Vibratory gyroscope utilizing a frequency-based measurement and providing a frequency output

• US 8,763,459 B2
• Filed: 11/03/2009
• Issued: 07/01/2014
• Est. Priority Date: 11/03/2008
• Status: Active Grant

• Current Assignee: Georgia Tech Research Corporation (University System of Georgia)
• Original Assignee: Georgia Tech Research Corporation (University System of Georgia)
• Inventors: Brand, Oliver, Schild, Stefan
• Primary Examiner(s): CHAPMAN JR, JOHN E
• Application Number:
  US13/127,224
• Publication Number:
  US 20120111120A1
• Time in Patent Office: 1,701 Days
• Field of Search: 735/041.2, 735/041.4
• 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

A vibratory gyroscope utilizing a frequency-based measurement and providing a frequency output.

Claims

1. A method of detecting rotation rate from changes in frequency comprising:

suspending a mass movable along or around one or more axes;

vibrating the mass along or around a first of the one or more axes at an initial sense mode frequency by a sense mode signal;

vibrating the mass along a second of the one or more axes at an initial drive mode frequency by a drive mode signal;

obtaining a change in the sense mode frequency from its initial sense mode frequency upon rotation of the mass about an axis that does not coincide with the first of the one or more axes;

wherein the change of frequency of the sense mode signal from the initial sense mode frequency is indicative of a rotation rate of the mass.

2. The method of claim 1, wherein the initial sense mode frequency is the resonant frequency of the mass along or around the first of the one or more axes.

3. The method of claim 1, wherein the rotation rate of the mass generates a force acting on the mass that has a component that is proportional to an amount of deflection along the first of the one or more axes.

4. The method of claim 1, wherein the initial drive mode frequency is approximately equal to the initial sense mode frequency.

5. The method of claim 1, wherein the initial sense mode frequency is the resonant frequency of the mass along or around the first of the one or more axes, and wherein the initial drive mode frequency is the resonant frequency of the mass along or around the second of the one or more axes.

6. The method of claim 1, wherein the first of the one or more axes and the second of the one or more axes are perpendicular to each other.

7. The method of claim 6, wherein the mass is rotated around an axis perpendicular to the drive mode axis and perpendicular to the first of the one or more axes and the second of the one or more axes.

8. A rotation rate sensor comprising:

at least one mass with two perpendicular vibration modes, capable of vibrating along an x axis at a resonant frequency f_x, and capable of vibrating along a y axis at a resonant frequency f_y,

a first driving mechanism that imparts a sense mode vibration having frequency, amplitude, and phase to the mass along a sense mode axis, being one of the x or y axes;

a second driving mechanism that imparts a drive mode vibration having frequency, amplitude, and phase to the mass along a drive mode axis, being the axis perpendicular to the sense mode axis;

a first feedback circuit for monitoring the sense mode vibration and making adjustments to the first driving mechanism; and

an output signal having a default frequency;

wherein upon rotation of the mass about an axis orthogonal to the x and y axes, the variation in the output signal from the default frequency is indicative of a rotation rate of the mass.

9. The rotation rate sensor of claim 8, further comprising a second feedback circuit for monitoring the drive mode vibration and making adjustments to the second driving mechanism.

10. The rotation rate sensor of claim 9, wherein the frequency of the drive mode vibration and the frequency of the sense mode vibration are approximately equal.

11. The rotation rate sensor of claim 9, wherein the phase of the vibration along the drive mode axis and the phase of the vibration along the sense mode axis are shifted approximately 90 degrees from one another.

12. The rotation rate sensor of claim 9, wherein the first and second driving mechanisms are each operated in a closed-loop configuration with constant amplitude at their respective resonance frequencies.

13. The rotation rate sensor of claim 9, wherein a constant ratio is maintained between the amplitude of vibration along the sense mode axis and the amplitude of vibration along the drive mode axis.

14. The rotation rate sensor of claim 9, wherein the amplitude of the frequency-modulated output signal maintains a constant level.

15. A method of detecting rate of rotation from changes in frequency comprising:

vibrating a mass along or around a first axis at an initial drive mode frequency by applying a force to the mass;

vibrating a mass along or around a second axis at an initial sense mode frequency by applying a force to the mass;

applying an additional force to the mass to restore the initial sense mode frequency of vibration to the mass; and

measuring the additional force needed to restore the initial frequency of vibration.