Micro rate of rotation sensor and method for operating a micro rate of rotation sensor

• US 9,784,580 B2
• Filed: 10/05/2015
• Issued: 10/10/2017
• Est. Priority Date: 12/28/2011
• Status: Active Grant

• Current Assignee: Hanking Electronics Hongkong Company Limited
• Original Assignee: Hanking Electronics, Ltd.
• Inventors: Coronato, Luca, Cazzaniga, Gabriele
• Primary Examiner(s): Kwok, Helen
• Application Number:
  US14/875,379
• Publication Number:
  US 20160033275A1
• Time in Patent Office: 736 Days
• Field of Search: 7350412, 7350414, 7350404, 7350402
• CPC Class Codes: G01C 19/42 for indicating rate of turn; for integrating rate of turn
• CPC Class Codes: G01C 19/5642 using vibrating bars or beams
• CPC Class Codes: G01C 19/5712 the devices involving a micromechanical structure
• CPC Class Codes: G01C 19/5719 using planar vibrating masses driven in a translation vibration along an axis
• CPC Class Codes: G01C 19/5747 each sensing mass being connected to a driving mass, e.g. driving frames

Abstract

The present invention relates to a method for operating a rotation sensor for detecting a plurality of rates of rotation about orthogonal axes (x,y,z). The rotation sensor comprises a substrate, driving masses, X-Y sensor masses, and Z sensor masses. The driving masses are driven by drive elements to oscillate in the X-direction. The X-Y sensor masses are coupled to the driving masses, and driven to oscillate in the X-Y direction radially to a center. When a rate of rotation of the substrate occurs about the X-axis or the Y-axis, the X-Y sensor masses are jointly deflected about the Y-axis or X-axis. When a rate of rotation of the substrate occurs about the Z-axis, the X-Y sensor masses are rotated about the Z-axis, and the Z sensor masses are deflected substantially in the X-direction.

Claims

1. A rotation sensor for detecting a rate of rotation about at least one axis of orthogonal axes, the rotation sensor comprising:

a substrate;

a central anchor coupled to the substrate;

a plurality of masses that are coupled to the central anchor and displaceable relative to the substrate and disposed in a first plane parallel to the substrate;

a first driving means that oscillates a first sensor mass within the plurality of masses, the first sensor mass radially oscillates in a first direction in the first plane and between first and second axes of the rotation sensor;

a second driving means that oscillates a second sensor mass within the plurality of masses, the second sensor mass radially oscillates in a second direction in the first plane and between the first and second axes of the rotation sensor; and

a first sensor element coupled to the first sensor mass, the first sensor element detects a first deflection of the first sensor mass caused by a first rotation about the first axis.

2. The rotation sensor of claim 1 further comprising a second sensor element coupled to the second sensor mass, the second sensor element detects a second deflection of the second sensor mass caused by the first rotation.

3. The rotation sensor of claim 2 wherein the first and second driving means move in antiphase to each other and the first and second sensor masses move radially to the central anchor and away and toward each other in the first and second directions.

4. The rotation sensor of claim 2 wherein a first rate of rotation is identified based on changes in the first and second deflections.

5. The rotation sensor of claim 1 further comprising a second sensor element coupled to the second sensor mass, the second sensor element detects a second deflection of the second sensor mass caused by a second rotation about the first or second axis.

6. The rotation sensor of claim 5 wherein the first and second directions are at angles of 45 degrees from the first and second axes.

7. The rotation sensor of claim 5 wherein a first rate of rotation around the first axis is identified based at least partially on the first deflection and a second rate of rotation around the second axis is identified based at least partially on the second deflection.

8. The rotation sensor of claim 1 wherein the first deflection is measured based on an electrical signal change.

9. The rotation sensor of claim 1 comprising a plurality of springs, a first spring within the plurality of springs being coupled to the first sensor mass and supporting movement of the first sensor mass along the first direction and a second spring within the plurality of springs being coupled to the second sensor mass and supporting movement of the second sensor mass along the second direction.

10. The rotation sensor of claim 1 further comprising:

a second sensor element coupled to the second sensor mass, the second sensor element detects a second deflection of the second sensor mass caused by a second rotation about the second axis;

a third sensor mass within the plurality of masses, the third sensor mass being connected to the first and second sensor masses to oscillate in the first direction; and

a third sensor element coupled to the third sensor mass, the third sensor element detects a third deflection of the third sensor mass caused by a third rotation about a third axis.

11. The rotation sensor of claim 10 wherein the third axis is a Z-axis that is orthogonal to the first and second axes.

12. The rotation sensor of claim 1 further comprising an elastic attachment configured as a gimbal suspension having axes of rotation about the first axis and disposed between the first sensor mass and the central anchor.

13. The rotation sensor of claim 1 further comprising synchronization springs between a subset of masses within the plurality of masses, the synchronization springs facilitate synchronized movement between the subset of masses.

14. The rotation sensor of claim 1 further comprising drive elements that drive movement of the first and second driving masses, the drive elements comprising a plurality of electrodes.

15. The rotation sensor of claim 1 wherein the first sensor element detects the first rotation using the first deflection to generate a first electrical signal, a second sensor element detects the first rotation using a second deflection to generate a second electrical signal, and a rate of the first rotation is determined using the first and second electrical signals.

16. A method for sensing at least one rate of rotation about at least one axis of orthogonal axes, the method comprising:

causing a first sensor mass to radially oscillate from a central location in a first direction between first and second axes and in a first plane;

detecting a first deflection of a first sensor element coupled to the first sensor mass, the first deflection resulting from a first rotation about the first axis;

detecting a second deflection of a second sensor element coupled to the first sensor mass, the second deflection resulting from the first rotation about the first axis; and

determining a rate of the first rotation by generating electrical signals corresponding to changes in the first and second deflections.

17. The method of claim 16 further comprising:

causing a second sensor mass to radially oscillate from the central location in a second direction between first and second axes and in the first plane, the first and second directions being at angles of 45 degrees from the first and second axes;

detecting a third deflection of a third sensor element coupled to the second sensor mass, the third deflection resulting from a second rotation about the second axis;

detecting a fourth deflection of a fourth sensor element coupled to the second sensor mass, the fourth deflection resulting from the second rotation about the second axis; and

determining a rate of the second rotation by generating electrical signals corresponding to changes in the first and second deflections.

18. The method of claim 17 further comprising the steps of:

identifying a first electrical signal change on the first sensor element based on the first deflection; and

identifying a second electrical signal change on the second sensor element based on the first deflection.

19. The method of claim 17 further comprising the step of coupling the first and second sensor masses by at least one spring causing the oscillations of the first and second sensor masses to be synchronized.