Fine resolution motor control

• US 8,058,833 B2
• Filed: 10/29/2008
• Issued: 11/15/2011
• Est. Priority Date: 10/29/2008
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Wilkens, Dean
• Primary Examiner(s): Benson; Walter
• Assistant Examiner(s): Agared; Gabriel
• Application Number:
  US12/260,763
• Publication Number:
  US 20100102765A1
• Time in Patent Office: 1,112 Days
• Field of Search: 318/400.04, 318/632, 318/701, 318/738, 318/605, 341/116
• US Class Current: 318/632
• CPC Class Codes: H02P 6/16 Circuit arrangements for detecting position

Abstract

Methods and apparatus are provided for deriving precision position and rate information for motors using relatively low precision analog sensors, and for implementing compensation techniques that overcome inherent sensor errors and rotor magnet flux tolerances.

Claims

1. A method of generating a motor control signal for a motor having a rotor that rotates at a rotational rate, the method comprising the steps of:

generating first, second, and third sinusoidal signals, each sinusoidal signal being 120-degrees out of phase with the other sinusoidal signals;

differentiating the first, second, and third sinusoidal signals to obtain first, second, and third cosine signals, respectively;

subtracting the first sinusoidal signal from the third sinusoidal signal to obtain a first sinusoidal difference signal;

subtracting the second sinusoidal signal from the first sinusoidal signal to obtain a second sinusoidal difference signal;

subtracting the third sinusoidal signal from the second sinusoidal signal to obtain a third sinusoidal difference signal;

multiplying the first sinusoidal difference signal and the second cosine signal to obtain a first product signal;

multiplying the second sinusoidal difference signal and the third cosine signal to obtain a second product signal;

multiplying the third sinusoidal difference signal and the first cosine signal to obtain a third product signal;

summing the first, second, and third product signals to obtain a summation signal; and

multiplying the summation signal by a constant to obtain a rate signal that is proportional to the rotational rate of the rotor.

2. The method of claim 1, wherein the constant is selected from the group consisting of

3. The method of claim 1, wherein the first, second, and third sinusoidal signals are generated by first, second, and third Hall-effect sensors.

4. The method of claim 1, wherein the rate signal is a first rate signal and wherein the method further comprises:

obtaining a second rate signal that is proportional to the rotational rate of the rotor, the second rate signal 180-degrees out of phase with the first rate signal.

5. The method of claim 4, wherein the step of obtaining the second rate signal comprises:

generating fourth, fifth, and sixth sinusoidal signals 120-degrees out of phase with each other, the fourth, fifth, and sixth sinusoidal signals 180-degrees out of phase with the first, second, and third sinusoidal signals, respectively;

differentiating the fourth, fifth, and sixth sinusoidal signals to obtain fourth, fifth, and sixth cosine signals, respectively;

subtracting the fourth sinusoidal signal from the sixth sinusoidal signal to obtain a fourth sinusoidal difference signal;

subtracting the fifth sinusoidal signal from the fourth sinusoidal signal to obtain a fifth sinusoidal difference signal;

subtracting the sixth sinusoidal signal from the fifth sinusoidal signal to obtain a sixth sinusoidal difference signal;

multiplying the fourth sinusoidal difference signal and the fifth cosine signal to obtain a fourth product signal;

multiplying the fifth sinusoidal difference signal and the sixth cosine signal to obtain a fifth product signal;

multiplying the sixth sinusoidal difference signal and the fourth cosine signal to obtain a sixth product signal;

summing the fourth, fifth, and sixth product signals to obtain a second summation signal; and

multiplying the second summation signal by the constant to obtain the second rate signal.

6. The method of claim 5, further comprising:

adding the first and second rate signals to obtain compensated rate signal that is proportional to the rotational rate of the rotor.

7. The method of claim 1, further comprising:

obtaining a position signal representative of an instantaneous position of the rotor;

supplying the position signal and the rate signal to a complementary filter to obtain a filtered position signal and a filtered rate signal.

8. The method of claim 7, further comprising:

subtracting the filtered position signal from the position signal to obtain a position error signal;

applying a predetermined gain to the position error signal to obtain an adjusted position error signal;

integrating the position error signal to obtain a rate adjustment signal;

multiplying the rate signal and the rate adjustment signal to obtain an adjusted rate signal;

summing the adjusted rate signal and the adjusted position error signal to obtain the filtered rate signal; and

integrating the filtered rate signal to obtain the filtered position signal.

9. A motor controller, comprising:

first, second, and third sensor means for generating first, second, and third sinusoidal signals, respectively, each sinusoidal signal being 120-degrees out of phase with the other sinusoidal signals;

first, second, and third differentiation means for differentiating the first, second, and third sinusoidal signals, respectively, to generate first, second, and third cosine signals, respectively;

first subtraction means for subtracting the first sinusoidal signal from the third sinusoidal signal to generate a first sinusoidal difference signal;

second subtraction means for subtracting the second sinusoidal signal from the first sinusoidal signal to generate a second sinusoidal difference signal;

third subtraction means for subtracting the third sinusoidal signal from the second sinusoidal signal to generate a third sinusoidal difference signal;

first multiplication means for multiplying the first sinusoidal difference signal and the second cosine signal to generate a first product signal;

second multiplication means for multiplying the second sinusoidal difference signal and the third cosine signal to generate a second product signal;

third multiplication means for multiplying the third sinusoidal difference signal and the first cosine signal to generate a third product signal;

summing means for summing the first, second, and third product signals to generate a summation signal; and

fourth multiplication means for multiplying the summation signal by a constant to generate a rate signal that is proportional to the rotational rate of the rotor.

10. The controller of claim 9, wherein the constant is selected from the group consisting of

11. The controller of claim 9, wherein the rate signal is a first rate signal and wherein the method further comprises:

fourth, fifth, and sixth sensor means for generating fourth, fifth, and sixth sinusoidal signals 120-degrees out of phase with each other, the fourth, fifth, and sixth sinusoidal signals 180-degrees out of phase with the first, second, and third sinusoidal signals, respectively;

fourth, fifth, and sixth differentiation means for differentiating the fourth, fifth, and sixth sinusoidal signals to obtain fourth, fifth, and sixth cosine signals, respectively;

fourth subtraction means for subtracting the fourth sinusoidal signal from the sixth sinusoidal signal to obtain a fourth sinusoidal difference signal;

fifth subtraction means for subtracting the fifth sinusoidal signal from the fourth sinusoidal signal to obtain a fifth sinusoidal difference signal;

sixth subtraction means for subtracting the sixth sinusoidal signal from the fifth sinusoidal signal to obtain a sixth sinusoidal difference signal;

fifth multiplication means for multiplying the fourth sinusoidal difference signal and the fifth cosine signal to obtain a fourth product signal;

sixth multiplication means for multiplying the fifth sinusoidal difference signal and the sixth cosine signal to obtain a fifth product signal;

seventh multiplication means for multiplying the sixth sinusoidal difference signal and the fourth cosine signal to obtain a sixth product signal;

second summing means for summing the fourth, fifth, and sixth product signals to obtain a second summation signal; and

eighth multiplication means for multiplying the second summation signal by the constant to obtain the second rate signal.

12. The controller of claim 11, further comprising:

third summing means for summing the first and second rate signals to obtain compensated rate signal that is proportional to the rotational rate of the rotor.

13. The controller of claim 9, further comprising:

rotor position determination means for generating a position signal representative of an instantaneous position of the rotor; and

a complementary filter coupled to receive the position signal and the rate signal and configured to supply a filtered position signal and a filtered rate signal.

14. The controller of claim 13, further comprising:

subtraction means for subtracting the filtered position signal from the position signal to supply a position error signal;

gain adjustment means for applying a predetermined gain to the position error signal to supply an adjusted position error signal;

first integration means for integrating the position error signal and supplying a rate adjustment signal;

multiplication means for multiplying the rate signal and the rate adjustment signal to generate an adjusted rate signal;

summing means for summing the adjusted rate signal and the adjusted position error signal to generate the filtered rate signal; and

second integration means for integrating the filtered rate signal to obtain the filtered position signal.

15. A motor control system, comprising:

a motor including a stator and a rotationally mounted rotor, the rotor configured, upon the stator being controllably energized, to rotate to a rotational position at a rotational rate;

first, second, and third sensors evenly spaced about the rotor to sense the rotational position thereof and supply first, second, and third sinusoidal sensor signals, respectively, each sinusoidal sensor signal being 120-degrees out of phase with the other sinusoidal sensor signals; and

a motor controller coupled to receive each of the sinusoidal sensor signals and configured to controllably energize the stator from a power source, the motor controller comprising;

first, second, and third differentiation means for differentiating the first, second, and third sinusoidal signals, respectively, to generate first, second, and third cosine signals, respectively;

first subtraction means for subtracting the first sinusoidal signal from the third sinusoidal signal to generate a first sinusoidal difference signal;

second subtraction means for subtracting the second sinusoidal signal from the first sinusoidal signal to generate a second sinusoidal difference signal;

third subtraction means for subtracting the third sinusoidal signal from the second sinusoidal signal to generate a third sinusoidal difference signal;

first multiplication means for multiplying the first sinusoidal difference signal and the second cosine signal to generate a first product signal;

second multiplication means for multiplying the second sinusoidal difference signal and the third cosine signal to generate a second product signal;

third multiplication means for multiplying the third sinusoidal difference signal and the first cosine signal to generate a third product signal;

summing means for summing the first, second, and third product signals to generate a summation signal; and

fourth multiplication means for multiplying the summation signal by a constant to generate a rate signal that is proportional to the rotational rate of the rotor.

16. The system of claim 15, wherein:

the rate signal is a first rate signal;

the system further comprises fourth, fifth, and sixth sensors evenly spaced about the rotor to sense the rotational rate thereof and supply fourth, fifth, and sixth sinusoidal sensor signals, respectively, each of the fourth, fifth, and sixth sinusoidal sensor signal being 120-degrees out of phase with each other, the fourth, fifth, and sixth sinusoidal signals additionally being 180-degrees out of phase with the first, second, and third sinusoidal signals, respectively; and

the motor controller further comprises;

fourth, fifth, and sixth differentiation means for differentiating the fourth, fifth, and sixth sinusoidal signals to obtain fourth, fifth, and sixth cosine signals, respectively;

fourth subtraction means for subtracting the fourth sinusoidal signal from the sixth sinusoidal signal to obtain a fourth sinusoidal difference signal;

fifth subtraction means for subtracting the fifth sinusoidal signal from the fourth sinusoidal signal to obtain a fifth sinusoidal difference signal;

sixth subtraction means for subtracting the sixth sinusoidal signal from the fifth sinusoidal signal to obtain a sixth sinusoidal difference signal;

fifth multiplication means for multiplying the fourth sinusoidal difference signal and the fifth cosine signal to obtain a fourth product signal;

sixth multiplication means for multiplying the fifth sinusoidal difference signal and the sixth cosine signal to obtain a fifth product signal;

seventh multiplication means for multiplying the sixth sinusoidal difference signal and the fourth cosine signal to obtain a sixth product signal;

second summing means for summing the fourth, fifth, and sixth product signals to obtain a second summation signal; and

eighth multiplication means for multiplying the second summation signal by the constant to obtain the second rate signal.

17. The system of claim 16, wherein the motor controller further comprises:

second summing means for summing the first and second rate signals to obtain compensated rate signal that is proportional to the rotational rate of the rotor.

18. The system of claim 15, further comprising:

rotor position determination means for generating a position signal representative of an instantaneous position of the rotor; and

a complementary filter coupled to receive the position signal and the rate signal and configured to supply a filtered position signal and a filtered rate signal.

19. The method of claim 18, further comprising:

subtraction means for subtracting the filtered position signal from the position signal to supply a position error signal;

gain adjustment means for applying a predetermined gain to the position error signal to supply an adjusted position error signal;

first integration means for integrating the position error signal and supplying a rate adjustment signal;

multiplication means for multiplying the rate signal and the rate adjustment signal to generate an adjusted rate signal;

summing means for summing the adjusted rate signal and the adjusted position error signal to generate the filtered rate signal; and

second integration means for integrating the filtered rate signal to obtain the filtered position signal.