Axis aligned rate and acceleration sensor

• US 5,886,259 A
• Filed: 04/01/1996
• Issued: 03/23/1999
• Est. Priority Date: 04/01/1996
• Status: Expired due to Term

• Current Assignee: L-3 Communications Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Alliedsignal Inc.
• Inventors: Hulsing, Rand H. II
• Primary Examiner(s): Oda, Christine K.
• Application Number:
  US08/626,306
• Time in Patent Office: 1,086 Days
• Field of Search: 73/504.04, 73/514.38, 73/514.18, 73/514.29, 73/504.12, 73/510, 73/504.02, 73/514.37
• 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

An angular rate sensor that utilizes the Coriolis effect and which includes two dithered accelerometers having proof masses suspended by a hinge fabricated out of a Silicon substrate, the proof masses are provided with support struts that can be adjusted by applying heat to the struts to compensate for misalignment of the proof masses along the dither axis. In one embodiment, the hinges are located on the same side of the substrate and a vibrating beam force transducers are connected between each of the proof masses and associated accelerometer frames in a push-pull arrangement.

Claims

1. An angular rate sensor comprising:

a support structure;

a generally planar substrate, having an angular rate sensing axis and a dither axis normal to each other and parallel to a plane of said substrate, secured within said support structure;

a mounting frame formed in said substrate;

a first and a second accelerometer formed in said substrate wherein each said accelerometer includes an accelerometer frame, a proof mass located within said accelerometer frame, a hinge attaching a first end of said proof mass to said accelerometer frame in order to permit at least limited angular rotation of said proof mass with respect to said accelerometer frame in response to acceleration in a force sensing axis normal to the plane of said substrate wherein said first and second proof masses are located on each side of and in parallel to said angular rate sensing axis, a first strut connecting a second end of said proof mass to said accelerometer frame, and a force detector connected between said proof mass and said accelerometer frame;

a plurality of frame flexures connecting said first and second accelerometer frames to said mounting frame;

dither means for dithering said first and second accelerometers along said dither axis at a frequency ω

;

processing means responsive to said first and second force detectors for generating a signal representing angular rotation of the sensor around said angular rate sensing axis, said processing means including means for generating a misalignment signal; and

means, responsive to said misalignment signal, for applying an alignment force to said first and second proof masses, said alignment force aligning each of said proof masses with said dither axis.

2. The sensor of claim 1 additionally including a link formed in said substrate, said link connecting said first and second accelerometers.

3. The sensor of claim 1 wherein said first accelerometer frame is connected to said mounting frame by a first one of said frame flexures attached to a first side of said mounting frame and to a first side of said accelerometer frame and a second one of said frame flexures is attached to a second side of said mounting frame and to a second side of said accelerometer frame.

4. The sensor of claim 1 wherein said force detector of said first accelerometer includes a first force sensing transducer for measurin the angular rotation of said first proof mass relative to said first accelerometer frame and said force detector of said second accelerometer includes a second force sensing transducer for measuring the angular rotation of said second proof mass relative to said second accelerometer frame.

5. The sensor of claim 4 wherein said force sensing transducers each include dual vibrating beams.

6. The sensor of claim 4 wherein said first and said second force sensing transducers are connected to said first and second proof masses so as to provide for a push-pull operation of said force sensing transducers.

7. The sensor of claim 6 wherein said first force sensing transducer is connected to a portion of said first proof mass located toward said second end of said proof mass away from said first hinge and wherein said force sensing transducer of said second accelerometer is connected to a portion of said second proof mass located towards said second end of said proof mass away from said second hinge.

8. The sensor of claim 7 wherein said first and second force sensing transducers each include dual vibrating beams.

9. The sensor of claim 1 wherein said alignment force applying means applies said alignment force though said first struts.

10. The sensor of claim 9 wherein said alignment force applying means includes a heater for applying heat to said first struts.

11. The sensor of claim 10 wherein said beater includes current means for selectively applying an electric current to said first struts.

12. The sensor of claim 11 wherein said first struts include an epitaxial material for conducting said current.

13. The sensor of claim 11 wherein said first struts include a Ni-Cr resistor for generating heat in response to said current.

14. The sensor of claim 11 wherein said current means includes misalignment means for generating misalignment signals representing a misalignment of said first and second proof masses with said dither axis.

15. The sensor of claim 14 wherein said misalignment means is responsive to a first and a second acceleration signal generated by said first and second force detecting means respectively and a signal equal to SGN (sin ω

t) where SGN represents the "sign of" and t represents time.

16. The sensor of claim 1 wherein each of said first and second accelerometers includes a second strut connecting said second end of said proof masses to said first and second accelerometer frames.

17. The sensor of claim 16 wherein said first and second struts are connected to approximately the center of said second ends of said first and second proof masses.

18. The sensor of claim 17 wherein said first and second struts are substantially parallel to said dither axis and are connected to a first and second side of said first and second accelerometer frames.

19. The sensor of claim 18 wherein said alignment force applying means selectively applying a torsional alignment force trough at least one of said first and second struts to each of said proof masses.

20. An angular rate sensor comprising:

a support structure;

a generally planar substrate, having an angular rate sensing axis and a dither axis normal to each other and parallel to a plane of said substrate, secured within said support structure;

a mounting frame formed in said substrate;

a first accelerometer formed in said substrate, located within said mounting frame on a first side of said angular rate sensing axis, including a first accelerometer frame, a first proof mass located within said first accelerometer frame, a first hinge attaching a first end of said first proof mass to said first accelerometer frame to permit at least limited angular rotation of said first proof mass with respect to a plane of said first accelerometer frame in response to acceleration along a force sensing axis normal to the plane of said substrate, a first suspension member connecting a second end of said first proof mass to said first accelerometer frame and first force detector connected between said first proof mass and said first accelerometer frame;

a first frame flexure connecting said first accelerometer frame to said mounting frame;

a second accelerometer formed in said substrate, located within said mounting frame on a second side of said angular rate sensing axis, including a second accelerometer frame, a second proof mass located within said second accelerometer frame, a second hinge attaching a first end of said second proof mass to said second accelerometer frame to permit at least limited angular rotation of said second proof mass with respect to a plane of said second accelerometer frame in response to acceleration along said force sensing axis, a second suspension member connecting a second end of said second proof mass to said second accelerometer frame and a second force detector connected between said second proof mass and said second accelerometer frame;

a second frame flexure connecting said second accelerometer frame to said mounting frame;

a link formed in said substrate connecting said first accelerometer to said second accelerometer;

dither means for dithering said first and second accelerometers along said dither axis at a frequency ω

;

processing means responsive to said first and second force detecting means and said dither means for generating an angular rotation signal representing the angular rotation of the sensor around said angular rate axis, and a misalignment signal; and

means, coupled to receive said misalignment signal, for selectively applying an alignment force in response to said misalignment signal to each of said first and second proof masses, said alignment force aligning each of said first and second proof masses along said dither axis.

21. The sensor of claim 20 wherein each of said first and second suspension members includes a first strut and second strut each of which are connected to said second ends of said first and second proof masses and to said first and second accelerometer frames, respectively.

22. The sensor of claim 20 wherein said first and second hinges are disposed toward a first side of said mounting frame.

23. The sensor of claim 21 wherein said alignment force applying means applies said alignment force through at least one of said first and second members.

24. The sensor of claim 23 wherein said alignment force applying means increases a length of at least one of said first and second struts to create said alignment force.

25. The sensor of claim 24 wherein said alignment force applies heat to at least one of each of said first and second struts to increase the length of said heated struts.

26. The sensor of claim 25 wherein said alignment force applying means is responsive to said first and second force detector and said dither means to generate a misalignment signal and wherein said heat is applied to said a struts in response to said misalignment signal.

27. The sensor of claim 20 wherein said substrate is composed of silicon.

28. The sensor of claim 23 wherein said first and second hinges are disposed toward a first side of said mounting frame.

29. The sensor of claim 28 wherein said first and second force detectors include a dual vibrating beam force transducers first and second proof masses and said first and second accelerometer frames.

30. A sensor comprising:

a support structure;

a mounting frame secured in said support structure;

a first planar proof mass;

first suspension means including a first hinge for connecting said first proof mass to said mounting frame such that a plane of said proof mass is generally maintained parallel to both a first axis and a second axis which are normal to each other and is permitted by said hinge at least limited angular rotation with respect to said first axis in response to acceleration along a force sensing axis normal to both said first axis and said second axis;

alignment force applying means for applying a first alignment force to said first proof mass through said first suspension means to maintain said proof mass in planar alignment with said second axis; and

wherein said alignment force applying means includes a first misalignment signal means for generating a first misalignment signal and wherein said alignment force applying means generates said first alignment force in response to said first misalignment signal.

31. The sensor of claim 30 wherein said first suspension means includes a first strut member and said alignment force means applies said first alignment force through said first strut member to said first proof mass.

32. The sensor of claim 31 wherein said alignment means applies said first alignment force to said proof mass by increasing a length of said first strut member.

33. The sensor of claim 32 wherein said alignment force applying means applies heat to said first strut member to increase length of said first strut member.

34. The sensor of claim 31 wherein the sensor includes a dither means for dithering said first proof mass along said second axis at a frequency ω

and a first force detecting means for measuring the angular rotation of said first proof mass and wherein said first misalignment signal means is responsive to both said dither means and said first force detecting means for generating a first misalignment signal and wherein said alignment_-- force applying means generates said first alignment force in response to said first misalignment signal.

35. The sensor of claim 31 wherein said sensor includes a second planar proof mass, a second suspension means including a second hinge and a second strut member for connecting said second proof mass to said mounting frame and for generally maintaining said second proof mass in parallel with both said first axis and said second axis and permitting said second proof mass to angularly rotate with respect to said first axis in response to acceleration along said force sensing axis and wherein said alignment means applies a second alignment force though said second strut member to said second proof mass to maintain said second proof mass in p alignment with said second axis.

36. The sensor of claim 35 wherein said sensor is an angular rate sensor and includes dither means for dithering said first and second proof masses along said second axis, first and second force detecting means for generating first and second output signals measuring the angular rotation of said first and second proof masses respectively and wherein said sensor includes processing means responsive to said dithering means and said first and second force detecting means for generating a rate signal representing the angular rotation of the sensor around said first axis.

37. The sensor of claim 36 wherein said first and second proof masses are configured out of silicon.

38. The sensor of claim 36 wherein said first and second force detecting means are connected to said first and second proof masses in a push-pull arrangement.

39. The sensor of claim 36 wherein said first and second proof masses are dithered at a frequency ω

and said alignment force applying means generates said first and second alignment forces as a function of ω and

the output signals of said first and second force detecting means.

40. The sensor of claim 39 wherein said alignment force applying means includes a demodulator for demodulating said first and second output signals as a function of SGN(sin ω

t) to produce a first and second misalignment signal which respectively generate said first and second alignment forces.