Power and temperature independent magnetic position sensor for a rotor

• US 4,746,859 A
• Filed: 12/22/1986
• Issued: 05/24/1988
• Est. Priority Date: 12/22/1986
• Status: Expired due to Fees

• Current Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Malik, Khalid
• Primary Examiner(s): Strecker, Gerard R.
• Application Number:
  US06/944,958
• Time in Patent Office: 519 Days
• Field of Search: 324/160, 324/163-166, 324/173, 324/174, 324/207, 324/208, 324/225, 123/414, 123/617, 318/653, 340/672, 340/686, 340/870.32, 340/870.33
• US Class Current: 324/207.12
• CPC Class Codes: G01D 2205/777 Whorl-shaped profiles
• CPC Class Codes: G01D 3/032 affecting incoming signal, e.g. by averaging; gating undesired signals
• CPC Class Codes: G01D 5/142 using Hall-effect devices measuring magnetic variables using Hall-effect or other galvanomagnetic devices G01R33/06
• CPC Class Codes: G01D 5/145 influenced by the relative movement between the Hall device and magnetic fields see G01R33/06

Abstract

In order to optimize the electrical performance in motors in terms of improved efficiency, power factor, and reduced current, a power and temperature magnetic position sensor for a rotor utilizes first and second magnetic sensing devices for accurately determining the angular position of the rotor. The first and second magnetic sensing devices include at least one target operatively associated with the rotor so as to rotate therewith, a first sensor disposed at a variable distance from the target dependent upon the angular position of the rotor to define a first air gap therebetween, and a second sensor disposed at a variable distance from the target dependent upon the angular position of the rotor to define a second air gap therebetween. The first and second sensors cooperate with the target to detect magnetic field intensity in the first and second air gaps, respectively, and produce output signals indicative of the magnetic field intensity which, at any point in time, is dependent upon the length of the first and second air gaps as determined by the position of the first and second sensors relative to the target at that point in time. The first and second sensors are also operatively associated with a compensating circuit which includes an electronic adder for adding the output signals produced by the first and second sensors, an electronic subtractor for subtracting the output signals produced by the first and second sensors, and an electronic divider for dividing the added output signals by the subtracted output signals. Since the output signals change in magnitude in a manner indicative of the magnetic field intensity by reason of changes in the length of the first and second air gaps, the electronic divider produces a numerical value representative of the accurate angular position of the rotor which is independent of power supply and temperature variations.

Claims

1. A power and temperature independent magnetic position sensor for a rotor, comprising:

first and second magnetic sensing means for accurately determining the angular position of said rotor, said first and second magnetic sensing means including at least one disk shaped target means having a continuously increasing radial dimension and being fixedly mounted in operatively associated relation to said rotor so as to rotate therewith, first sensor means fixedly mounted in spaced relation to the periphery of said target means and disposed at a variable distance from said target means dependent upon the angular position of said rotor to define a first air gap therebetween, and second sensor means fixedly mounted in spaced relation to the periphery of said target means and disposed at a variable distance from said target means dependent upon the angular position of said rotor to define a second air gap therebetween, said first and second sensor means cooperating with said target means to detect magnetic field intensity in said first and second air gaps, respectively;

said first and second sensor means producing output signals indicative of said magnetic field intensity in said first and second air gaps, said magnetic field intensity in said first and second air gaps at any point in time being dependent upon the length of said first and second air gaps as determined by the position of said first and second sensor means relative to said target means at that point in time, said output signals changing in magnitude in a manner indicative of said magnetic field intensity by reason of changes in the length of said first and second air gaps; and

compensating means operatively associated with said first and second sensor means, said compensating means including means for adding said output signals produced by said first and second sensor means, means for subtracting said output signals produced by said first and second sensor means, and means for dividing said added output signals by said subtracted output signals to produce a numerical value representative of the accurate angular position of said rotor, said numerical value being independent of power supply and temperature variations.

2. The position sensor as defined by claim 1 wherein said first and second sensor means comprise first and second magnetic sensors mounted in fixed positions relative to said target means.

3. The position sensor as defined by claim 2 wherein said target means includes first and second wheels having generally smooth outer surfaces about the peripheries thereof, said first and second wheels comprising first and second circular disks having continuously increasing radial dimensions, said first and second circular disks having radial offsets on said outer surfaces at common points of maximum and minimum radial dimension.

4. The position sensor as defined by claim 3 wherein said first and second magnetic sensors are disposed in respective common planes with said first and second circular disks, said first and second magnetic sensors being disposed in confronting but radially spaced relation to said outer surfaces of said first and second circular disks, said first magnetic sensor always being spaced from said first circular disk by a distance less than the distance said second magnetic sensor is spaced from said second circular disk.

5. The position sensor as defined by claim 2 wherein said target means includes a single wheel having a generally smooth outer surface about the periphery thereof, said wheel comprising a circular disk having a continuously increasing radial dimension, said circular disk having a radial offset on said outer surface at a common point of maximum and minimum radial dimension.

6. The position sensor as defined by claim 5 wherein said first and second magnetic sensors are disposed in a common plane with said circular disk, said first and second magnetic sensors being disposed in confronting but radially spaced relation to said outer surface of said circular disk and in angularly spaced relation to one another, said first magnetic sensor always being spaced from said circular disk by a distance different from the distance said second magnetic sensor is spaced from said circular disk.

7. A power and temperature independent magnetic position sensor for a rotor, comprising:

first and second magnetic sensing means for accurately determining the angular position of said rotor, said first and second magnetic sensing means including first and second disk shaped target means each having a continuously increasing radial dimension and each being fixedly mounted in operatively associated relation to said rotor so as to rotate therewith, first sensor means fixedly mounted in spaced relation to the periphery of said first target means and disposed at a variable distance from said first target means dependent upon the angular position of said rotor to define a first linearly variable air gap therebetween, and second sensor means fixedly mounted in spaced relation to the periphery of said second target means and disposed at a variable distance from said second target means dependent upon the angular position of said rotor to define a second linearly variable air gap therebetween, said first and second sensor means cooperating with said first and second target means to detect magnetic field intensity in said first and second air gaps, respectively;

said first and second sensor means producing output signals indicative of said magnetic field intensity in said first and second air gaps, said magnetic field intensity in said first and second air gaps at any point in time being dependent upon the length of said first and second air gaps as determined by the position of said first and second sensor means relative to said first and second target means at that point in time, said output signals changing in magnitude in a manner indicative of said magnetic field intensity by reason of changes in the length of said first and second air gaps;

the length of said first air gap always being less than the length of said second air gap so that the magnitude of said output signal produced by said first sensor means is always greater than the magnitude of said output signal produced by said second sensor means; and

compensating means operatively associated with said first and second sensor means, said compensating means including means for adding said output signals produced by said first and second sensor means, means for subtracting said output signals produced by said first and second sensor means, and means for dividing said added output signals by said subtracted output signals to produce a numerical value representative of said accurate angular position of said rotor, said numerical value being independent of power supply and temperature variations.

8. The position sensor as defined by claim 7 wherein said first and second target means include first and second wheels having generally smooth outer surfaces about the peripheries thereof, said first and second wheels comprising first and second circular disks having continuously increasing radial dimensions, said first and second circular disks having radial offsets on said outer surfaces at common points of maximum and minimum radial dimension.

9. The position sensor as defined by claim 8 wherein said first and second magnetic sensors are disposed in respective common planes with said first and second circular disks, said first and second magnetic sensors being disposed in confronting but radially spaced relation to said outer surfaces of said first and second circular disks, said first magnetic sensor always being spaced from said first circular disk by a distance less than the distance said second magnetic sensor is spaced from said second circular disk.

10. The position sensor as defined by claim 7 wherein said compensating means comprises an electrical circuit, said adding means includes an electronic adder in said electrical circuit, said subtracting means includes an electronic subtractor in said electrical circuit, and said dividing means includes an electronic divider in said electrical circuit.

11. The position sensor as defined by claim 10 including means for amplifying said output signals produced by said first and second sensor means, said amplifying means including a first amplifier for receiving said output signal produced by said first sensor means and a second amplifier for receiving said output signal produced by said second sensor means, said first and second amplifiers being disposed intermediate said electronic adder and subtractor and said first and second sensor means.

12. The position sensor as defined by claim 11 including means for multiplying said added outut signals and said subtracted output signals, said multiplying means including a first multiplier for receiving said added output signals from said electronic adder and a second multiplier for receiving said subtracted output signals from said electronic subtractor, said first and second multipliers being disposed intermediate said electronic divider and said electronic adder and subtractor.

13. The position sensor as defined by claim 12 wherein said output signal received by said first amplifier is amplified by a gain of 10, said output signal received by said second amplifier is amplified by a gain of 10, said added output signals received by said first multiplier are scaled by a factor of 0.2, and said subtracted output signals received by said second multiplier are scaled by a factor of 1.0.

14. The position sensor as defined by claim 13 wherein said electronic divider also multiplies said numerical value produced by dividing said amplified and multiplied output signals by said amplified and multiplied subtracted output signals by a reference voltage of 10 volts.

15. A power and temperature independent magnetic position sensor for a rotor comprising:

first and second magnetic sensing means for accurately determining the angular position of said rotor, said first and second magnetic sensing means including single disk shaped target means having a continuously increasing radial dimension and being fixedly mounted in operatively associated relation to said rotor so as to rotate therewith, first sensor means fixedly mounted in spaced relation to the periphery of said target means in a manner so as to be disposed at a variable distance from said target means dependent upon the angular position of said rotor to define a first linearly variable air gap therebetween, and second sensor means fixedly mounted in spaced relation to the periphery of said target means in a manner so as to be disposed at a variable distance from said target means dependent upon the angular position of said rotor to define a second linearly variable air gap therebetween, said first and second sensor means cooperating with said target means to detect magnetic field intensity in said first and second air gaps, respectively;

said first and second sensor means producing output signals indicative of said magnetic field intensity in said first and second air gaps, said magnetic field intensity in said first and second air gaps at any point in time being dependent upon the length of said first and second air gaps as determined by the position of said first and second sensor means relative to said target means at that point in time, said output signals changing in magnitude in a manner indicative of said magnetic field intensity by reason of changes in the length of said first and second air gaps;

the length of said first air gap normally being less than the length of said second air gap so that the magnitude of said output signal produced by said first sensor means is normally greater than the magnitude of said output signal produced by said second sensor means; and

p1 compensating means operatively associated with said first and second sensor means, said compensating means including means for adding said output signals produced by said first and second sensor means, means for subtracting said output signals produced by said first and second sensor means, and means for dividing said output signals by said subtracted output signals to produce a numerical value representative of the accurate angular position of said rotor, said numerical value being independent of power supply and temperature variations.

16. The position sensor as defined by claim 15 wherein said first and second sensor means comprise first and second magnetic sensors mounted in fixed positions relative to said target means.

17. The position sensor as defined by claim 16 wherein said target means includes a single wheel having a generally smooth outer surface about the periphery thereof, said wheel comprising a circular disk having a continuously increasing radial dimension, said circular disk having a radial offset on said outer surface at a common point of maximum and minimum radial dimension.

18. The position sensor as defined by claim 17 wherein said first and second magnetic sensors are disposed in a common plane with said circular disk, said first and second magnetic sensors being disposed in confronting but radially spaced relation to said outer surface of said circular disk and in angularly spaced relation to one another, said first magnetic sensor always being spaced from said circular disk by a distance different from the distance said second magnetic sensor is spaced from said circular disk.

19. The position sensor as defined by claim 15 wherein said compensating means includes an electrical circuit, said adding means includes an electronic adder in said electrical circuit, said subtracting means includes an electronic subtractor in said electrical circuit, and said dividing means includes an electronic divider in said electrical circuit.

20. The position sensor as defined by claim 19 including means for amplifying said output signals produced by said first and second sensor means, said amplifying means including a first amplifier for receiving said output signal produced by said first sensor means and a second amplifier for receiving said output signal produced by said second means, said first and second amplifiers being disposed intermediate said electronic adder and subtractor and said first and second sensor means.

21. The position sensor as defined by claim 20 including switch means comprising a first analog switch and a second analog switch, said first analog switch being disposed intermediate said electronic adder and said electronic divider and receiving said added output signals directly from said electronic adder as a first input to said first analog switch and indirectly from said electronic adder after said added output signals have been multiplied by a first multiplier as a second input to said first analog switch, said second analog switch being disposed intermediate said electronic subtractor and said electronic divider and receiving said subtracted output signals directly from said electronic subtractor as a first input to said second analog switch and indirectly from said electronic subtractor after said subtracted output signals have been multiplied by a second multiplier as a second input to said second analog switch, said first and second multipliers being disposed intermediate said first and second analog switches and said electronic adder and subtractor.

22. The position sensor as defined by claim 21 including a comparator adapted to receive said subtractor output signals directly from said electronic subtractor, said comparator being operatively associated with said first and second analog switches to cause either said first inputs or second inputs to said first and second analog switches to be received by said electronic divider, said comparator causing said second inputs to be received by said electronic divider when said subtracted output signals is a negative value.

23. The position sensor as defined by claim 22 wherein said output signal received by said first amplifier is amplified by a gain of 10, said output signal received by said second amplifier is amplified by a gain of 10, said added output signals received by said first multiplier are scaled by a factor of G1, and said subtracted output signals received by said second multiplier are scaled by a factor of -G2.

24. The position sensor as defined by claim 23 wherein said comparator also multiplies said numerical value produced by dividing said added output signals by said subtracted output signal by a reference voltage of 10 volts.

25. In a compensating circuit for accurately determining the angular position of a rotor with a magnetic position sensor independent of power supply and temperature variations, said magnetic position sensor including first and second magnetic sensing means for accurately determining the annular position of said rotor, said first and second magnetic sensing means including at least one disk shaped target means having a continuously increasing radial dimension and being fixedly mounted in operatively associated relation to said rotor so as to rotate therewith, first sensor means fixedly mounted in spaced relation to the periphery of said target means and disposed at a variable distance from said target means dependent upon the angular position of said rotor to define a first air gap therebetween, and second sensor means fixedly mounted in spaced relation to the periphery of said target means and disposed at a variable distance from said target means dependent upon the angular position of said rotor to define a second air gap therebetween, said first and second sensor means cooperating with said target means to detect magnetic field intensity in said first and second air gaps, the improvement comprising:

means for adding output signals from said first and second sensor means of said magnetic position sensor, said output signals being indicative of said magnetic field intensity in said first and second air gaps and said adding means being operatively associated with said first and second sensor means;

means for subtracting said output signals from said first and second sensor means of said magnetic position sensor, said output signals changing in magnitude with changes in the length of said first and second air gaps and said subtracting means being operatively associated with said first and second sensor means; and

means operatively associated with said adding and subtracting means for dividing said added output signals by said subtracted output signals to produce a numerical value representative of the accurate angular position of said rotor;

said numerical value being independent of power supply and temperature variations.

26. The compensating circuit as defined by claim 25 wherein said adding means includes an electronic adder, said subtracting means includes an electronic subtractor, and said dividing means includes an electronic divider.

27. The compensating circuit as defined by claim 26 including a first amplifier for amplifying said output signal from said first sensor means before said output signals are added by said electronic adder and subtracted by said electronic subtractor and a second amplifier for amplifying said output signal from said second sensor means before said output signals are added by said electronic adder and subtracted by said electronic subtractor.

28. The compensating circuit as defined by claim 27 including means for multiplying said added output signals and said subtracted output signals, said multiplying means including a first multiplier for receiving said added output signals from said electronic adder and a second multiplier for receiving said subtracted output signals from said electronic subtractor, said first and second multipliers being disposed intermediate said electronic divider and said electronic adder and subtractor.

29. The compensating circuit as defined by claim 28 wherein said output signal received by said first amplifier is amplified by a gain of 10, said output signal received by said second amplifier is amplified by a gain of 10, said added output signals received by said first multiplier are scaled by a factor of 0.2, and said subtracted output signals received by said second multiplier are scaled by a factor of 1.0.

30. The compensating circuit as defined by claim 29 wherein said electronic divider also multiplies said numerical value produced by dividing said amplified and multiplied added output signals by said amplified and multiplied subtracted output signals by a reference voltage of 10 volts.

31. The compensating circuit as defined by claim 27 including switch means comprising a first analog switch and a second analog switch, said first analog switch being disposed intermediate said electronic adder and said electronic divider and receiving said added output signals directly from said electronic adder as a first input to said first analog switch and indirectly from said electronic adder after said added output signals have been multiplied by a first multiplier as a second input to said first analog switch, said second analog switch being disposed intermediate said electronic subtractor and said electronic divider and receiving said subtracted output signals directly from said electronic subtractor as a first input to said second analog switch and indirectly from said electronic subtractor after said subtracted output signals have been multiplied by a second multiplier as a second input to said second analog switch, said first and second multipliers being disposed intermediate said first and second analog switches and said electronic adder and subtractor.

32. The compensating circuit as defined by claim 31 including a comparator adapted to receive said subtracted output signals directly from said electronic subtractor, said comparator being operatively associated with said first and second analog switches to cause either said first inputs or said second inputs to said first and second analog switches to be received by said electronic divider, said comparator causing said second inputs to be received by said electronic divider when said subtracted output signals is a negative value.

33. The compensating circuit as defined by claim 32 wherein said output signal received by said first amplifier is amplified by a gain of 10, said output signal received by said second amplifier is amplified by a gain of 10, said added output signals received by said first multiplier are scaled by a factor of G1, and said subtracted output signals received by said second multiplier are scaled by a factor of -G2.

34. The compensating circuit as defined by claim 33 wherein said comparator also multiplies said numeric value produced by dividing said added output signals by said subtracted output signals by a reference voltage of 10 volts.

35. A method for accurately determining the angular position of a rotor with a magnetic position sensor, said magnetic position sensor including first and second ensor means disposed relative to target means operatively associated with said rotor to rotate therewith to define first and second air gaps therebetween, respectively, the angular position being determined independent of power supply and temperature variations, comprising the steps of:

adding rotor angle-related linearly variable output signals from said first and second sensor means of said magnetic position sensor, said output signals being indicative of said magnetic field intensity in said first and second air gaps;

subtracting said rotor angle-related linearly variable output signals from said first and second sensor means of said magnetic position sensor, said output signals changing in magnitude with changes in the length of said first and second air gaps;

said output signals being dependent upon the angular position of said rotor at any point in time; and

dividing said added output signals by said subtracted output signals to produce a numerical value representative of the accurate angular position of said rotor;

said numerical value being independent of power supply and temperature variations.

36. The method of accurately determining the angular position of a rotor as defined by claim 35 wherein said output signal from said first sensor means is amplified before said output signals are added and subtracted and said output signal from said second sensor means is amplified before said output signals are added and subtracted.

37. The method for accurately determining the angular position of a rotor as defined by claim 36 wherein said added output signals and said subtracted output signals are multiplied before said added output signals are divided by said subtracted output signals.

38. The method for determining the angular position of a rotor as defined by claim 37 wherein said output signal from said first sensor means is amplified by a gain of 10, said output signal from said second sensor means is amplified by a gain of 10, said added output signals are scaled by a factor of 0.2, and said subtracted output signals are scaled by a factor of 1.0.

39. The method of accurately determining the angular position of a rotor as defined by claim 38 wherein said numerical value produced by dividing said amplified and multiplied output signals by said amplified and multiplied subtracted output signals is further multiplied by a reference voltage of 10 volts.

40. The method for accurately determining the angular position of a rotor as defined by claim 36 including the step of providing a first analog switch for receiving said added output signals directly as a first input to said first analog switch and indirectly after said added output signals have been multiplied as a second input to said first analog switch, and including the step of providing a second analog switch for receiving said subtracted output signals directly as a first input to said second analog switch and indirectly after said subtracted output signals have been multiplied as a second input to said second analog switch.

41. The method for determining the angular position of a rotor as defined by claim 40 including the step of providing a comparator adapted to directly receive the subtracted output signals, said comparator being operatively associated with said first and second analog switches to cause either said first inputs or said second inputs to said first and second analog switches to be divided to produce said numerical value representative of the accurate angular position of said rotor, said comparator causing said second inputs to be divided when said subtracted output signals is a negative value.

42. The method for accurately determining the angular position of a rotor as defined by claim 41 wherein said output signal from said first sensor means is amplified by a gain of 10, said output signal from said second sensor means is amplified by a gain of 10, said added output signals are scaled by a factor of G1, and said subtracted output signals are scaled by a factor of -G2.

43. The method for accurately determining the angular position of a rotor as defined by claim 42 wherein said numerical value produced by dividing said added output signals by said subtracted output signals is multiplied by a reference voltage of 10 volts.