Abstract
In Chapter 11 we defined the ring laser gyroscope (RLG) as an active resonator optical gyro. Clifford Heer conceived the RLG in 1961 [1]; he saw that the properties of the laser, recently invented by Schawlow and Townes, could be exploited to measure rotation. Heer and Adolph Rosenthal [2] independently developed the theory, and, in 1963, Macek and Davis [3] demonstrated the first RLG, a square gyro, 1 m on a side. Scientists around the world contributed to the field during the 1970s, and Bogdanov’s survey article [4] describes the results.
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References
Heer, C.V., “Interference of electromagnetic and matter waves in a nonpermanent gravitational field,” Bull. Am. Phys. Soc. 6, 58, Jan. 1961.
Rosenthal, A.H., “Regenerative circulatory multiple-beam interferometry for the study of light propagation effects,” J. Opt. Soc. Am., 52, 10, pp. 1143–1148, Oct. 1962.
Macek, W.M., D.T.M. Davis, “Rotation rate sensing with traveling-wave ring lasers,” Appl. Phys. Lett., 2, 3, pp. 67–68, 1 Feb. 1963.
Bogdanov, A.D., “Laser gyroscopes,” NASA TT F-15, 641, June 1974.
Aronowitz, F., “The laser gyro,” Laser Applications, Monte Ross (Ed.), Volume 1, Academic Press, New York, 1971.
Fowles, G.R., Introduction to Modern Optics, Holt, Rinehart, and Winston, Inc., New York, 1968.
Yariv, A., Introduction to Optical Electronics, Holt, Rinehart, and Winston, Inc., New York, Chapter 7, 1971.
Matthews, A., H. Welter, “Cost-effective, high-accuracy inertial navigation,” Navigation, J. Inst. Nay., 36, 2, pp. 157–172, Summer 1989.
Shackleton, B.R., “Mechanical design considerations for a ring laser gyro dither mechanism,” Mechanical Technology of Inertial Devices, Proc. Inst. Mech. Eng. (London), 1987–2, Paper C60/87.
Hammons, S.W., V.J. Ashby, “Mechanically dithered RLG at the quantum limit,” IEEE NAECON Record, Vol. 1, pp. 388–392, 1982.
Podgorski, T.J., “Control apparatus,” U.S. Patent 3 390 606, 2 July 1968.
Killpatrick, J., “The laser gyro,” IEEE Spectrum, pp. 44–55, Oct. 1967.
Tahara, Y., Y. Takizawa, H. Nakayasu, M. Otsuki, Y. Kojima, Y. Uehara, “Development of a space-use ring laser gyroscope in Japan,” DGON Symposium Gyro Technology, Stuttgart, 1985.
Lim, W.L, J.P. Hauck, J.W. Raquet, “Pentagonal ring laser gyro design,” U.S. Patent 4 705 398, 10 Nov. 1987.
Kerr, J., “On rotation of the plane of polarization by reflection from the pole of a magnet,” Phil. Mag., 3, ser. 5, pp. 321–342, May 1877.
Krebs, J.J., W.G. Maisch, G.A. Prinz, D.W. Forester, “Applications of magneto-optics in ring laser gyroscopes,” IEEE Trans. on Magnetics, MAG-16, 5, pp. 1179–1184, Sept. 1980.
Gauert, R., “Investigations of magneto-optic bias elements for laser gyros,” DGON Symposium Gyro Technology, Stuttgart, 1981.
Morrison, R.F., C.B. Strang, “A missile laser gyro rate sensor,” AIAA Guidance and Control Conference, 16–18 Aug. 1976.
Morrison, R.F., E. Levinson, R.W. McAdory, “The SLIC-15 laser gyro IMU for midcourse missile guidance,” Institute of Navigation, April 1976.
Hughes, D., “Northrop develops miniature laser gyros for tactical missiles,” Aviation Week and Space Technology, pp. 77–78, 8 Feb. 1988.
Perlmutter, M.S., J.M. Bresman, H.A. Perkins, “A low cost tactical ring laser gyroscope with no moving parts,” DGON Symposium Gyro Technology, Stuttgart, 1990.
Bresman, J., H. Cook, D. Lysobey, “Differential laser gyro development,” Navigation, J. Inst. Nay., 24, 2, pp. 153–159, Summer 1977.
Andringa, K., “Laser gyroscope,” U.S. Patents 3 741657, 26 June 1973, and 3 854 819, 17 Dec. 1974.
Yntema, G.B., D.C. Grant, R.T. Warner, “Differential laser gyro system,” U.S. Patent 3 862 803, 28 Jan. 1975.
Dorschner, T.A., I.W. Smith, “Clear-path four-frequency resonators for ring laser gyros,” J. Opt. Soc., 68, p.1381, 1978.
Simms, G.J., “Ring laser gyroscopes,” U.S. Patent 4 407 583, 4 Oct. 1983.
Simms, G.J., “A tri-axial laser gyro,” Mechanical Technology of Inertial Devices, Proc. Inst. Mech. Eng. (London), 1987–2, Paper C56/87.
Weber, D.J., “A three-axis monolithic ring laser gyro,” Navigation, J. Inst. Nay., 35, 1, pp. 15–22, Spring 1988.
Ezekiel, S., H.J. Arditty (Eds.) Fiber-Optic Rotation Sensors, Springer-Verlag, New York, p. 7, 1982.
Mark, J., A. Brown, “Laser gyroscope random walk determination using a fast filtering technique,” DGON Symposium Gyro Technology, Stuttgart, 1984.
IEEE STD 647–1981. Specification Format Guide and Test Procedure for Single-Axis Laser Gyros.
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Lawrence, A. (1998). The Ring Laser Gyro. In: Modern Inertial Technology. Mechanical Engineering Series. Springer, New York, NY. https://doi.org/10.1007/978-1-4612-1734-3_14
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DOI: https://doi.org/10.1007/978-1-4612-1734-3_14
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