Dual cavity laser gyro

Optics: measuring and testing – By dispersed light spectroscopy – Utilizing a spectrometer

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G01C 1964

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045211108

ABSTRACT:
A laser gyro having two cavities which are physically separated so that neither mode volumes have any common parts. Each cavity supports a wave traveling in only one direction either clockwise or counter-clockwise. Other waves, which are normally set up in a ring laser gyro, are prevented by a reversed feedback mirror. The gyro produces two waves whose frequencies are shifted in opposite directions by rotation. Lock-in is not possible. The two frequencies are mixed and the beat frequency is detected by optical heterodyne techniques. The response of this rotation sensor is linear down to zero rotation rate and its accuracy is limited by quantum effects.

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patent: 4120587 (1978-10-01), Vali et al.
patent: 4219275 (1980-08-01), Henry
patent: 4429398 (1984-01-01), Chenausky et al.
Honeycutt et al., "FM-CW Radar Range Measurement with a CO.sub.2 Laser", E Journal of Quantum Electronics, vol. QE-8, No. 2, pp. 91-21, Feb. 1972.
Matthews et al., "A High Resolution Laser Gyro," National Aerospace and Electronics Conference, (Preprint, pp. 1-13), May 16-18, 1978.
Dorschner et al., "A Manganese Bismuth Magnetic Mirror for the Raytheon Laser Gyro," National Aerospace and Electronics Conference, (5 pages), May 16-18, 1978.
Smith et al., "Biasing the Raytheon Four-Frequency Ring Laser Gyroscope," SPIE Vol. 157, Laser Inertial Rotational Sensors, (1978), pp. 21-29.
Dorschner et al., "Laser Gyro at Quantum Limit", IEEE Journal of Quantum Electronics, vol. QE-16, No. 12, Dec. 1980, pp. 1376-1379.

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