WO1996001980A1 - Method of and apparatus for calibrating rotary position transducers - Google Patents

Method of and apparatus for calibrating rotary position transducers Download PDF

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Publication number
WO1996001980A1
WO1996001980A1 PCT/GB1995/001371 GB9501371W WO9601980A1 WO 1996001980 A1 WO1996001980 A1 WO 1996001980A1 GB 9501371 W GB9501371 W GB 9501371W WO 9601980 A1 WO9601980 A1 WO 9601980A1
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WO
WIPO (PCT)
Prior art keywords
positions
markers
sensor
measuring
rotational speed
Prior art date
Application number
PCT/GB1995/001371
Other languages
French (fr)
Inventor
Benjamin James Bradshaw
Anthony Claude Wakeman
Original Assignee
Lucas Industries Public Limited Company
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 Lucas Industries Public Limited Company filed Critical Lucas Industries Public Limited Company
Priority to US08/765,561 priority Critical patent/US5864775A/en
Priority to EP95924403A priority patent/EP0769134B1/en
Priority to DE69522943T priority patent/DE69522943T2/en
Publication of WO1996001980A1 publication Critical patent/WO1996001980A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/0097Electrical control of supply of combustible mixture or its constituents using means for generating speed signals
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01DMEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D18/00Testing or calibrating apparatus or arrangements provided for in groups G01D1/00 - G01D15/00
    • G01D18/002Automatic recalibration
    • G01D18/004Continuous recalibration
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P21/00Testing or calibrating of apparatus or devices covered by the preceding groups
    • G01P21/02Testing or calibrating of apparatus or devices covered by the preceding groups of speedometers

Definitions

  • the present invention relates to a method of and apparatus for calibrating rotary position transducers. Such a method and apparatus may be used within an internal combustion engine so as to compensate for systematic errors in measurements of the engine position.
  • US 5 177 681 describes measuring the positions of teeth on a position sensor for an internal combustion engine by running the engine up to a high speed and then cutting the fuel to the engine. It is assumed that the engine will undergo smooth deceleration. The average velocity of the engine is measured over one or more complete revolutions. Further measurements of velocity are made between consecutive teeth and these measurements are compared with the average measurement. Discrepancies in the velocity measurements are attributed to non- uniformities in the positions of the teeth.
  • the first element may be a shaft of an internal combustion engine, such as a crankshaft or a cam shaft.
  • the first element carries a toothed wheel thereon, the wheel being arranged to rotate with the shaft and the teeth being arranged to pass a sensor.
  • the first and second positions are separated by no more than (720/N) degrees where N is the number of cylinders of the internal combustion engine.
  • the third and fourth positions are one intertooth separation apart.
  • the third and fourth positions are substantially symmetrically disposed about a midpoint between the first and second positions.
  • the speed of the engine is monitored so as to ensure that measurements are only taken during periods when the rate of change of acceleration is less than a predetermined threshold.
  • the times, during a single revolution or rotation slightly in excess of a single revolution, at which each one of the teeth passes the sensor are recorded.
  • the measurements of the time may be analysed in conjunction with engine position data so as to determine the relative position of each tooth with respect to a reference tooth and/or the position of each tooth with respect to its neighbours.
  • the engine position data is provided by counting the passage of the teeth past the sensor.
  • a rotary position measurement apparatus comprising an apparatus according to the second aspect of the present invention.
  • the first element carries a toothed wheel having nominally uniformly spaced teeth.
  • the measurements of speed are made by comparing the times at which teeth pass the sensor and assuming that the amount of rotation can be accurately determined since the teeth are substantially uniformly spaced at a predetermined angular separation.
  • the error data may be used to correct speed measurement data so as to increase the accuracy of measurements of speed of the first element.
  • Figure 1 is a schematic diagram of an internal combustion engine having an engine management system incorporating an apparatus constituting an embodiment of the present invention
  • Figure 2 is a timing diagram illustrating operation of an embodiment of the present invention
  • Figure 3 is a flow chart illustrating the steps taken by the microprocessor shown in Figure 1 ;
  • Figure 4 shows a comparison of speed measured using a toothed wheel both with and without applying a correction for errors in the positioning of the teeth together with an indication of the actual speed.
  • the engine 1 shown in Figure 1 has a crankshaft 2 carrying a toothed wheel 3.
  • a sensor 4 is located adjacent the toothed wheel 3 and is arranged to provide an output signal indicating the passage of each tooth.
  • An output of the sensor 4 is provided to an engine management system 5.
  • the engine management system 5 is embodied by a programmable data processor 6 which performs instructions stored in a read only memory (ROM) 7 and is arranged to store data, such as corrected positions of the teeth, into a non-volatile memory, such as an electrically erasable programmable read only memory (EEPROM) 8.
  • ROM read only memory
  • EEPROM electrically erasable programmable read only memory
  • the toothed wheel 3 has sixty regularly spaced teeth formed around the circumference thereof. Thus, each tooth is nominally spaced at six degree intervals. Manufacturing tolerances give rise to position errors of approximately plus or minus 0.1 degrees relative to an arbitrary reference tooth. Thus, for the case in which speed measurements are made over an angular interval of 12 degrees, they are subject to a maximum error of approximately 1.6%. The tooth position errors are systematic errors.
  • the engine management system 5 is arranged to analyse the distribution of teeth around the toothed wheel 3 so as to compensate for tooth position errors.
  • Figure 2 shows an idealised output signal from the sensor 4. Tooth zero is taken as the reference tooth and corresponds to the top dead centre (TDC) position of a predetermined cylinder.
  • Tooth error (N) (30 x ( ⁇ tO/ ⁇ TO)) - 6
  • Figure 3 shows a flow chart for a calibration procedure indicating how the positional error for each tooth of the toothed wheel 3 can be determined.
  • the flow chart commences at step 18. Control is passed to step 19 where a variable COUNT is initialised by being set to zero. The value of COUNT is incremented at step 20. The value of count is tested at step 21. If count is less than 100, control is passed to step 22, otherwise control is passed to step 58 which terminates the procedure. A decision is taken at step 22 as to whether the operating conditions are suitable to perform a measurement of the teeth positions. Suitable conditions may be that the engine speed, and/or load/driver demand are within predetermined values and that the rate of engine acceleration or deceleration is substantially uniform, and ideally zero.
  • the flow chart illustrates the calculations to be undertaken when the engine is running at substantially uniform speed. However, the steps may be modified to account for uniform acceleration and deceleration, in which case the calculation should be performed in terms of revolutions per minute instead of time.
  • control is returned to the start of the step 22. If conditions are suitable, control is passed to step 24 where the times of passage of 65 consecutive teeth are recorded in variables t-2 to t62. The variable tO corresponds to the tooth edge passing the sensor 4 at TDC. Control is then passed to step 26 where a check on the engine operating conditions is again performed. If the conditions are unsuitable, control is passed to step 20, whereas if the conditions are suitable control is passed to step 28. Should suitable conditions not be obtained in 100 attempts (as indicated by the value of COUNT), then the calibration is aborted. The procedure may be reentered at a later time, for instance the next time the engine is started.
  • Steps 28 to 36 calculate the intertooth time period between consecutive teeth.
  • a variable N is set to -2 at step 28.
  • Step 30 calculates the intertooth period ⁇ tN between the Nth and the (N + 1)th teeth.
  • the value of ⁇ tN is stored at step 32, the value of N is incremented at step 34 and step 36 checks to see whether the value of N is greater than 61. Control is returned from step 36 to step 30 if the value of N is less than or equal to 61 , whereas control is passed to step 38 if the value of N is greater than 61.
  • Steps 38 to 46 calculate the time taken for the engine to undergo 30 degrees of revolution substantially centred about the Nth and (N + 1)th teeth.
  • the value of N is reset to zero at step 38.
  • Step 40 calculates a period ⁇ TN for the 30 degrees of revolution occurring between the times at which the T(N + 3)th and the T(N-2)th teeth pass the sensor 4.
  • the value ⁇ TN is stored at step 42, the value of N is incremented at step 44, and step 46 tests the value of N to see whether it exceeds 61. If the value of N is less than or equal to 61 , control is returned to step 40; otherwise control is passed to step 48.
  • Steps 48 to 56 calculate the separation between consecutive teeth.
  • the variable N is reset to zero at step 48.
  • the intertooth separation ⁇ DN between the Nth and the (N + 1)th teeth is calculated at step 50 by multiplying the quotient of ⁇ tN divided by ⁇ TN by 30.
  • the value of ⁇ DN is stored at step 52, the value of N is incremented at step 54, and step 56 examines the value of N to see if it exceeds 59. If N is less than or equal to 59, control is passed to step 50. Otherwise control is passed to step 58 where the procedure is terminated.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Transmission And Conversion Of Sensor Element Output (AREA)

Abstract

A rotary position transducer comprises a sensor (4) cooperating with a toothed wheel (3) which has nominally evenly spaced teeth and which may, for instance, be mounted on the crankshaft (2) of an internal combustion engine (1). The times at which the teeth pass the sensor (4) are stored (24). The time intervals (Δtn) between consecutive teeth are calculated (30), for instance during fuel cut-off operation of the engine. An error in the angular spacing between consecutive teeth is calculated (50) from the time interval between consecutive teeth, a time interval (ΔTN) between further teeth disposed symmetrically about the consecutive teeth, and the nominal angular spacing between the further teeth.

Description

METHOD OF AND APPARATUS FOR CALIBRATING ROTARY POSITION TRANSDUCERS.
The present invention relates to a method of and apparatus for calibrating rotary position transducers. Such a method and apparatus may be used within an internal combustion engine so as to compensate for systematic errors in measurements of the engine position.
US 5 177 681 describes measuring the positions of teeth on a position sensor for an internal combustion engine by running the engine up to a high speed and then cutting the fuel to the engine. It is assumed that the engine will undergo smooth deceleration. The average velocity of the engine is measured over one or more complete revolutions. Further measurements of velocity are made between consecutive teeth and these measurements are compared with the average measurement. Discrepancies in the velocity measurements are attributed to non- uniformities in the positions of the teeth.
It has been found that even though the measurements are taken under fuel cut conditions, a cyclic variation in the engine speed is still present due to cylinder compressions and piston intertial effects. This causes inaccuracies when comparing intertooth velocities with averaged velocities measured over one or more cycles of the engine.
According to a first aspect of the present invention there is provided a method of calibrating an apparatus for measuring rotational movement, the apparatus comprising a plurality of markers arranged to move past a sensor in response to rotary motion of a first element whose position is to be measured, the method comprising measuring a first rotational speed of the first element between first and second positions separated by less than one revolution and corresponding to a first number of markers passing the sensor, measuring a second rotational speed of the first element between third and fourth positions corresponding to a second number of markers passing the sensor, the third and fourth positions lying between the first and second positions, and correcting an estimate of the distance between the third and fourth positions by comparing the first rotational speed measurement with the second rotational speed measurement.
It is thus possible to determine errors in the positioning of the markers and to use the estimation of the errors to correct subsequent measurements of rotary position and/or speed.
The first element may be a shaft of an internal combustion engine, such as a crankshaft or a cam shaft. Advantageously the first element carries a toothed wheel thereon, the wheel being arranged to rotate with the shaft and the teeth being arranged to pass a sensor.
Preferably the first and second positions are separated by no more than (720/N) degrees where N is the number of cylinders of the internal combustion engine. Advantageously the third and fourth positions are one intertooth separation apart.
Preferably the third and fourth positions are substantially symmetrically disposed about a midpoint between the first and second positions. Advantageously the speed of the engine is monitored so as to ensure that measurements are only taken during periods when the rate of change of acceleration is less than a predetermined threshold.
Advantageously the times, during a single revolution or rotation slightly in excess of a single revolution, at which each one of the teeth passes the sensor are recorded. The measurements of the time may be analysed in conjunction with engine position data so as to determine the relative position of each tooth with respect to a reference tooth and/or the position of each tooth with respect to its neighbours.
Preferably the engine position data is provided by counting the passage of the teeth past the sensor.
According to a second aspect of the present invention there is provided an apparatus for calibrating an apparatus for measuring rotational movement, the apparatus for measuring rotational movement comprising a plurality of markers arranged to move past a sensor in response to rotary motion of a first element whose position is to be measured, the apparatus for calibrating position errors comprising speed measuring means for measuring a first rotational speed of the first element between first and second positions separated by less than one revolution and corresponding to a first number of markers passing the sensor, and for measuring a second rotational speed of the first element between third and fourth positions corresponding to a second number of markers passing the sensor, the third and fourth positions lying between the first and second positions, and correcting means for correcting an estimate of the distance between the third and fourth positions by comparing the first rotational speed measurement with the second rotational speed measurement.
According to a third aspect of the present invention there is provided a rotary position measurement apparatus comprising an apparatus according to the second aspect of the present invention.
Preferably the first element carries a toothed wheel having nominally uniformly spaced teeth.
Preferably the measurements of speed are made by comparing the times at which teeth pass the sensor and assuming that the amount of rotation can be accurately determined since the teeth are substantially uniformly spaced at a predetermined angular separation.
It is thus possible to estimate and account for positioning errors in the positions of each one of the teeth of the toothed wheel. The error data may be used to correct speed measurement data so as to increase the accuracy of measurements of speed of the first element.
The present invention will further be described, by way of example, with reference to the accompanying drawings, in which:
Figure 1 is a schematic diagram of an internal combustion engine having an engine management system incorporating an apparatus constituting an embodiment of the present invention;
Figure 2 is a timing diagram illustrating operation of an embodiment of the present invention; Figure 3 is a flow chart illustrating the steps taken by the microprocessor shown in Figure 1 ; and
Figure 4 shows a comparison of speed measured using a toothed wheel both with and without applying a correction for errors in the positioning of the teeth together with an indication of the actual speed.
The engine 1 shown in Figure 1 has a crankshaft 2 carrying a toothed wheel 3. A sensor 4 is located adjacent the toothed wheel 3 and is arranged to provide an output signal indicating the passage of each tooth. An output of the sensor 4 is provided to an engine management system 5. The engine management system 5 is embodied by a programmable data processor 6 which performs instructions stored in a read only memory (ROM) 7 and is arranged to store data, such as corrected positions of the teeth, into a non-volatile memory, such as an electrically erasable programmable read only memory (EEPROM) 8.
The toothed wheel 3 has sixty regularly spaced teeth formed around the circumference thereof. Thus, each tooth is nominally spaced at six degree intervals. Manufacturing tolerances give rise to position errors of approximately plus or minus 0.1 degrees relative to an arbitrary reference tooth. Thus, for the case in which speed measurements are made over an angular interval of 12 degrees, they are subject to a maximum error of approximately 1.6%. The tooth position errors are systematic errors. The engine management system 5 is arranged to analyse the distribution of teeth around the toothed wheel 3 so as to compensate for tooth position errors. Figure 2 shows an idealised output signal from the sensor 4. Tooth zero is taken as the reference tooth and corresponds to the top dead centre (TDC) position of a predetermined cylinder. The microprocessor is arranged to record the time at which the leading edge of each tooth passes the sensor 4. Starting with the reference tooth at time tO, the time at which the leading edge of the first tooth passes the sensor 4 is recorded at t1 , the time at which leading edge of the second tooth passes the sensor 4 is recorded at t2, and so on.
An exemplary calculation of the intertooth error between tooth zero and tooth 1 will now be described with reference to Figure 2. The series of time measurements t-2 to t62 taken over slightly more than one revolution of the crankshaft is analysed so as to determine the time that elapsed between the passage of the leading edges of the zeroth and first teeth. This time, corresponding to t1-t0, is stored in a first value ΔtO. A second value ΔTO corresponding to the average speed of the engine during a period substantially symmetrically disposed about the period t1- tO is calculated for the 30 degrees of engine rotation between t-2 and t3. The tooth position error for tooth zero can then be calculated from:
Tooth error (N) = (30 x (ΔtO/ΔTO)) - 6
Thus, for example, if tl-tO is equal to 1 ,006.4 microseconds, and t3-(t-2) is equal to 4,995.2 microseconds, then the intertooth distance between teeth 0 and 1 is in error by + 0.0442 degrees.
Figure 3 shows a flow chart for a calibration procedure indicating how the positional error for each tooth of the toothed wheel 3 can be determined. The flow chart commences at step 18. Control is passed to step 19 where a variable COUNT is initialised by being set to zero. The value of COUNT is incremented at step 20. The value of count is tested at step 21. If count is less than 100, control is passed to step 22, otherwise control is passed to step 58 which terminates the procedure. A decision is taken at step 22 as to whether the operating conditions are suitable to perform a measurement of the teeth positions. Suitable conditions may be that the engine speed, and/or load/driver demand are within predetermined values and that the rate of engine acceleration or deceleration is substantially uniform, and ideally zero. The flow chart illustrates the calculations to be undertaken when the engine is running at substantially uniform speed. However, the steps may be modified to account for uniform acceleration and deceleration, in which case the calculation should be performed in terms of revolutions per minute instead of time. If the conditions are unsuitable, control is returned to the start of the step 22. If conditions are suitable, control is passed to step 24 where the times of passage of 65 consecutive teeth are recorded in variables t-2 to t62. The variable tO corresponds to the tooth edge passing the sensor 4 at TDC. Control is then passed to step 26 where a check on the engine operating conditions is again performed. If the conditions are unsuitable, control is passed to step 20, whereas if the conditions are suitable control is passed to step 28. Should suitable conditions not be obtained in 100 attempts (as indicated by the value of COUNT), then the calibration is aborted. The procedure may be reentered at a later time, for instance the next time the engine is started.
Steps 28 to 36 calculate the intertooth time period between consecutive teeth. A variable N is set to -2 at step 28. Step 30 calculates the intertooth period ΔtN between the Nth and the (N + 1)th teeth. The value of ΔtN is stored at step 32, the value of N is incremented at step 34 and step 36 checks to see whether the value of N is greater than 61. Control is returned from step 36 to step 30 if the value of N is less than or equal to 61 , whereas control is passed to step 38 if the value of N is greater than 61.
Steps 38 to 46 calculate the time taken for the engine to undergo 30 degrees of revolution substantially centred about the Nth and (N + 1)th teeth. The value of N is reset to zero at step 38. Step 40 calculates a period ΔTN for the 30 degrees of revolution occurring between the times at which the T(N + 3)th and the T(N-2)th teeth pass the sensor 4. The value ΔTN is stored at step 42, the value of N is incremented at step 44, and step 46 tests the value of N to see whether it exceeds 61. If the value of N is less than or equal to 61 , control is returned to step 40; otherwise control is passed to step 48.
Steps 48 to 56 calculate the separation between consecutive teeth. The variable N is reset to zero at step 48. The intertooth separation ΔDN between the Nth and the (N + 1)th teeth is calculated at step 50 by multiplying the quotient of ΔtN divided by ΔTN by 30. The value of ΔDN is stored at step 52, the value of N is incremented at step 54, and step 56 examines the value of N to see if it exceeds 59. If N is less than or equal to 59, control is passed to step 50. Otherwise control is passed to step 58 where the procedure is terminated.
The measured intertooth separations are stored in the memory 8 and are used in engine speed calculations performed by the engine management system 5. Although the position error of each tooth is relatively small, significant improvements in measurement of engine speed can be obtained by making a correction for changes in the intertooth separation between adjacent teeth. Figure 4 shows experimental data in which the broken line 70 shows estimates of the speed based on the assumption that each tooth of the toothed wheel 3 was separated from its neighbours by exactly 6 degrees, line 72 indicates speed data calculated using corrected intertooth separations as calculated by an embodiment of the present invention, and line 74 indicates the actual speed upon which the other data is based. It is noted that the measurements of speed are much improved. The calibration routine, as indicated in Figure 3, need only be performed infrequently and at times such that the cyclic variation of engine speed is small compared to the mean engine speed.
It is thus possible to enhance the accuracy of speed measurements taken using a toothed wheel or a similar rotating element carrying a plurality of markers.

Claims

1. A method of calibrating an apparatus for measuring rotational movement, the apparatus comprising a plurality of markers arranged to move past a sensor in response to rotary motion of an element whose position is to be measured, the method comprising measuring a first rotational speed of the element between first and second positions separated by less than one revolution and corresponding to a first number of markers passing the sensor, measuring a second rotational speed of the element between third and fourth positions corresponding to a second number of markers passing the sensor, the third and fourth positions being between the first and second positions, and correcting an estimate of the distance between the third and fourth positions by comparing the first rotational speed measurement with the second rotational speed measurement.
2. A method as claimed in Claim 1 , in which the markers comprise teeth of a toothed wheel mounted on the element.
3. A method as claimed in Claim 1 , in which the element comprises a rotating part of an internal combustion engine.
4. A method as claimed in Claim 3, in which the first and second positions are separated by no more than 720/N degrees, where N is the number of cylinders of the internal combustion engine.
5. A method as claimed in Claim 3, in which the speed of the engine is monitored and the first and second rotational speeds are measured when the rate of change of acceleration of the engine is less than a predetermined threshold.
6. A method as claimed in Claim 3, in which engine position data are provided by counting the passage of the markers past the sensor.
7. A method as claimed in Claim 1 , in which the third and fourth positions are spaced apart by one intermarker separation.
8. A method as claimed in Claim 1 , in which the third and fourth positions are substantially symmetrically disposed about the midpoint between the first and second positions.
9. A method as claimed in Claim 8, in which the corrected angular distance between the third and fourth positions is calculated as (α-ΔtO)/ΔTO, where α is the angular distance between the first and second positions, ΔTO is the time interval between passage of first and second markers at the first and second positions past the sensor, and ΔtO is the time interval between passage of third and fourth markers at the third and fourth positions past the sensor.
10. A method as claimed in Claim 1 , in which the time at which each of the markers passes the sensor is recorded during a single revolution or during rotation slightly in excess of a single revolution of the element.
1 1. An apparatus for calibrating an apparatus for measuring rotational movement, the apparatus for measuring rotational movement comprising a plurality of markers arranged to move past a sensor in response to rotary motion of an element whose position is to be measured, the calibrating apparatus comprising: speed measuring means for measuring a first rotational speed of the element between first and second positions separated by less than one revolution and corresponding to a first number of markers passing the sensor, and for measuring a second rotational speed of the element between third and fourth positions corresponding to a second number of markers passing the sensor, the third and fourth positions lying between the first and second positions; and correcting means for correcting an estimate of the distance between the third and fourth positions by comparing the first rotational speed with the second rotational speed.
12. A method of determining a position or an error in a position of a first of a plurality of nominally equi-angularly spaced markers on a rotating element, comprising: measuring a first time interval between passages of the first marker and a second of the markers past a reference point; measuring a second time interval between passages of third and fourth of the markers past the reference point, the third and fourth markers being disposed between the first and second markers; and calculating the position or error from the first and second time intervals and the nominal angular spacings between the first and second markers and the third and fourth markers.
PCT/GB1995/001371 1994-07-07 1995-06-12 Method of and apparatus for calibrating rotary position transducers WO1996001980A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US08/765,561 US5864775A (en) 1994-07-07 1995-06-12 Method of and apparatus for calibrating rotary position transducers
EP95924403A EP0769134B1 (en) 1994-07-07 1995-06-12 Method of and apparatus for calibrating rotary position transducers
DE69522943T DE69522943T2 (en) 1994-07-07 1995-06-12 METHOD AND DEVICE FOR CALIBRATING A ROTATIONAL POSITION SENSOR

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB9413677.7 1994-07-07
GB9413677A GB9413677D0 (en) 1994-07-07 1994-07-07 Method of and apparatus for calibrating rotary position transducers

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WO1996001980A1 true WO1996001980A1 (en) 1996-01-25

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US (1) US5864775A (en)
EP (1) EP0769134B1 (en)
DE (1) DE69522943T2 (en)
ES (1) ES2163518T3 (en)
GB (1) GB9413677D0 (en)
WO (1) WO1996001980A1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0902292A2 (en) * 1997-08-14 1999-03-17 Bayerische Motoren Werke Aktiengesellschaft, Patentabteilung AJ-3 Method for correcting the signal of a speed sensor
DE19961504A1 (en) * 1999-12-20 2001-06-28 Bosch Gmbh Robert Rotational speed signal error detection method for anti-slip or anti-lock regulation system of vehicle, involves detecting speed change based on specific condition involving pulse width of falling pulses of measurement signal
GB2555436A (en) * 2016-10-27 2018-05-02 Delphi Int Operations Luxembourg Sarl Method to determine angular pitch of a toothed crank wheel or gear
US20220402507A1 (en) * 2021-06-16 2022-12-22 Bendix Commercial Vehicle Systems Llc Direction detection using a wheel speed sensor and exciter ring

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19721488A1 (en) * 1997-05-23 1998-11-26 Itt Mfg Enterprises Inc Method for compensating for deviations in a wheel speed sensor
DE19733958A1 (en) * 1997-08-06 1999-02-11 Bosch Gmbh Robert Method and device for correcting tolerances of a sensor wheel
US6125690A (en) * 1997-09-12 2000-10-03 Shell Oil Company Device for testing of diesel fuel
AT4801U3 (en) * 2001-08-22 2002-06-25 Avl List Gmbh METHOD AND DEVICE FOR PROVIDING A CRANK ANGLE-BASED SIGNAL PROCESS
ATE376620T1 (en) * 2002-01-24 2007-11-15 Fraunhofer Ges Forschung METHOD FOR DETERMINING AND COMPENSATING GEOMETRIC ERRORS OF A ROTARY ENCODER WHEEL
DE10241893A1 (en) * 2002-09-10 2004-03-11 Robert Bosch Gmbh Combustion engine angular position or velocity determination system in which incremental encoder wheel markings are compensated based on comparison of their positions and corresponding pressure measurements with ideal values
EP1460387A1 (en) * 2003-03-21 2004-09-22 AFT Atlas Fahrzeugtechnik GmbH Method for increasing the measuring accuracy for a limited path in a measuring system
DE102004044248B4 (en) * 2004-09-10 2016-05-12 Volkswagen Aktiengesellschaft Method for determining the dead center of a piston of an internal combustion engine
EP2824303B1 (en) * 2005-08-23 2017-03-22 Denso Corporation Rotation angle sensing device
JP4508036B2 (en) * 2005-08-23 2010-07-21 株式会社デンソー Rotation angle detector
JP4339347B2 (en) * 2006-10-30 2009-10-07 本田技研工業株式会社 Crank angular velocity detection device for internal combustion engine
US7400993B2 (en) * 2006-10-31 2008-07-15 General Electric Company Method and system for accuracy of speed and acceleration measurements on rotating machinery with a speed wheel
CN101266141B (en) * 2007-03-13 2010-05-19 同济大学 Signal wheel tooth phase angle automatic detection device
US7610800B2 (en) * 2007-08-29 2009-11-03 Gm Global Technology Operations, Inc. Method and system for collecting crankshaft position data
CN107525949A (en) * 2017-08-22 2017-12-29 商丘师范学院 2 Linear-speed measuring instrument calibrating installations and calibration method

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2198241A (en) * 1986-11-07 1988-06-08 Diesel Kiki Co Spacing time measuring apparatus and method for revolution sensor
US5170365A (en) * 1985-12-12 1992-12-08 General Electric Company Propeller speed and phase sensor

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0442687B1 (en) * 1990-02-14 1998-04-15 Lucas Industries Public Limited Company Method of and apparatus for detecting misfire
US5117681A (en) * 1990-10-01 1992-06-02 Ford Motor Company Correction of systematic position-sensing errors in internal combustion engines

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5170365A (en) * 1985-12-12 1992-12-08 General Electric Company Propeller speed and phase sensor
GB2198241A (en) * 1986-11-07 1988-06-08 Diesel Kiki Co Spacing time measuring apparatus and method for revolution sensor

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0902292A2 (en) * 1997-08-14 1999-03-17 Bayerische Motoren Werke Aktiengesellschaft, Patentabteilung AJ-3 Method for correcting the signal of a speed sensor
EP0902292A3 (en) * 1997-08-14 1999-08-11 Bayerische Motoren Werke Aktiengesellschaft, Patentabteilung AJ-3 Method for correcting the signal of a speed sensor
DE19735313B4 (en) * 1997-08-14 2008-02-07 Bayerische Motoren Werke Ag Method for determining speed-independent frequencies of a useful signal component
DE19961504A1 (en) * 1999-12-20 2001-06-28 Bosch Gmbh Robert Rotational speed signal error detection method for anti-slip or anti-lock regulation system of vehicle, involves detecting speed change based on specific condition involving pulse width of falling pulses of measurement signal
GB2555436A (en) * 2016-10-27 2018-05-02 Delphi Int Operations Luxembourg Sarl Method to determine angular pitch of a toothed crank wheel or gear
GB2555436B (en) * 2016-10-27 2019-05-08 Delphi Tech Ip Ltd Method to determine tooth error in period of one or more teeth of a rotating toothed wheel
US20220402507A1 (en) * 2021-06-16 2022-12-22 Bendix Commercial Vehicle Systems Llc Direction detection using a wheel speed sensor and exciter ring
US11814055B2 (en) * 2021-06-16 2023-11-14 Bendix Commercial Vehicle Systems Llc Direction detection using a wheel speed sensor and exciter ring

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EP0769134A1 (en) 1997-04-23
GB9413677D0 (en) 1994-08-24
US5864775A (en) 1999-01-26
EP0769134B1 (en) 2001-09-26
ES2163518T3 (en) 2002-02-01
DE69522943D1 (en) 2001-10-31
DE69522943T2 (en) 2002-04-11

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