Coriolis effect rotation rate sensor and method

• US 5,604,311 A
• Filed: 06/07/1995
• Issued: 02/18/1997
• Est. Priority Date: 06/07/1995
• Status: Expired due to Fees

• Current Assignee: Litton Systems Incorporated (Northrop Grumman Corporation)
• Original Assignee: Litton Systems Incorporated (Northrop Grumman Corporation)
• Inventors: Voros, Arthur R., Kumar, Lalit
• Primary Examiner(s): Oda, Christine K.
• Application Number:
  US08/480,218
• Time in Patent Office: 622 Days
• Field of Search: 73/504.02, 73/504.04, 73/504.12, 73/504.03, 73/504.14
• US Class Current: 73/504.14
• CPC Class Codes: G01C 19/5719 using planar vibrating masses driven in a translation vibration along an axis

Abstract

A monolithic Coriolis rate sensor includes a first member and a vibration generator that causes the member to vibrate along a first direction. At least one other member is mechanically coupled to the first member so that orthogonal vibrational modes are coupled to the other member when the members are rotated about a rotation axis. The vibrational mode coupling occurs as a result of the Coriolis effect. A vibration sensor is used to sense the orthogonal vibrational modes, the amplitude of which determines the rate at which the members are rotated. In a preferred embodiment, a central and two transverse end members with substantially equal resonant frequencies are mechanically coupled to form an "I"-shaped structure. The center member is vibrated at its resonant frequency, and orthogonal vibrational modes are coupled to the end members when the structure is rotated about a rotational axis that is orthogonal to both vibration directions. A tuning mechanism is also provided that allows for in-situ tuning of the members'"'"' resonant frequencies.

Claims

1. A sensor for sensing the Coriolis effect, comprising:

a mechanical structure, consisting of a base, a longitudinal member and one or more transverse members, said one or more transverse members being attached at their centers to the ends of said longitudinal member, said one or more transverse members and said longitudinal member lying in a plane, the ends of said one or more transverse members and any end of said longitudinal member not attached to a transverse member being attached to said base,

a vibration generator for generating vibrations in said longitudinal member along an x-direction, said x-direction being in the plane of said one or more transverse members and said longitudinal member and parallel to said transverse members, and

a vibration sensor for sensing vibrations in said one or more transverse members along a y-direction, said y-direction being in the plane of said one or more transverse members and said longitudinal member and parallel to said longitudinal member,

said x-direction vibrations causing said one or more transverse members to vibrate along said y-direction when said base is rotated about a rotation axis that is orthogonal to said x and y-directions as a result of the Coriolis force exerted on said longitudinal member.

2. The sensor of claim 1, further comprising a processor connected to said vibration sensor for calculating said structure'"'"'s rate of rotation from said y-direction vibrations.

3. A rotation sensor, comprising:

a base,

a first member oriented parallel to a y-direction,

an oscillation generator positioned to initiate and maintain flexural oscillations in said first member at a driving frequency along an x-axis normal to the first member, the first member having a resonant frequency, the driving frequency being substantially equal to the resonant frequency of the first member,

at least one other member oriented parallel to the x-axis and attached at its center to an end of said first member, said at least one other member and said first member lying in a plane, any end of said first member not attached to another member and the ends of said at least one other member being attached to the base, said at least one other member having a resonant frequency substantially equal to the resonant frequency of said first member, said x-direction flexural oscillations inducing a Coriolis force along said y-direction when said base is rotated about a rotation axis that is orthogonal to said x and y directions, thereby causing flexural oscillations along said y-direction in said at least one other member,

at least one oscillation sensor for sensing the amplitude of said at least one other member'"'"'s flexural oscillations along said y-direction, and

a processor for calculating said rate of rotation about said rotation axis from the amplitude of said flexural oscillations along said y-direction.

4. The sensor of claim 3, wherein said first member comprises a first central member, and said at least one other member comprises second and third transverse members that are mechanically coupled to said first central member to form an "I"-shaped structure.

5. The sensor of claim 4, wherein said base and said first, second, and third members are etched from a dielectric substrate, said base and said first, second, and third members forming a monolithic structure.

6. The sensor of claim 5, wherein said first, second, and third members are coated with an electrically conductive material, and said oscillation generator comprises;

a first capacitive forcer electrode positioned on said substrate to apply an electric force to said first member along said x-direction,

a first capacitive pickoff electrode positioned on said substrate to sense the flexure of said first member along said x-direction, and

an oscillation controller for varying the electric force applied by said forcer electrode in response to feedback from said pickoff electrode, so that a constant amplitude flexure oscillation is set up in said first member at said first member'"'"'s resonant frequency.

7. The sensor of claim 5, wherein said at least one oscillation sensor comprises:

second and third capacitive pickoff electrodes positioned on said substrate to sense flexural oscillations in said second and third members, respectively, along said y-direction,

second and third capacitive forcer electrodes positioned on said substrate to apply a compensating electric force to said second member along said y-direction,

fourth and fifth capacitive forcer electrodes positioned on said substrate to apply a compensating electrical force to said third member along said y-direction, and

an oscillation sensor controller for adjusting the electric force applied by said second, third fourth, and fifth capacitive forcer electrodes so that the flexural oscillations in said second and third members are nulled.

8. The sensor of claim 7, wherein said processor is calibrated to calculate the rate of rotation about said rotation axis from the amount of electric force required to null the flexural oscillations in said second and third members.

9. The sensor of claim 7, wherein said first, second, and third members are enclosed in an evacuated enclosure.

10. The sensor of claim 9, wherein said enclosure further comprises a tuning mechanism for tuning the resonant frequencies of said members, said tuning mechanism comprising:

a plurality of cavities on the inside surface of said enclosure, and

metallic material disposed in said cavities,

each of said cavities positioned so that its respective metallic material is deposited on at least one of said first, second, and third members when said metallic material is evaporated, thereby changing the mass and resonant frequency of said at least one member.

11. The sensor of claim 10, wherein said enclosure comprises a dielectric that is optically transparent at a predetermined optical wavelength so that said metallic material can be heated and evaporated by directing an optical beam to said material through said enclosure, thereby allowing in-situ frequency tuning of said first, second, or third member.

12. A method of measuring rotation rate about a rotation axis, comprising the steps of:

inducing vibrational oscillations in a first member along an x-direction that is orthogonal to said rotational axis, said first member mechanically coupled to at least one other member that is restrained so that it can only oscillate along a y-direction that is orthogonal to said rotation axis and said x-direction,

sensing vibrational oscillations in the at least one other member that are induced along said y-direction by the Coriolis effect, and

deriving the rate at which said members are rotated about said rotation axis from the amplitude of said oscillations along said y-direction, the term members denoting said first member and said at least one other member.

13. The method of claim 12, wherein said members are tuned so that they have substantially equal resonant frequencies.

14. The method of claim 12, wherein said oscillations are induced in said first member by:

applying a time-varying force to said first member along said x-direction, and

monitoring said induced oscillations and adjusting said force to maintain a constant oscillation amplitude and an oscillation frequency substantially equal to said first member'"'"'s resonant frequency.

15. The method of claim 12, wherein the oscillations along said y-direction are sensed by:

monitoring the amplitude of y-direction oscillations in said at least one other member, and

applying a force to said at least one other member sufficient to null said y-direction oscillations.

16. The method of claim 15, wherein said rotation rate is derived from the amount of force required to null said oscillations in said at least one other member.

17. The method of claim 13, wherein said members are tuned by reducing the mass of at least one of said members.

18. The method of claim 13, wherein said members are tuned by adding mass to at least one of said members.

19. The method of claim 18, wherein mass is added to at least one of said members by:

enclosing said members in an evacuated enclosure, said enclosure having a plurality of cavities on its inside surface and metallic material disposed in said cavities, with each of said cavities positioned so that its respective metallic material is deposited on at least one of said members when said metallic material is evaporated, and

evaporating the metallic material in at least one of said cavities until said members are tuned to substantially equal resonant frequencies.

20. The method of claim 19, wherein said members are enclosed in a dielectric enclosure that is optically transparent at a predetermined optical wavelength, and said metallic material is evaporated by heating it with an optical beam, at said predetermined wavelength, that is directed to said material through an outer surface of said enclosure.

21. The method of claim 20, wherein said members are enclosed in a dielectric enclosure that is optically transparent at approximately 1.06 microns and said metallic material is heated with a ND:

YAG laser beam that is focused onto said material through said enclosure.