Ring laser gyro

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

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372 94, G01B 902, G02F 109, H01S 3083

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active

053715900

ABSTRACT:
A ring laser gyro uses a composition for the gain medium which optimizes the effect of the Fresnel-Fizeau drag on the output signal of the gyro. In one embodiment, a composition of the gain medium is used which produces no change in the Fresnel-Fizeau component of the output signal as the discharge current varies from a nominal amount. In another embodiment, a gain medium composition is used which eliminates the Fresnel-Fizeau component of the output signal at a predetermined level of discharge current.

REFERENCES:
patent: 3744908 (1973-07-01), Podgorski
patent: 4158821 (1979-06-01), Bresman
patent: 4329057 (1982-05-01), Zampiello
patent: 4470701 (1984-09-01), Smith
patent: 4481635 (1984-11-01), Broberg et al.
Technical Report AFWAL-TR-80-1174, "Ring Laser Gyro Technology for Advanced Aircraft Navigation (Phase II)", J. B. Matthews et al; Raytheon Company, Nov. 1980; pp. 48-60.
DTIC Technical Abstract Bulletin No. 81-18; Aug. 28, 1981; No. AD-B952 517; p. 35.
IEEE Journal of Quantum Electronics, vol. QE-4, No. 1, Jan. 1968 "Langmuir Flow Effects in the Laser Gyro" Ted J. Podgorski and Frederick Aronowitz, pp. 11-18.
Optical Engineering, vol. 18 No. 4, Jul.-Aug. 1979 "Dispersion and gas flow effects in the ring laser gyro" F. Aronowitz and W. L. Lim, pp. 376-380.
F. Aronwitz, "Single-Isotape Laser Gyro", Feb. 1972, pp. 405-412, Appl. Opt., vol. 11, #2.

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