Method and apparatus for controlling dither in a multiple gyro system

• US 5,331,401 A
• Filed: 06/03/1985
• Issued: 07/19/1994
• Est. Priority Date: 06/03/1985
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Litton Systems Incorporated
• Inventors: Tazartes, Daniel A., Dykeman, Ray D., Ware, William B., Mark, John G.
• Primary Examiner(s): Buczinski, Stephen G.
• Application Number:
  US06/740,731
• Time in Patent Office: 3,333 Days
• Field of Search: 356/350, 372/94, 73/504, 74/5.6 A, 74/5.6 D
• US Class Current: 356/475
• CPC Class Codes: G01C 19/664 means for removing the dither signal
• CPC Class Codes: Y10T 74/1264 Optical

Abstract

A method and apparatus for controlling dither in a multiple gyro system. Each gyro is driven at a distinct nominal frequency. The resulting gyro motions are measured, then demodulated to determine their cross-axis frequency content. Virtual drive signals are generated in light of the cross-axis interactions, then combined with the nominal drive frequencies in such a way that the measured cross-axis effects, resulting in either signal intermodulation or block coning, are nulled.

Claims

1. A method for controlling cross-coupling in a navigation system of the type wherein a plurality of gyroscopes is dithered about a plurality of axes of rotation with respect to an instrument block, said method comprising the steps of:

a) driving each of said gyroscopes at a distinct frequency whereby a predetermined drive frequency is associated with an axis of rotation;

then

b) measuring the resulting rotations;

then

c) demodulating said resulting rotations to determine the cross-axis frequency content of each;

then

d) deriving virtual drive signal components for each axis at said cross-axis frequencies;

then

e) combining said virtual drive signal components with said predetermined frequency for each axis to create a new drive signal for each axis;

then

f) driving said gyroscopes with said new drive signals; and

then

g) repeating steps a through f above.

2. A method as defined in claim 1 further characterized in that said distinct frequencies are separated by the inverse of the rotation sampling period.

3. A method as defined in claim 2 wherein the demodulating step further includes the step of deriving the Fourier series expansion coefficients of the cross-axis frequencies.

4. A method as defined in claim 3 wherein the step of deriving virtual drive signal components is further characterized by:

a) calculating the response of said gyroscopes to the cross axis drive frequencies;

then

b) creating output-input models of said response for each of said gyroscopes; and

then

c) applying said Fourier series coefficients to said model.

5. A method as defined in claim 4 further characterized by dithering three gyroscopes about three orthogonal axes.

6. A method as defined in claim 5 wherein the step of measuring the resulting rotations comprises measuring the gyroscope pickoff signals.

7. A method as defined in claim 5 wherein the step of measuring the resulting rotations comprises measuring the block motion.

8. Apparatus for controlling cross-coupling in a navigation system of the type wherein a plurality of gyroscopes is dithered about a plurality of axes with respect to an instrument block wherein the improvement comprises:

a) means for driving each of said gyroscopes at a distinct frequency;

b) means for generating a signal responsive q to the resulting movement of each of said gyroscopes;

c) means for demodulating each of said signals to determine the cross-axis frequency content thereof;

d) means for deriving virtual drive signal components at said cross-axis frequencies; and

e) means for combining said virtual drive signal components with said distinct frequencies.

9. Apparatus as defined in claim 8 wherein said means for driving each of said gyroscopes at a distinct frequency comprises a plurality of digital oscillators.

10. Apparatus as defined in claim 9 wherein said means for demodulating said signals includes means for determining the Fourier series expansion coefficients of the cross-axis frequencies in said signals responsive to the movements of said gyroscopes.

11. Apparatus as defined in claim 10 wherein said means for deriving virtual drive signal components includes an output-input model of the frequency response of the gyroscopes to the cross-axis frequencies.

12. Apparatus as defined in claim 11 wherein said means for generating a signal comprises a gyroscope pickoff.

13. Apparatus as defined in claim 11 wherein said means for generating comprises:

a) a gyroscope pickoff; and

b) means for subtracting the output of said pickoff from gyro output.