CN103105509A - Nonlinear correction method of zero temperature drift of acceleration sensor - Google Patents

Nonlinear correction method of zero temperature drift of acceleration sensor Download PDF

Info

Publication number
CN103105509A
CN103105509A CN2013100095083A CN201310009508A CN103105509A CN 103105509 A CN103105509 A CN 103105509A CN 2013100095083 A CN2013100095083 A CN 2013100095083A CN 201310009508 A CN201310009508 A CN 201310009508A CN 103105509 A CN103105509 A CN 103105509A
Authority
CN
China
Prior art keywords
temperature
zero
precision
point
value
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.)
Pending
Application number
CN2013100095083A
Other languages
Chinese (zh)
Inventor
王治国
童晓华
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.)
SHANGHAI BULUE TECHNOLOGY Co Ltd
Original Assignee
SHANGHAI BULUE 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 SHANGHAI BULUE TECHNOLOGY Co Ltd filed Critical SHANGHAI BULUE TECHNOLOGY Co Ltd
Priority to CN2013100095083A priority Critical patent/CN103105509A/en
Publication of CN103105509A publication Critical patent/CN103105509A/en
Pending legal-status Critical Current

Links

Landscapes

  • Indication And Recording Devices For Special Purposes And Tariff Metering Devices (AREA)

Abstract

Provided is a nonlinear correction method of zero temperature drift of an acceleration sensor. Zero deviation value of each acceleration sensor changes with different temperature deviation values, so precision of an acceleration magnitude is influenced to a great extent. The invention puts forward a correction method of zero temperature drift: first, arranging three specific correction temperature points according to a temperature working range which is required by precision; then recording three corresponding zero deviation values, evaluating a specific quadratic polynomial equation of one variable of the acceleration magnitude by conducting Lagrange's interpolation on three groups of values and obtaining the zero deviation values with temperature changes; finally choosing a specific temperature point for verification, comparing the real value of the zero deviation with the calculated value of the zero deviation so as to test whether the precision fits in with the specification. The nonlinear correction method of zero temperature drift of the acceleration sensor corrects the zero deviation of the acceleration sensor and necessarily improves precision and stability of the acceleration, especially the angle precision of measurement and application of an angle of inclination.

Description

The non-linear correction method that the zero point of acceleration transducer, temperature was floated
Technical field
This patent relates to the application of the accuracy correction of acceleration sensing technical field, particularly acceleration.
Background technology
Acceleration transducer is because have various in various degree skews with temperature zero point, so precision of its output accekeration can't ensure, is difficult to use in actual application environment again; Simultaneously, because zero migration value and temperature are not to be linear relationship, therefore take the method for linearity correction zero temperature skew, also can't really improve the precision of acceleration, satisfy practical application to the high-precision requirement of accekeration.
Summary of the invention
The object of the invention is to the zero migration value by the corrected acceleration sensor, improve significantly the precision of acceleration and ensure its stability.
The present invention is the non-linear correction method that zero point, temperature was floated of acceleration transducer.At first according to the temperature working range of accuracy requirement, two critical and normal temperature are set amount to three Tc points, then ask for three zero migration values corresponding to these three Tc points by the accekeration of output, for the nonlinear quadratic function, according to Lagrange's interpolation, obtain the specific quadratic polynomial function of this acceleration transducer, get final product to get temperature variant zero migration value, select at last specific two temperature point for verification, whether actual value and the calculated value of zero migration is up to specification to recently checking its precision.
Embodiment
Comprise calibration equipment, the description of trimming process and the method for inspection.
Calibration equipment:
Acceleration transducer is measured as high-precision tilt angle and is used, in operating temperature range under its angle precision requires, 3 Tc point environment are set, the requirement that arranges of 3 Tc points is, 1 high-temperature point (mxm. of working temperature), 1 normal temperature point (mean value in operating temperature range), 1 low temperature point (minimum of working temperature).
Trimming process:
Record out respectively zero migration value (Z0, Z1, Z2) and its corresponding temperature (T0, T1, T2) of acceleration transducer at 3 correcting mark fixed temperature points.Gather three groups of following quadratic interpolations of data substitution (lagrange polynomial), the particular constant k in computing function, m, n
L0=Z0/((T0-T1)*(T0-T2))
L1=Z1/((T1-T0)*(T1-T2))
L2=Z2/((T2-T0)*(T2-T1))
Then draw k, m, n:
k=L0*T1*T2+L1*T0*T2+L2*T0*T1
m=-L0*(T1+T2)-L1*(T0+T2)-L2*(T0+T1)
n=L0+L1+L2
With k, m, the nonlinear quadratic interpolation function of n substitution, the specific equation that just can obtain the temperature variant zero migration value of this acceleration transducer in whole operating temperature range is as follows:
Zc=k+m×T+n×T 2
Zc wherein: acceleration zero migration value
T: working temperature
The method of inspection:
For guarantee to proofread and correct accurately, proofread and correct complete after, need to zero point temperature float check point and test apart from the temperature spot of maximum.(1 is the interim temperature value of proofreading and correct between high-temperature point and normal temperature point at 2 verification temperature spots, 1 is normal temperature point and proofreaies and correct interim temperature value between low temperature point) employing checks frock to carry out Zero calibration under Current Temperatures zero point, obtain test value, compare with the result of calculation of the zero migration computing formula of acceleration transducer, see whether meet the acceleration transducer system requirements that zero point, temperature was floated.
The present invention has accurately revised acceleration transducer zero migration, precision and its stability of acceleration have been improved to necessity, especially the angle precision of acceleration transducer in measurement of dip angle is used, be very suitable for high-end equipment as accurate core component technology, industrial automation, surveying instrument, the fields such as automobile.

Claims (3)

1. the non-linear correction method that the zero point of an acceleration transducer, temperature was floated is characterized by and comprises following steps:
1.1 set specific three Tc points;
1.2 calculate the One-place 2-th Order polynomial equation of zero migration value and the temperature of acceleration transducer;
1.3 set specific two temperature point for verification, carry out the actual value of zero migration and calculated value to recently check.
2. the method in claim 1, step 1.1 is characterized as the setting of three temperature spots:
1 high-temperature point: the mxm. of working temperature;
1 normal temperature point: the mean value in operating temperature range;
1 low temperature point: the minimum of working temperature.
3. the method in claim 1, step 1.3 is characterized as the setting of two temperature spots:
First temperature spot: the correction high-temperature point in claim 2 and the interim temperature value between normal temperature point;
Second temperature spot: the interim temperature value between the normal temperature point in claim 2 and correction low temperature point.
CN2013100095083A 2013-01-10 2013-01-10 Nonlinear correction method of zero temperature drift of acceleration sensor Pending CN103105509A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2013100095083A CN103105509A (en) 2013-01-10 2013-01-10 Nonlinear correction method of zero temperature drift of acceleration sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2013100095083A CN103105509A (en) 2013-01-10 2013-01-10 Nonlinear correction method of zero temperature drift of acceleration sensor

Publications (1)

Publication Number Publication Date
CN103105509A true CN103105509A (en) 2013-05-15

Family

ID=48313514

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2013100095083A Pending CN103105509A (en) 2013-01-10 2013-01-10 Nonlinear correction method of zero temperature drift of acceleration sensor

Country Status (1)

Country Link
CN (1) CN103105509A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104237565A (en) * 2014-09-29 2014-12-24 陕西宝成航空仪表有限责任公司 Testing and calibration method of micromechanical accelerator temperature system
CN110542870A (en) * 2019-08-08 2019-12-06 宁波中车时代传感技术有限公司 Compensation circuit for sensitivity and zero temperature drift in Hall sensor integrated chip and compensation method thereof

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201859152U (en) * 2010-06-30 2011-06-08 中山市嘉科电子有限公司 Full-automatic correction system of acceleration sensor
JP2012237682A (en) * 2011-05-12 2012-12-06 Fujikura Ltd Multi-axis sensor output correction device and multi-axis sensor output correction method

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201859152U (en) * 2010-06-30 2011-06-08 中山市嘉科电子有限公司 Full-automatic correction system of acceleration sensor
JP2012237682A (en) * 2011-05-12 2012-12-06 Fujikura Ltd Multi-axis sensor output correction device and multi-axis sensor output correction method

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
刘大健等: "二元函数插值法校正传感器非线性及温度漂移", 《仪表技术》, no. 5, 31 December 2001 (2001-12-31), pages 50 - 51 *
王永祥等: "电子压力计温漂校正算法分析", 《石油仪器》, vol. 19, no. 6, 31 December 2005 (2005-12-31) *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104237565A (en) * 2014-09-29 2014-12-24 陕西宝成航空仪表有限责任公司 Testing and calibration method of micromechanical accelerator temperature system
CN110542870A (en) * 2019-08-08 2019-12-06 宁波中车时代传感技术有限公司 Compensation circuit for sensitivity and zero temperature drift in Hall sensor integrated chip and compensation method thereof
CN110542870B (en) * 2019-08-08 2021-08-24 宁波中车时代传感技术有限公司 Compensating circuit and method for sensitivity and zero temperature drift of Hall sensor integrated chip

Similar Documents

Publication Publication Date Title
CN103278264B (en) A kind of calibration steps of surface source blackbody temperature accuracy and calibration system thereof
CN104374317A (en) Machine tool error calibration method based on multi-point measurement technology of laser tracker
CN206057424U (en) A kind of current measuring device
CN103837300A (en) Pressure sensor calibration method with temperature compensation function
CN103162901A (en) Nonlinear calibrating method for multiple temperature points of pressure sensor
CN108152325B (en) Method for calibrating heat conductivity instrument based on heat shield plate method
CN105387859A (en) Temperature drift error compensation method of MEMS (Micro-electromechanical System) sensor group
CN103823084A (en) Method for calibrating three-axis acceleration sensor
CN106199166A (en) A kind of method and device of current measurement
CN102331266A (en) Multi-parameter gas sensor compensating method
CN104970776B (en) A kind of body temperature detection method and a kind of Dynamic High-accuracy calibration electric body-temperature counter device
CN104422399A (en) Measuring instrument line laser measuring head calibration system and method
CN110595508A (en) Optical fiber gyroscope scale factor error compensation method
CN105371993A (en) Temperature sensor calibration method based on twice application of polynomial fitting
CN103983938B (en) The bearing calibration of electric energy meter small-signal biasing
CN115704697A (en) Temperature calibration compensation method, device, equipment and medium of gyroscope
CN104716904A (en) Crystal oscillator frequency compensation method
CN105143825A (en) Positioning device, method for controlling same, and program
CN103105509A (en) Nonlinear correction method of zero temperature drift of acceleration sensor
CN102654515B (en) Calibration algorithm for z sensitive shaft of three-shaft acceleration transducer
CN103913479A (en) Device for detecting thermal expansion coefficient of grating ruler
CN105571666A (en) Flow compensation method, compensation device and flow sensor
CN113447234A (en) Wind tunnel electronic pressure scanning valve traceability device and traceability method thereof
CN106524887A (en) Hall sensor displacement measurement method and device
CN104142299A (en) Pressure compensation method of infrared methane sensor

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20130515