The Dynamically Tuned Gyroscope

  • Anthony Lawrence
Part of the Mechanical Engineering Series book series (MES)

Abstract

In the 1940s engineers in Scotland designed a gyro that used a spinning flywheel on a universal (Hooke’s) joint (Figure 9.1). The gyro was surprisingly unstable, and Arnold and Maunder at the University of Edinburgh showed that the dynamic inertia effects of the gimbal in the universal joint were responsible.

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References

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    Howe, E.W., P.H. Savet, “The dynamically tuned free rotor gyro,” Control Engineering, pp. 67–72, June 1964.Google Scholar
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    Craig, R.J.G., “Theory of operation of an elastically supported tuned gyroscope,” and “Theory of errors of a multigimbal, elastically supported tuned gyroscope,” IEEE Trans. on Aerospace and Electronic Systems, AES-8, 3, pp. 280–297, May 1972.CrossRefGoogle Scholar
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    Willems, P.Y. (Ed.), Gyrodynamics, Springer-Verlag, New York, 1974. Includes: Maunder, L., “Some designs and features of dynamically tuned gyroscopes”; Fogarasy, A.A., “A contribution to the dynamics of a spring restrained Hooke’s joint gyroscope”; Lawrence, A.W., “A simulation of a dynamically tuned gyroscope.”Google Scholar
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    Carroll, R., “Dynamically tuned gyroscope,” in Ragan, R.R. (Ed.) “Inertial technology for the future,” IEEE Trans. on Aerospace and Electronic Systems AES-20, 4, pp. 414–444, July 1984.Google Scholar
  9. 9.
    Beardmore, G., “The design and development of a novel strapdown DTG incorporating a gas bearing and fabricated flexure hinge,” DGON Symposium Gyro Technology, Stuttgart, 1984.Google Scholar
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    Karnick, H., “Effects of hinge improvements on design and production cost of a dynamically tuned gyro,” DGON Symposium Gyro Technology, Stuttgart, 1978.Google Scholar
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Copyright information

© Springer Science+Business Media New York 1998

Authors and Affiliations

  • Anthony Lawrence
    • 1
  1. 1.LunenbergUSA

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