B (en) * 2011-05-23 2013-03-13 南京航空航天大学 Tilt angle sensor based on optical fiber Bragg gratings and method for measuring tilt angle of tilt angle sensor

Also Published As

Publication number Publication date
CN104819703A (en) 2015-08-05

Similar Documents

Publication Publication Date Title
CN110375694B (en) Self-calibration method for circular grating angle measurement error based on portable articulated coordinate measuring machine
CN109990712B (en) Online calibration method for width gauge
CN101706294B (en) Method for automatically judging calibration time of sensor
CN111998919B (en) Gas meter calibration method and device
CN110030953B (en) Circular grating angle measurement error compensation method
CN108362911A (en) A kind of current meter scaling method based on least square method and interpolation method
CN105953946A (en) Least squares algorithm based calibration method for temperature coefficient of fiber optic gyroscope temperature control device
CN106063132A (en) On-chip analog-to-digital converter (adc) linearity test for embedded devices
CN110906993B (en) Flow meter metering temperature compensation method and ultrasonic flow meter
CN106053727A (en) Standard curve correction method and system
CN114608682A (en) Calibration method of flowmeter
EP2905595A1 (en) Gauge Testing Device
CN102879061A (en) Water gauge error correction method based on fitted equation
CN104819703B (en) A kind of angle of inclination parameter fitness method that fulcrum is sensed for inclination angle
CN103542905A (en) Water meter flow identifying method
CN109029304A (en) A kind of surface roughness measuring method of concrete
CN106323587B (en) The monocular video high-precision measuring method of wing model in wind tunnel flexible deformation
CN205642396U (en) High accuracy level bar calibrating installation based on sine
CN112344864A (en) Precision calibration method and device for laser thickness and length synchronous measuring instrument
KR102055055B1 (en) Electronic Flow Meter and The Measurement Error Correcting Methode
CN215004083U (en) Static pressure characteristic testing device of differential pressure transmitter
CN105466631B (en) A kind of calibration method and calibrating installation of piston gage piston effective area
RU200017U1 (en) HIGH PRECISION SPINDLE ASSEMBLY FOR ANGULAR COMPARATOR
CN107607142B (en) A kind of calibration system and scaling method of sensor
CN108375337B (en) Robot and method and device for measuring relative pose of process equipment of robot

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
EXSB Decision made by sipo to initiate substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant