Reduction of demodulator offset errors in fibre-optic gyroscopes

• US 5,131,749 A
• Filed: 12/06/1991
• Issued: 07/21/1992
• Est. Priority Date: 03/15/1989
• Status: Expired due to Term

• Current Assignee: Litef GmbH (Northrop Grumman Corporation)
• Original Assignee: British Aerospace, Inc. (BAE Systems Plc)
• Inventors: Varnham, Malcolm P.
• Primary Examiner(s): Turner, Samuel A.
• Application Number:
  US07/803,784
• Time in Patent Office: 228 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

A fibre optic gyroscope which reduces the sensitivity of the gyroscope to offsets in the demodulator, the reduction in sensitivity being achieved by modulating the radiation passing through the gyroscope by a first waveform which is derived from second and third periodic waveforms, the third waveform having a frequency substantially less than that of the second waveform in use and the second waveform having a frequency of about 1/2T where T is the time taken for the radiation to travel through the gyroscope, and detecting said radiation which is subsequently demodulated with respect to both second and third waveforms in order to minimize any offset introduced by the demodulation with respect to the second waveform.

Claims

1. A fibre-optic gyroscope comprising:

a light source;

a coil of optical fibre, connected to the light source for receiving light therefrom;

beam splitting/combining means for splitting light from the light source and directing it in opposite directions around the coil and then combining said light;

phase modulation means for modulating the phase of the light in the coil in accordance with a combined signal produced by combining a first signal at a first frequency with a second chopper signal at a frequency lower than the first frequency so as to produce a phase shift in the light passing through the coil;

a light detector for detecting the combined light passing from said coil and for producing an output signal;

a first rate demodulator for demodulating the output from the light detector so as to produce an output signal whose amplitude is a measure of the non-reciprocity occurring in the gyro as well as a dc signal of which part will be due to the offsets in the first rate demodulator;

second demodulation means for demodulating the output signal from the first demodulator at a frequency lower than the frequency at which the first demodulator operates so as to produce a signal whose amplitude is substantially unaffected by any dc signal due to the offsets in the second demodulator and is substantially a measure of the non-reciprocity occurring in the gyro.

2. A fibre-optic gyroscope as claimed in claim 1 in which the first signal has a frequency of 1/2T, where T is the time taken for light to pass around the coil, and has an amplitude such as to produce a phase shift of plus and minus π

/4 of the light passing through the modulator.

3. A fibre-optic gyroscope as claimed in claim 1 including inversion means for inverting the first signal in phase synchronously with the second, chopper, signal.

4. A fibre-optic gyroscope as claimed in claim 1 including a serrodyne voltage controller oscillator (VCO) for receiving an output signal from the second demodulation means and for generating a nulling signal to null the non-reciprocity in the gyro induced by rotation.

5. A fibre-optic gyroscope as claimed in claim 1 including a serrodyne voltage controller oscillator (VCO) for receiving an output signal from the second demodulation means and for generating a nulling signal to null the non-reciprocity in the gyro induced by rotation and in which the nulling signal is a serrodyne having a sawtooth waveform and amplitude of substantially 2 mpi, where m is the integer.

6. A fibre-optic gyroscope as claimed in claim 1 including a serrodyne voltage controller oscillator (VCO) for receiving an output signal from the second demodulation means and for generating a nulling signal to null the non-reciprocity in the gyro induced by rotation, the nulling signal being a serrodyne having a sawtooth waveform and amplitude of substantially 2 mpi, where m is the integer, and means for controlling the amplitude of the serrodyne waveform which is obtained from error pulses which occur synchronously with resets of the serrodyne.

7. A fibre-optic gyroscope as claimed in claim 6 including deriving means for deriving an error signal to correct the serrodyne amplitude by synchronous demodulation of the detector signal using reference signals derived by both dither and chopper waveforms.

8. A fibre-optic gyroscope as claimed in claim 1 in which the first and second demodulators are ac coupled.

9. A fibre-optic gyroscope as claimed in claim 1 including a gain between the first and second demodulation means.

10. A fibre-optic gyroscope as claimed in claim 1 in which the first and/or second demodulators implement demodulation digitally.

11. A fibre-optic gyroscope as claimed in claim 1 including a sample and hold device and a narrow band filter prior to the second demodulator.