Force rebalancing for MEMS inertial sensors using time-varying voltages

• US 7,444,868 B2
• Filed: 06/29/2006
• Issued: 11/04/2008
• Est. Priority Date: 06/29/2006
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Johnson, Burgess R.
• Primary Examiner(s): Kwok; Helen C.
• Application Number:
  US11/427,767
• Publication Number:
  US 20080000296A1
• Time in Patent Office: 859 Days
• Field of Search: 735/040.2, 735/040.4, 735/041.2, 735/041.4, 735/041.5, 735/143.2
• US Class Current: 73/504.12
• CPC Class Codes: G01C 19/5719 using planar vibrating masses driven in a translation vibration along an axis

Abstract

MEMS devices and methods employing one or more electrodes coupled to a time-varying rebalancing voltage are disclosed. A MEMS inertial sensor in accordance with an illustrative embodiment can include one or more proof masses, at least one sense electrode positioned adjacent to each proof mass, and one or more torquer electrodes. Rebalancing voltages can be applied to the torquer electrodes to electrostatically null quadrature and/or Coriolis-related proof mass motion along a sense axis of the device. The rebalancing voltages applied to each of the torquer electrodes can be adjusted using feedback from one or more force rebalancing control loops.

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; and

a plurality of torquer electrodes positioned adjacent to each of the one or more proof masses, wherein the torquer electrodes comprise;

one or more first torquer electrodes adapted to selectively control Coriolis-related motion of the one or more proof masses along the sense axis; and

one or more second torquer electrodes adapted to selectively control quadrature-related motion of the one or more proof masses along the sense axis; and

one or more time-varying rebalancing voltages applied to said torquer electrodes, the rebalancing voltages adapted to maintain a fixed capacitance between each sense electrode and its corresponding proof mass.

2. The MEMS inertial sensor of claim 1, wherein the time-varying rebalancing voltages includes an include one or more AC rebalancing voltages voltage.

3. The MEMS inertial sensor of claim 2, wherein the AC rebalancing voltages include voltage includes a rebalancing voltage signal component whose frequency is half of a motor drive frequency and a carrier voltage signal component whose frequency is half of a motor drive frequency, wherein said rebalancing voltage signal component is 90°

out-of-phase with the carrier voltage signal component.

4. The MEMS inertial sensor of claim 2, wherein the AC rebalancing voltage is a sinusoidal rebalancing voltage.

5. The MEMS inertial sensor of claim 1, wherein the one or more time-varying rebalancing voltages are outputs from at least one force rebalancing control loop.

6. The MEMS inertial sensor of claim 5, wherein said at least one force rebalancing control loop comprises a single force rebalancing control loop.

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

8. The MEMS inertial sensor of claim 1, wherein said one or more rebalancing voltages comprises:

one or more AC rebalancing voltages coupled to the one or more first torquer electrodes and adapted to control the Coriolis-related motion of the one or more proof masses; and

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

9. The MEMS inertial sensor of claim 1, wherein said one or more first number of torquer electrodes are coupled to a first rebalancing voltage signal outputted from a first force rebalance controller, and wherein said one or more second Humber of torquer electrodes are coupled to a second rebalancing voltage signal outputted from a second force rebalance controller.

10. The MEMS inertial sensor of claim 9, wherein the first rebalancing voltage signal is 9B 45°

out-of-phase with the second rebalancing voltage signal.

11. The MEMS inertial sensor of claim 9, wherein the first and second force rebalance controllers are separate controllers.

12. The MEMS inertial sensor of claim 9, wherein the first and second force rebalance controllers comprise a single controller.

13. The MEMS inertial sensor of claim 12, wherein said single controller is a multiple-input multiple-output controller.

14. The MEMS inertial sensor of claim 1, wherein said MEMS inertial sensor is a MEMS gyroscope.

15. The MEMS inertial sensor of claim 14, wherein said MEMS gyroscope is an in-plane MEMS gyroscope.

16. The MEMS inertial sensor of claim 14, wherein said MEMS gyroscope is an out-of-plane MEMS gyroscope.

17. The MEMS inertial sensor of claim 1, wherein said MEMS inertial sensor is an accelerometer.

18. 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 capacitively sense proof mass motion along a sense axis perpendicular to a drive axis of the one or more proof masses;

a first number of torquer electrodes adapted to provide rebalancing forces on said proof masses along the sense axis in a first direction, the first number of torquer electrodes adapted to selectively control Coriolis-related motion of the one or more proof masses along the sense axis; and

a second number of torquer electrodes adapted to provide rebalancing forces in an opposite direction from the first direction along the sense axis, the second number of torquer electrodes adapted to selectively control quadrature-related motion of the one or more proof masses along the sense axis;

wherein the rebalancing forces are adapted to maintain a fixed capacitance between each sense electrode and corresponding proof mass based on feedback from one or more force rebalancing control loops.

26. The MEMS inertial sensor of claim 18, wherein said proof masses are interposed between a lower substrate and an upper substrate, and said first number of torquer electrodes are positioned on said lower substrate, and said second number of torquer electrodes are positioned on said upper substrate.

19. A method of force rebalancing a MEMS inertial sensor, the MEMS inertial sensor including one or more proof masses adapted to oscillate at a motor drive frequency, and at least one sense electrode positioned adjacent to each of the one or more proof masses, each sense electrode coupled to a sense bias voltage source for sensing displacement of the one or more proof masses along a sense axis perpendicular to a drive axis of the one or more proof masses, the method comprising the steps of:

applying one or more time-varying rebalancing voltages to a plurality of torquer electrodes adjacent to each proof mass, wherein applying the rebalancing voltages comprises;

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

sensing any displacement of the one or more proof masses along the sense axis and outputting a sense voltage having an amplitude in proportion to the proof mass displacement; and

electrostatically nulling any proof mass motion along the sense axis based on the outputted sense voltage.

20. The method of claim 19, wherein the rebalancing voltages applied to each of the torquer electrodes are adapted to maintain a fixed capacitance between each sense electrode and corresponding proof mass.

21. The method of claim 19, wherein said step of electrostatically nulling proof mass motion along the sense axis is accomplished by adjusting the rebalancing voltages using at least one force rebalancing control loop.

22. The method of claim 21, wherein said at least one force rebalancing control loop comprises a single force rebalancing control loop.

23. The method of claim 21, wherein said at least one force rebalancing control loop comprises multiple force rebalancing control loops.

24. The method of claim 19, wherein the time-varying rebalancing voltages include one or more AC rebalancing voltages.

25. The method of claim 24, wherein the AC rebalancing voltages include a rebalancing voltage signal component whose frequency is about half of a motor drive frequency, and a carrier voltage signal component whose frequency is about half of the motor drive frequency, wherein said rebalancing voltage signal component is 90°

out-of-phase with the carrier voltage signal component.

27. The method of claim 19, wherein said proof masses are interposed between a lower substrate and an upper substrate, and said first number of torquer electrodes are positioned on said lower substrate, and said second number of torquer electrodes are positioned on said upper substrate.