Force rebalancing and parametric amplification of MEMS inertial sensors

• US 7,444,869 B2
• Filed: 10/16/2006
• Issued: 11/04/2008
• Est. Priority Date: 06/29/2006
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Johnson, Burgess R., Cabuz, Eugen I.
• Primary Examiner(s): Kwok; Helen C.
• Application Number:
  US11/549,769
• Publication Number:
  US 20080236280A1
• Time in Patent Office: 750 Days
• Field of Search: 735/040.2, 735/040.4, 735/041.2, 735/041.4, 735/041.5, 735/041.6, 735/041.3, 735/143.2, 735/141.6
• US Class Current: 73/504.12
• CPC Class Codes: G01C 19/5719 using planar vibrating masses driven in a translation vibration along an axis
• CPC Class Codes: G01C 19/5726 Signal processing

Abstract

MEMS devices and methods for measuring Coriolis forces using force rebalancing and parametric gain amplification techniques are disclosed. A MEMS inertial sensor can include one or more proof masses, at least one sense electrode positioned adjacent to each proof mass, a number of torquer electrodes for electrostatically nulling quadrature and Coriolis-related proof mass motion, and a number of pump electrodes for producing a pumping force on the proof masses. Force rebalancing voltages can be applied to some torquer electrodes to electrostatically null quadrature and/or Coriolis-related proof mass motion along a sense axis of the device. A pumping voltage at approximately twice the motor drive frequency of the proof masses can be used to pump the proof masses along the sense axis.

Claims

1. A MEMS inertial sensor, comprising:

one or more proof masses adapted to oscillate at a motor drive frequency;

at least one sense electrode positioned adjacent to each of the one or more proof masses, the sense electrode adapted to sense proof mass motion along a sense axis perpendicular to a drive axis of the one or more proof masses;

a first number of force rebalancing torquer electrodes coupled to an AC force rebalancing voltage signal and adapted to control Coriolis-related motion of the one or more proof masses; and

a second number of force rebalancing torquer electrodes coupled to a DC force rebalancing voltage signal and adapted to control quadrature-related motion of the one or more proof masses.

2. The MEMS inertial sensor of claim 1 further comprising:

at least one pump electrode coupled to a pump voltage and adapted to produce a pumping force on the one or more proof masses in a direction of the sense axis.

3. The MEMS inertial sensor of claim 1, wherein at least one of said AC force rebalancing voltage signal and said DC force rebalancing voltage signal is adapted to maintain a fixed capacitance between each sense electrode and corresponding proof mass.

4. The MEMS inertial sensor of claim 1, wherein at least one of said force rebalancing voltage signals are an output voltage from at least one force rebalancing control loop.

5. The MEMS inertial sensor of claim 4, wherein said at least one force rebalancing control loop comprises multiple force rebalancing control loops.

6. The MEMS inertial sensor of claim 2, wherein the pump voltage has a frequency at approximately twice the motor drive frequency of the one or more proof masses.

7. The MEMS inertial sensor of claim 2, wherein the pumping force produced by the pump voltage is at approximately twice the motor drive frequency of the one or more proof masses.

8. The MEMS inertial sensor of claim 2, wherein the pumping force is adapted to produce non-linear mechanical and electrical mixing within the inertial sensor for parametrically amplifying Coriolis forces exerted on the one or more proof masses along the sense axis.

9. The MEMS inertial sensor of claim 2, wherein the pump voltage includes a DC bias voltage component and an AC pump voltage component adapted to modulate a resonant frequency one of more of the proof masses along the sense axis.

10. The MEMS inertial sensor of claim 1, wherein said MEMS inertial sensor is an in-plane MEMS gyroscope.

11. The MEMS inertial sensor of claim 1, wherein said MEMS inertial sensor is an out-of-plane MEMS gyroscope.

12. A MEMS inertial sensor, comprising:

one or more proof masses adapted to oscillate at a motor drive frequency;

at least one sense electrode positioned adjacent to each of the one or more proof masses, the sense electrode adapted to sense proof mass motion along a sense axis perpendicular to a drive axis of the one or more proof masses;

at least one force rebalancing electrode coupled to a time-varying rebalancing voltage, the time-varying rebalancing voltage having a frequency at half the motor drive frequency; and

at least one pump electrode coupled to a pump voltage, the pump voltage having a frequency at twice the motor drive frequency of the one or more proof masses;

wherein a pumping force produced by the pump voltage is adapted to parametrically amplify Coriolis forces exerted on the one or more proof masses along the sense axis.

13. A method of measuring Coriolis forces on a MEMS inertial sensor, comprising the steps of:

oscillating one or more proof masses at a motor drive frequency;

sensing any displacement of the one or more proof masses in a sense mode of oscillation along a sense axis perpendicular to a drive axis of the one or more proof masses;

providing a first rebalancing force to the one or more proof masses along the sense axis, the first rebalancing force for controlling a quadrature-related motion of the one or more proof masses;

providing a second rebalancing force to the one or more proof masses along the sense axis, the second rebalancing force for controlling a Coriolis-related motion of the one or more proof masses;

providing a pumping force to the one or more proof masses along the sense axis at approximately twice the motor drive frequency; and

detecting Coriolis forces on the one or more proof masses in the sense mode of oscillation.

14. The method of claim 13, wherein said step of providing a first and a second rebalancing force to the one or more proof masses includes the step of electrostatically nulling proof mass motion based on voltage signals from at least one force rebalancing control loop.

15. The method of claim 14, wherein said at least force rebalancing control loop includes:

a first force rebalancing control loop for controlling the quadrature-related motion of the one or more proof masses; and

a second force rebalancing control loop for controlling the Coriolis-related motion of the one or more proof masses.

16. The method of claim 13, wherein said step of providing a rebalancing force to the one or more proof masses includes the steps of:

providing a first rebalancing voltage to a first number of torquer electrodes adapted to selectively control the quadrature-related motion of the one or more proof masses along the sense axis; and

providing a second rebalancing voltage to a second number of torquer electrodes adapted to selectively control the Coriolis-related motion of the one or more proof masses along the sense axis.

17. The method of claim 16, wherein said second rebalancing voltage is a time-varying rebalancing voltage having a frequency approximately half of the motor drive frequency.

18. The method of claim 13, wherein said step of providing a pumping force to the one or more proof masses includes the step of applying a pump voltage to a number of torquer electrodes, the pump voltage including a DC bias voltage component and an AC pump voltage component adapted to modulate a sense mode resonant frequency of the one or more proof masses.

19. The method of claim 13, wherein the pumping force is adapted to produce non-linear mechanical and electrical mixing within the inertial sensor for parametrically amplifying Coriolis related motion of the one or more proof masses.