Angular rate sensor utilizing two vibrating accelerometers secured to a parallelogram linkage

• US 4,510,802 A
• Filed: 09/02/1983
• Issued: 04/16/1985
• Est. Priority Date: 09/02/1983
• Status: Expired due to Term

• Current Assignee: L-3 Communications Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Sundstrand Data Control, Inc.
• Inventors: Peters, Rex B.
• Primary Examiner(s): Gill, James J.
• Application Number:
  US06/528,774
• Time in Patent Office: 592 Days
• Field of Search: 73/505, 73/510, 73/516 R, 73/517 R, 73/517 B
• US Class Current: 73/504.12
• CPC Class Codes: G01C 19/5776 Signal processing not specific to any of the devices covered by groups G01C19/5607 - G01C19/5719
• CPC Class Codes: G01P 15/14 by making use of gyroscopes gyroscopes per se G01C19/00

Abstract

In an inertial system for sensing the angular rotation and translational motion of a structure utilizing a pair of accelerometers in a back-to-back arrangement vibrating substantially linearly along an axis normal to their force sensing axes, a mechanism utilizing a parallelogram structure is used to impart the vibratory motion to the accelerometers.

Claims

1. An apparatus for generating a signal representing the angular rate motion of a structure comprising:

a first accelerometer having a first force sensing axis;

a second accelerometer having a second force sensing axis;

a parallelogram mechanism including a first accelerometer support member secured to said first accelerometer, a second accelerometer support member secured to said second accelerometer and a linkage mechanism attached to said first and said second accelerometer support members and secured to the structure such that said first and said second force sensing axes are aligned in parallel;

drive means operatively connected to said parallelogram mechanism for vibrating said first and second accelerometer support members in a direction substantially normal to said first and second force sensing axes at a frequency ω

; and

signal processing means operatively connected to said first and second accelerometers for generating a rate signal representing the angular rate motion of the structure.

2. The apparatus of claim 1 wherein said linkage mechanism includes a first linkage member pivotably connected to said first and second accelerometer support members, a second linkage member pivotably connected to said first and second accelerometer support members and a central support member secured to the structure and pivotably connected to said first and second linkage members.

3. The apparatus of claim 2 wherein said drive means includes a first electromagnetic drive member secured to said central support member and a second electromagnetic drive member secured to said first linkage member.

4. The apparatus of claim 2 wherein said first and second linkage members are pivotably connected to said first and second accelerometer support members by flexures.

5. The apparatus of claim 4 wherein said central support member is pivotably connected to said first and second linkage members by flexures.

6. The apparatus of claim 1 wherein said drive means vibrates said first and second accelerometers through an angle θ

of 0.01-0.1 radians.

7. The apparatus of claim 1 wherein said frequency ω

is a constant frequency of 200-400 radians per second.

8. The apparatus of claim 11 wherein said first and second accelerometers are vibrating through an angle θ

offset by an angle Ψ

from a nominal position and wherein said drive means includes adjustment means for adjusting the offset angle Ψ

to a desired value.

9. The apparatus of claim 1 wherein said drive means includes phase control means for adjusting the phase of the vibration of said first and second accelerometers.

10. The apparatus of claim 1 wherein said drive means includes:

a periodic signal generator circuit for generating an output signal having the frequency ω

;

an amplifier circuit operatively connected to said periodic signal generator for amplifying the output of said periodic signal generator;

a drive element operatively connected to said parallelogram mechanism and responsive to said amplified periodic signal for vibrating said first and second accelerometers at said frequency ω

; and

feedback means responsive to the position of said parallelogram mechanism for applying a feedback signal to said amplifier circuit to control the amplitude θ

of the vibration of said first and second accelerometers.

11. The apparatus of claim 10 additionally including adjustment means for adjusting an offset angle Ψ

representing the deviation from a nominal position of the vibration θ

, to a desired value.

12. The apparatus of claim 11 wherein said adjustment means includes a voltage supply circuit for applying an adjustable voltage to said amplifier circuit.

13. The apparatus of claim 10 additionally including a phase control circuit operatively connected to said periodic signal generator effective to vary the phase of the frequency ω

at which said first and second accelerometers are vibrated.

14. An angular rate sensing accelerometer structure comprising:

a central support member;

a first linkage member pivotably connected to one end of said central support member;

a second linkage member pivotably connected to the other end of said central support member;

a first accelerometer support member pivotably connected to one end of each of said first and second linkage members;

a first accelerometer secured to said first accelerometer support member such that its force sensing axis is generally normal to said first accelerometer support member;

a second accelerometer support member pivotably connected to said other end of each of said linkage members; and

a second accelerometer secured to said second accelerometer support member such that its force sensing axis is generally normal to said first accelerometer support member and generally parallel to the force sensing axis of said first accelerometer.

15. The structure of claim 14 wherein the force sensing axes of said first and second accelerometers are generally parallel to said first and second linkage members.

16. The structure of claim 15 wherein the force sensing axes of said first and second accelerometers are in opposite directions.

17. The structure of claim 14 wherein said first and second linkage members are connected to said central support member by flexures.

18. The structure of claim 17 wherein said first and second linkage members are connected to said first and second accelerometer support members by flexures.

19. The structure of claim 14 additionally including a drive mechanism operatively connected to said central support member and said first lineage member for vibrating said first and second accelerometer support members at a frequency ω

.

20. The apparatus of claim 19 wherein said drive mechanism includes a first electromagnetic drive member secured to said support member and a second electromagnetic drive member secured to said first linkage member.

21. The apparatus of claim 19 wherein said frequency ω

is a constant frequency of 200-400 radians per second.

22. The apparatus of claim 21 wherein said drive mechanism vibrates said first and second accelerometers through an angle θ

of 0.01-0.1 radians.

23. A drive signal generator circuit for vibrating at least one accelerometer in an inertial measurement system at a frequency ω

comprising;

a periodic signal generator circuit for generating an output signal having the frequency ω

;

an amplifier circuit operatively connected to said periodic signal generator circuit for amplifying the output of said periodic signal generator;

a drive element operatively connected to said accelerometer and responsive to said amplified periodic signal for vibrating the accelerometer at frequency ω

; and

feedback means responsive to the position of the accelerometer for applying a feedback signal to said amplifier circuit to control the amplitude of the vibration.

24. The circuit of claim 23 additionally including adjustment means for adjusting the position of the center point about which the accelerometer vibrates.

25. The circuit of claim 24 wherein said adjustment means includes a voltage supply circuit for applying an adjustable voltage to said amplifier circuit.

26. The circuit of claim 23 additionally including a phase control circuit operatively connected to said periodic signal generator effective to vary the phase of the frequency ω

at which the accelerometer is vibrated.

27. A drive signal generator circuit for vibrating at least one accelerometer at a frequency ω

in an inertial measurement system comprising;

a pulse generator for generating pulses at a frequency that is a function of ω

;

a sine wave generator circuit connected to said pulse generator and responsive to said pulses for generating a sinusoidal drive signal for a frequency ω

;

a high gain amplifier circuit connected to said sine wave generator for amplifying said sinusoidal drive signal;

a drive element operatively connected to the accelerometer and said high gain amplifier and responsive to said amplified drive signal to vibrate the accelerometer at a frequency ω

;

feedback means including a position element for generating a feedback signal indicating the amplitude of accelerometer vibration and for applying said feedback signal to said high gain amplifier; and

a vibration phase control circuit operatively connected to said sine wave generator.

28. A drive signal generator circuit for vibrating at least one accelerometer at a frequency ω

in an inertial measurement system comprising;

a pulse generator for generating pulses at a frequency that is a function of ω

;

a sine wave generator circuit connected to said pulse generator and responsive to said pulses for generating a sinusoidal drive signal for a frequency ω

;

a high gain amplifier circuit connected to said sine wave generator for amplifying said sinusoidal drive signal;

a drive element operatively connected to the accelerometer and said high gain amplifier and responsive to said amplified drive signal to vibrate the accelerometer at a frequency ω

;

feedback means including a position sensing element for generating a feedback signal indicating the amplitude of accelerometer vibration and for applying said feedback signal to said high gain amplifier; and

an adjustment circuit operatively connected to said high gain amplifier circuit for applying a voltage to said high gain amplifier circuit for adjusting the position of the center point about which the accelerometer vibrates.