Fiber optic gyroscope with variable output period

• US 5,949,545 A
• Filed: 09/11/1997
• Issued: 09/07/1999
• Est. Priority Date: 05/23/1996
• Status: Expired due to Fees

• Current Assignee: L-3 Communications Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Inventors: Kovacs, Robert A., Lo, Pei-Hwa
• Primary Examiner(s): Turner, Samuel A.
• Application Number:
  US08/928,037
• Time in Patent Office: 726 Days
• Field of Search: 356/350
• US Class Current: 356/464
• CPC Class Codes: G01C 19/726 Phase nulling gyrometers, i.e. compensating the Sagnac phase shift in a closed loop system

Abstract

The linearity of a fiber optic gyroscope can be improved by dithering the gyroscope'"'"'s feedback signal. An output signal can be taken over any time interval by sampling the feedback signal before dithering is applied.

Claims

1. A system, comprising:

a fiber optic gyroscope for sensing angular rate comprising

a light source for generating a light output;

a splitter/modulator for splitting the light output into two beams, modulating one of the beams, and recombining the two beams;

a fiber optic sense coil for directing one of the beams in a clockwise direction through the fiber optic sense coil and the other of the beams in a counterclockwise direction through the fiber optic sense coil; and

a detector for detecting the recombined beams and providing an output proportional to the magnitude of the recombined beams; and

a processor for generating a feedback signal and an output signal, comprising

first ramp generator means, responsive to the output of the detector, for generating a feedback signal proportional to the phase difference between the clockwise and the counterclockwise beams, where the feedback signal assumes a steady-state operating point for any given angular rate;

a biasing function generator for shifting the steady-state operating point of the feedback signal;

a dither pattern generator for generating a waveform for continuously oscillating the feedback signal about the instantaneous value of the operating point;

means for providing the feedback signal to the splitter/modulator;

second ramp generator means, responsive to the output of the detector, for generating a signal proportional to the phase difference between the clockwise and the counterclockwise beams, where the signal assumes a steady-state operating point for any given angular rate; and

output processing means, responsive to the signal generated by the second ramp generator means, for generating an output signal.

2. A system as set forth in claim 1, where the dither pattern generator includes means for generating a symmetrical waveform.

3. A system as set forth in claim 1, where the dither pattern generator includes means for generating a triangular waveform or a digital stair-step ramp approximating a triangular waveform.

4. A system as set forth in claim 1, further including means for adding a compensation signal to the output of the detector to remove the component of the output introduced by the dither pattern generator.

5. A system as set forth in claim 4, where the compensation signal is a square wave having the same frequency and phase as the output of the dither pattern generator.

6. A signal processor for generating a feedback signal and an output signal in response to the output of a rate-sensing fiber optic gyroscope comprising a light source for generating a light output;

a splitter/modulator for splitting the light output into two beams, modulating the beams in response to the feedback signal, and recombining the two beams;

a fiber optic sense coil for directing one of the beams from the splitter/modulator in a clockwise direction through the fiber optic sense coil and the other of the beams in a counterclockwise direction through the fiber optic sense coil; and

a detector for detecting the recombined beams and providing an output proportional to the magnitude of the recombined beams;

the signal processor comprising;

first ramp generator means, responsive to the output, for generating a feedback signal proportional to the phase difference between the clockwise and the counterclockwise beams, where the feedback signal assumes a steady-state operating point for any given angular rate;

a biasing function generator for shifting the steady-state operating point;

a dither pattern generator for generating a waveform for continuously oscillating the feedback signal about the instantaneous value of the operating point;

means for providing the feedback signal to the splitter/modulator;

second ramp generator means, responsive to the output of the detector, for generating a signal proportional to the phase difference between the clockwise and the counterclockwise beams, where the signal assumes a steady-state operating point for any given angular rate; and

output processing means, responsive to the signal generated by the second ramp generator means, for generating an output signal.

7. A system as set forth in claim 6, where the dither pattern generator includes means for generating a symmetrical waveform.

8. A system as set forth in claim 6, where the dither pattern generator includes means for generating a triangular waveform or a digital stair-step ramp approximating a triangular waveform.

9. A system as set forth in claim 6, further including means for adding a compensation signal to the output of the detector to remove the component of the output introduced by the dither pattern generator.

10. A system as set forth in claim 9, where the compensation signal is a square wave having the same frequency and phase as the output of the dither pattern generator.

11. A method of sensing angular rate in a fiber optic gyroscope comprising a fiber optic sense coil, comprising the steps of:

generating a light output;

splitting the light output into two beams;

directing one of the beams in a clockwise direction through the fiber optic sense coil and the other of the beams in a counterclockwise direction through the fiber optic sense coil;

recombining the two beams;

detecting the recombined beams and providing an output proportional to the magnitude of the recombined beams; and

in response to the output, generating a feedback signal and modulating one of the light beams in response to the feedback signal, the step of generating a feedback signal including the steps of;

generating a feedback signal proportional to the phase difference between the clockwise and the counterclockwise beams, where the feedback signal assumes a steady-state operating point for any given angular rate;

shifting the steady-state operating point; and

continuously oscillating the feedback signal about the instantaneous value of the operating point;

in response to the output, generating a second signal proportional to the phase difference between the clockwise and the counterclockwise beams, where the second signal assumes a steady-state operating point for any given angular rate; and

in response to the step of generating a second signal, generating an output signal.

12. A method as set forth in claim 11, where step of continuously oscillating the feedback signal about the instantaneous value of the operating point includes the step of generating a symmetrical waveform.

13. A method as set forth in claim 11, where step of continuously oscillating the feedback signal about the instantaneous value of the operating point includes the step of generating a triangular waveform or a digital stair-step ramp approximating a triangular waveform.

14. A method as set forth in claim 11, further including the step of adding a compensation signal to the output to remove the component of the output introduced by the step of continuously oscillating the feedback signal about the instantaneous value of the operating point.

15. A system as set forth in claim 14, where the compensation signal is a square wave having the same frequency and phase as the dither signal.

16. An apparatus for reducing non-linearity in a closed-loop fiber optic gyroscope for sensing applied angular rate, comprising:

means for generating a feedback signal proportional to the applied angular rate;

means for continuously oscillating the feedback signal about the instantaneous value of the operating point; and

means for extracting the feedback signal prior to the means for continuously oscillating the signal.

17. A method of reducing non-linearity in a closed-loop fiber optic gyroscope for sensing applied angular rate, comprising the steps of:

generating a feedback signal proportional to the applied angular rate;

continuously oscillating the feedback signal about the instantaneous value of the operating point; and

extracting the feedback signal prior to oscillating the signal about the operating point.