Skip to main content

Vibrating Gyroscopes

  • Chapter
Modern Inertial Technology

Part of the book series: Mechanical Engineering Series ((MES))

Abstract

Gyroscopes would be more reliable and less expensive if they had neither spinning wheels nor flotation fluids. Single-degree-of-freedom gyro (SDFG) wheel bearings must be stiff and isoelastic, and for both SDFGs and dynamically tuned gyros (DTGs) the bearings must be noiseless, as low friction as possible, and must start at low temperatures. Gas bearings cost more, and flotation fluids can require temperature control, damping compensation, and scrupulously clean assembly. By the 1960s every reasonable path around these problems had been tried.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 189.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 249.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 249.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. Quick, W.H., “Theory of the vibrating string as an angular motion sensor,” Trans. ASME, J. Appl. Mech., pp. 523–534, Sept. 1964.

    Google Scholar 

  2. Chen Feng-Yu, Quing Rong-Kang, “The development of piezoelectric crystal gyroscopes in China,” DGON Symposium Gyro Technology, Stuttgart, 1988.

    Google Scholar 

  3. Boocock, D., L. Maunder, “Vibration of a symmetric tuning fork,” J. Mech. Eng. Sci., 11, 4, 1969.

    Google Scholar 

  4. Fox, C.H.J., D.J.W. Hardie, “Vibratory gyroscopic sensors,” DGON Symposium Gyro Technology, Stuttgart, 1984.

    Google Scholar 

  5. Hunt, G.W., A.E.W. Hobbs, “Development of an accurate tuning-fork gyroscope,” Symposium on Gyros, Proc. Inst. Mech. Eng. (London), 1964–65, 179, 3E.

    Google Scholar 

  6. Barbour, N., J. Connelly, J. Gilmore, P. Greiff, A. Kourepenis, M. Weinberg, “Micromechanical silicon instrument and systems development at Draper Laboratory,” AAIA Guidance, Navigation and Control Conference, San Diego, CA, 29–31 July 1996.

    Google Scholar 

  7. Weinberg, M., J. Bernstein, S. Cho, A.T. King, A. Kourepenis, P. Maciel, “A micromachined comb-drive tuning fork rate gyroscope,” Institute of Navigation, Proc. 49th Annual Meeting, Cambridge, MA, 21–23 June 1993.

    Google Scholar 

  8. Lynch, D.D., “Hemispherical resonator gyro,” 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. Bryan, G.H., “On the beats in the vibrations of a revolving cylinder or bell,” Proc. Camb. Phil. Soc., Vol VII, Nov. 24, pp. 101–111, 1890.

    Google Scholar 

  10. Loper, E.J., D.D. Lynch, “Projected system performance based on recent HRG test results,” Paper S83–105, IEEE/AIAA Fifth Digital Avionics Systems Conference, 31 Oct.-3 Nov. 1983.

    Google Scholar 

  11. Loper, E.J., D.D. Lynch, “The HRG: A new low-noise inertial rotation sensor,” 16th Joint Services Data Exchange for Inertial Systems, Los Angeles, CA, 16–18 Nov. 1982.

    Google Scholar 

  12. Scott, W.B., “Delco makes low-cost gyro prototype,” Aviation Week and Space Technology, 25 Oct. 1982.

    Google Scholar 

  13. Fox, C.H.J., “Vibrating cylinder rate gyro, theory of operation and error analysis,” DGON Symposium Gyro Technology, Stuttgart, 1988.

    Google Scholar 

  14. Burdess, J.S., “The dynamics of a thin piezoelectric cylinder gyroscope,” Proc. Inst. Mech. Engrs. (London), Vol. 200, No. C4, pp. 271–280, 1986.

    Google Scholar 

  15. Harris, D.G., “START: A novel gyro for weapon’s guidance,” DGON Symposium Gyro Technology, Stuttgart, 1988.

    Google Scholar 

  16. Koning, M.G., “Vibrating cylinder gyroscope and method,” U.S. Patent 4 793 195, 27 Dec. 1988.

    Google Scholar 

  17. Pittman, R., “Rate sensor,” U.S. Patent 3 359 806, 26 Dec. 1967.

    Google Scholar 

  18. Jones, B.G., “The development of a miniature twin-axis rate gyro,” in Mechanical Technology of Inertial Devices,Proc. Inst. Mech. Eng. (London), 1987–2, Paper C62/87.

    Google Scholar 

  19. Rider, B.F., “Sensor assembly having means for cancellation of harmonic induced bias from a two-axis linear accelerometer,” U.S. Patent 4 462 254, 31 July 1984.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

Copyright information

© 1998 Springer Science+Business Media New York

About this chapter

Cite this chapter

Lawrence, A. (1998). Vibrating Gyroscopes. In: Modern Inertial Technology. Mechanical Engineering Series. Springer, New York, NY. https://doi.org/10.1007/978-1-4612-1734-3_11

Download citation

  • DOI: https://doi.org/10.1007/978-1-4612-1734-3_11

  • Publisher Name: Springer, New York, NY

  • Print ISBN: 978-1-4612-7258-8

  • Online ISBN: 978-1-4612-1734-3

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics