Tri-axis Angular Rate Sensor

• US 20100236327A1
• Filed: 03/17/2009
• Published: 09/23/2010
• Est. Priority Date: 03/17/2009
• Status: Active Grant

• Current Assignee: Memslink Technologies, Co. Ltd.
• Original Assignee: Minyao Mao
• Inventors: Mao, Minyao
• Granted Patent: US 8,256,290 B2
• Time in Patent Office: Days
• US Class Current: 73/504.120
• CPC Class Codes: G01C 19/5719 using planar vibrating masses driven in a translation vibration along an axis

Abstract

Angular rate sensor for detecting rotation about first, second and third mutually perpendicular input axes having a plurality of generally planar proof masses coupled together for linear drive-mode oscillation along multi-directional drive axes in a plane formed by the first and second input axes. The masses are mounted on a generally planar sense frame for linear movements relative to the sense frame in drive-mode and for rotation together with the sense frame in sense modes. The sense frame is mounted for rotation with the masses in sense modes about the first, second, and third input axes independent of each other, in response to Coriolis forces produced by rotation of the masses about the first, second, and third input axes respectively. And capacitance sensors responsive to the rotational movements of the masses and the sense frame in sense modes are employed for monitoring rate of rotation.

Claims

1. An angular rate sensor for detecting rotation about first, second and third mutually perpendicular input axes, comprising a substrate, a sense frame disposed in a plane formed by the first and second input axes, means for mounting the sense frame on the substrate and permitting the sense frame to rotate about the first, second, and third input axes independently of one another, a plurality of proof masses having predetermined drive axes in the plane with at least two drive axes forming an angle with one another which is larger than 0 and less than 180 degrees, means for mounting the masses on the sense frame and constraining each mass for linear movement relative to the sense frame along the drive axis of the mass in drive-mode and for rotation with the sense frame in sense modes, means for coupling the proof masses together to form a single drive-mode oscillation, actuation means for driving the masses to oscillate in drive-mode, detection means for monitoring sense mode rotation of the proof masses and the sense frame about the first, second, and third input axes in response to Coriolis forces produced by rotation of the masses about the first, second, and third input axes respectively.

2. The angular rate sensor of claim 1 wherein the proof masses are generally planar and disposed in the plane around a center so that their drive axes intersect one another approximately at the center.

3. The angular rate sensor of claim 1 wherein said means for mounting each mass on the sense frame comprises a set of flexures, which are relatively flexible in the direction along the drive axis of the mass, but relatively stiff in other directions.

4. The angular rate sensor of claim 1 wherein said means for coupling the proof masses comprises a plurality of coupling structures connected between adjacent ones of the masses.

5. The angular rate sensor of claim 4 wherein each said coupling structure is a link beam, which is disposed between two adjacent masses and extends along a direction that forms predetermined angles to the drive axes of the two masses.

6. The angular rate sensor of claim 4 wherein each said coupling structure is a box spring, which is disposed between two adjacent masses and oriented with its longitudinal axis forming predetermined angles to the drive axes of the two masses.

7. The angular rate sensor of claim 1 wherein said means for coupling the proof masses comprises a plurality of coupling structures connected between adjacent ones of the masses with at least one member of each coupling structure mounted on the sense frame.

8. The angular rate sensor of claim 7 wherein each said coupling structure comprises a pair of tilt beams joined at one end to form a joint, with the other ends connected to two adjacent masses respectively, each of said tilt beams being extended in a direction tilted with a predetermined angle from that perpendicular to the drive axis of the mass to which the beam is connected, a supporting beam oriented in a direction which forms predetermined angles to the drive axes, with one end joined to the joint of the tilt beams and the other end mounted to the sense frame.

9. The angular rate sensor of claim 7 wherein each said coupling structure comprises a first pair of tilt beams with one end connected to the masses, each of said tilt beams being extended in a direction tilted with a predetermined angle from that perpendicular to the drive axis of the mass to which the beam is connected, a second pair of supporting beams mounted on the sense frame at one end, with the other end connected to the other end of the first pair of beams to form a first, and second joints respectively, a third pair of transfer beams connected to the first, and second joints at one end respectively and joined together at the other end to form a third joint, the third joint being further mounted to the sense frame by a lateral spring extended in a predetermined direction for constraining the joint for movement perpendicular to that direction.

10. The angular rate sensor of claim 1 wherein said means for mounting and permitting the sense frame to rotate about the first, second, and third input axes comprises a first and second gimbals disposed in the plane and positioned within the sense frame with the first one surrounding the second, an anchor post positioned within the second gimbal and affixed to the substrate, a plurality of flexures connected between the sense frame and the first gimbal and extended in radial directions for constraining the sense frame for rotation about the third input axis relative to the first gimbal, a first pair of torsion beams connected between the first and second gimbals and extended along the first input axis for the first gimbal to rotate relative to the second gimbal about the first input axis, a second pair of torsion beams connected between the second gimbal and the anchor post and extended along the second input axis for the second gimbal to rotate about the second input axis.

11. The angular rate sensor of claim 1 wherein said means for mounting and permitting the sense frame to rotate about the first, second, and third input axes comprises a first and second gimbals disposed in the plane with the first gimbal surrounding the sense frame and the second gimbal surrounding the first one, a plurality of anchor posts positioned surrounding the second gimbal, a first pair of torsion beams connected between the sense frame and the first gimbal and extended along the first input axis for the sense frame to rotate relative to the first gimbal about the first input axis, a second pair of torsion beams connected between the first and second gimbals and extended along the second input axis for the first gimbal to rotate relative to the second one about the second input axis, a plurality of flexures connected between the second gimbal and the anchor posts and extended in radial directions for constraining the second gimbal for rotation about the third input axis.

12. The angular rate sensor of claim 1 wherein said actuation means includes comb drives mounted on at least one of the proof masses.

13. The angular rate sensor of claim 1 wherein said detection means for monitoring sense mode rotation of the masses and the sense frame in response to Coriolis forces includes electrode plates disposed on the substrate beneath the masses and the sense frame to form capacitors with the masses and the sense frame for monitoring the sense rotation about the first, and second input axes, parallel plate capacitors with moving plates mounted on the sense frame and interleaved with stationary plates affixed to the substrate for monitoring the sense rotation about the third axis.

14. An angular rate sensor for detecting rotation, comprising a substrate, a plurality of generally planar proof masses disposed around a center for linear oscillations along multi-directional drive axes which lie in the plane of the masses and intersect one another approximately at the center with at least two drive axes forming an angle with one another which is larger than 0 and less than 180 degrees, coupling structures connected between adjacent ones of the masses for constraining the masses to oscillate in a cooperative manner in drive-mode, comb drives mounted on at least one of the masses for driving the masses to oscillate in drive-mode, a first, second and third mutually perpendicular input axes with the first and second input axes lying in the plane of the masses and the third input axis perpendicular to the plane, a sense frame disposed in the plane of the masses and mounted on the substrate by a suspension structure for rotation about the first, second and third input axes independent of one another, flexures mounting the masses on the sense frame for linear movements relative to the sense frame along the drive axes in drive-mode and for rotation with the sense frame about each input axis in sense modes, and capacitance sensors responsive to sense mode rotation movements of the masses and the sense frame about the first, second, and third input axes in response to Coriolis forces produced by rotation of the masses about the first, second, and third input axes respectively, for monitoring rate of rotation.

15. The angular rate sensor of claim 14 wherein said cooperative manner is in-phase manner.

16. The angular rate sensor of claim 14 wherein said cooperative manner is anti-phase manner.

17. The angular rate sensor of claim 14 wherein said suspension structure includes multiple rotation members connected in series by gimbals.

18. The angular rate sensor of claim 17 wherein said rotation members are disposed within the sense frame.

19. The angular rate sensor of claim 17 wherein said rotation members are disposed surrounding the sense frame.

20. An angular rate sensor for detecting rotation, comprising at least one input axis, each being pre-selected from three mutually perpendicular axes, a plurality of proof masses being coupled together for linear drive-mode oscillation along drive axes in a plane formed by the first and second axes of said three mutually perpendicular axes, with at least two masses oscillating along drive axes forming an angle with one another which is larger than zero and less than 180 degrees, means for driving the masses to oscillate in drive-mode, a sense frame disposed in the plane for supporting the masses and mounted for rotation with the masses about each said input axis independent of one another in sense mode in response to Coriolis forces produced by rotation of the masses about the input axis, and means responsive to the rotational movement of the sense frame and the masses about each input axis for monitoring the rate of rotation.

21. The angular rate sensor of claim 20 wherein the masses are generally planar and disposed in the plane around a center so that their drive axes intersect one another approximately at the center.

22. The angular rate sensor of claim 20 wherein each mass is mounted on the sense frame by a set of flexures, which are relatively flexible along the drive axis of the mass for linear movement relative to the sense frame in drive-mode, and relatively stiff in all other directions so that the masses and the sense frame move together in each sense mode.

23. The angular rate sensor of claim 20 wherein the proof masses are coupled by a plurality of coupling structures with each one connected between two adjacent masses.

24. The angular rate sensor of claim 23 wherein each said coupling structure comprises a link beam that is disposed between two adjacent masses and extends along a direction that forms predetermined angles to the drive axes of the two masses.

25. The angular rate sensor of claim 23 wherein each said coupling structure comprises a box spring which is disposed between two adjacent masses with its longitudinal axis forming predetermined angles to the drive axes of the two masses.

26. The angular rate sensor of claim 20 wherein the proof masses are coupled by a plurality of coupling structures with each one connected between two adjacent masses and having at least one member of each coupling structure mounted on the sense frame.

27. The angular rate sensor of claim 26 wherein each said coupling structure comprises a pair of tilt beams joined at one end to form a joint, with the other ends connected to two adjacent masses respectively, each of said tilt beams being extended in a direction tilted with a predetermined angle from that perpendicular to the drive axis of the mass to which the beam is connected, a supporting beam oriented in a direction which forms predetermined angles to the drive axes, with one end joined to the joint of the tilt beams and the other end mounted to the sense frame.

28. The angular rate sensor of claim 26 wherein each said coupling structure comprises a first pair of tilt beams with one end connected to the masses, each of said tilt beams being extended in a direction tilted with a predetermined angle from that perpendicular to the drive axis of the mass to which the beam is connected, a second pair of supporting beams mounted on the sense frame at one end, with the other ends connected to the other end of the first pair of beams to form a first and second joints respectively, a third pair of transfer beams connected to the first and second joints respectively at one end and joined together at the other end to form a third joint, the third joint being further mounted to the sense frame by a lateral spring extended in a predetermined direction for constraining the joint for movement perpendicular to that direction.

29. The angular rate sensor of claim 20 wherein means for driving the masses to oscillate in drive-mode includes comb drives mounted on at least one of the masses.

30. The angular rate sensor of claim 20 wherein the at least one input axis is the first, second, or third axis.

31. The angular rate sensor of claim 20 wherein the at least one input axis consists of two input axes, which are the first and second axes, the second and third axes, or the first and third axes.

32. The angular rate sensor of claim 20 wherein the at least one input axis consists of three input axes, which are the first, second, and third axes.