Counterbalanced triaxial multisensor with resonant accelerometers

• US 5,932,803 A
• Filed: 08/01/1997
• Issued: 08/03/1999
• Est. Priority Date: 08/01/1997
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Litton Systems Incorporated
• Inventors: Wyse, Stanley F.
• Primary Examiner(s): Williams, Hezron
• Assistant Examiner(s): Kwok, Helen C.
• Application Number:
  US08/904,923
• Time in Patent Office: 732 Days
• Field of Search: 73/510, 73/504.04, 73/504.12, 73/504.02, 73/504.03
• US Class Current: 73/504.04
• CPC Class Codes: G01C 19/5705 using masses driven in reciprocating rotary motion about an axis
• CPC Class Codes: G01C 19/5783 Mountings or housings not specific to any of the devices covered by groups G01C19/5607 - G01C19/5719

Abstract

A multisensor of the type that employs counteroscillating rotor-mounted accelerometers to measure both linear and Coriolis accelerations operates open loop to sense linear acceleration and closed loop to sense the Coriolis acceleration from angular rate inputs. Accelerometers mounted to arms of the counteroscillating rotors are designed so that the natural frequency of the proofmass with respect to the accelerometer frame closely approximates the resonant frequency ω_D of the driven rotor pair. A robust hinge design permits open loop operation for low frequency linear acceleration inputs without saturation. Low voltage closed-loop operation is made possible by the highly compliant nature of the resonant structure in responding to the much higher frequency Coriolis accelerations generated by angular rate inputs.

Claims

1. A multisensor comprising, in combination:

a) a pair of rotors, each of said rotors comprising a plurality of radially-directed rotor arms;

b) means for driving said rotors to counteroscillate at a resonant frequency ω

_D ;

c) an accelerometer assembly fixed to each of said rotor arms;

d) each of said accelerometer assemblies including an accelerometer having a substantially-planar proofmass, said proofmass being joined to a substantially-planar accelerometer frame by a hinge so that said proofmass may be angularly displaced with respect to the plane of said frame; and

e) each of said accelerometers being arranged so that a natural frequency of vibration of said proofmass is substantially the same as that of said resonant frequency ω

_D.

2. A multisensor as defined in claim 1 further including:

a) a means for measuring deflection of said proofmass; and

b) means for deriving linear acceleration in response to said measured deflection.

3. A multisensor as defined in claim 2 further including:

a) means for generating a force for nulling vibrations of said proofmass of frequency ω

_D ; and

b) means for measuring rotation rate in response to said force.

4. A multisensor as defined in claim 3 wherein said means for deriving linear acceleration further includes:

a) means for generating a voltage signal in response to deflection of said proofmass;

b) an amplifier for receiving said voltage signal; and

c) means responsive to measured linear acceleration for conditioning said voltage signal prior to application to said amplifier.

5. A multisensor as defined in claim 1 wherein said accelerometer further comprises:

a) said accelerometer frame having an internal rectangular aperture;

b) said proofmass being substantially rectangular and located within said aperture;

c) said hinge joining a side of said proofmass to a side of said aperture; and

d) said hinge being an integral member.

6. A multisensor as defined in claim 5 wherein said accelerometer further includes:

a) said accelerometer being of silicon; and

b) said proofmass and frame comprising an integral structure.

7. A multisensor as defined in claim 6 wherein said resonant frequency exceeds 2 kHz.

8. A multisensor as defined in claim 1 further including means for adjusting the natural frequency of said proofmass.

9. A multisensor as defined in claim 8 wherein said means for adjusting the natural frequency of said proofmass further comprises means for applying a d.c. bias voltage to said proofmass.

10. A multisensor as defined in claim 1 wherein said accelerometer assembly further includes:

a) an upper cover and a lower cover;

b) said upper and lower covers being fixed to opposed surfaces of said accelerometer; and

c) at least one electrode fixed to the surfaces of each of said upper and lower covers facing said accelerometer.

11. A multisensor as defined in claim 10 wherein electrodes are arranged in at least one aligned pair fixed to said surfaces of said upper and lower covers facing said accelerometer.

12. A multisensor as defined in claim 11 further including:

a) a first electrical circuit in electrical connection with a first electrode fixed to said upper cover and said aligned electrode fixed to said lower cover for applying equal and opposite d.c. bias voltages thereto;

b) a second electrical circuit for sensing angular vibration of said proofmass of frequency ω

_D and generating an a.c. voltage signal in response for nulling said vibration; and

c) said second electrical circuit being in electrical connection with said first circuit and with said aligned electrodes for applying said a.c. voltage signal thereto.

20. A multisensor as defined in claim 2 further including:

a) said accelerometer frame having an internal rectangular aperture;

b) said proofmass being substantially rectangular and located within said aperture;

c) said hinge joining an edge of said proofmass to an edge of said aperture; and

d) said hinge being an integral member.

21. A multisensor as defined in claim 20 further including means for electronically adjusting a natural frequency of said proofmass.

22. A multisensor as defined in claim 21 wherein said means for electronically adjusting the natural frequency of said proofmass includes means for applying a predetermined d.c. bias.

23. A multisensor as defined in claim 22 further characterized in that:

a) said d.c. bias comprises d.c. voltages of equal magnitude and opposite sign; and

b) said d.c. voltages are applied to said aligned electrodes fixed to said upper and lower covers.

13. A multisensor comprising, in combination:

a) a pair of rotors, each of said rotors comprising a plurality of radially-directed rotor arms;

b) means for driving said rotors to counteroscillate at a resonant frequency ω

_D ;

c) an accelerometer assembly fixed to each of said rotor arms;

d) each of said accelerometer assemblies including an accelerometer having a substantially-planar proofmass, said proofmass being joined to a substantially-planar accelerometer frame by a hinge so that said proofmass may be angularly displaced with respect to the plane of said frame and said hinge being of sufficient stiffness so that the natural frequency of said proof mass is substantially equal to ω

_D ;

e) means for generating a first signal in response to said angular displacement of said proofmass wherein said first signal provides a measure of linear acceleration; and

f) means for generating a second signal in response to said first signal for nulling displacements of said proofmass of frequency substantially equal to ω

_D.

14. A multisensor as defined in claim 13 further including:

a) means for conditioning said first signal;

b) an amplifier for receiving said conditioned signal; and

c) a low-pass filter for receiving the output of said amplifier and providing a measure of linear acceleration.

15. A multisensor as defined in claim 14 wherein said means for conditioning is responsive to said measure of linear acceleration.

16. A multisensor as defined in claim 15 wherein said accelerometer comprises an integral structure of silicon fabrication.

17. A multisensor as defined in claim 16 wherein said resonant frequency exceeds 2 kHz.

18. A multisensor as defined in claim 13 wherein said accelerometer assembly further includes:

a) an upper cover and a lower cover;

b) said upper and lower covers being fixed to opposed surfaces of said accelerometer; and

c) a plurality of electrodes being fixed to the surfaces of said upper and lower covers adjacent said accelerometer.

19. A multisensor as defined in claim 18 further including aligned electrodes fixed to said upper and lower covers in communication with said means for generating a first signal for detecting angular displacement of said proofmass and said means for generating a second signal for nulling displacements of said proofmass of said frequency.