Skip to main content

Abstract

This chapter presents the principle of operation of a class of nongyroscopic electromechanical sensors based on the Coriolis effect. The significant ongoing technological development effort in a number of leading industries in the United States now yielded prototypes that have demonstrated promising performance. These efforts may eventually lead to the replacement of the relatively cumbersome gyroscopic spinning mass technology.

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

Access this chapter

Subscribe and save

Springer+ Basic
$34.99 /Month
  • Get 10 units per month
  • Download Article/Chapter or eBook
  • 1 Unit = 1 Article or 1 Chapter
  • Cancel anytime
Subscribe now

Buy Now

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 129.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 179.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 169.99
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. Merhav, S., “A Nongyroscopic Inertial Measurement Unit,” AIAA Journal of Guidance, Control and Dynamics, Vol. 5, No. 3, pp. 227–235, May-June, 1982.

    Article  Google Scholar 

  2. Goldstein, H., Classical Mechanics, Addison-Wesley, Reading, 1959.

    Google Scholar 

  3. Merhav, S., “Apparatus and Method for measuring Specific Force and Angular rate,” United States Patent No. 4,445,376, May, 1984.

    Google Scholar 

  4. Klass, P.J., “Inertial Sensor Utilizes Coriolis Effect,” Aviation Week and space Technology, pp. 89–91, October 10, 1983.

    Google Scholar 

  5. Merhav, S., “Apparatus for Measuring Inertial Specific Force and Angular Rate of a Moving Body,” United States Patent No. 4,590,801, May 1986.

    Google Scholar 

  6. Hulsing, R., “Multi Axis Angular Rate Sensor Having a Single Dither Axis,” United States Patent No. 4,821,572, April 1989.

    Google Scholar 

  7. Hulsing, R., and MacGugan, D., “Miniature IMU Based on Micromachined Coriolis Sensor,” ION paper, January 21, 1993.

    Google Scholar 

  8. Savage, P.G., “Strapdown Inertial Sensors, Theory and Applications,” AGARD lecture Series No. 95, June 1978.

    Google Scholar 

  9. Barbour, N.M., Elwell, J.M., and Setterlund R.H., “Inertial Instruments — Where to Now”, Proc. AIAA Guidance, Navigation and Control Conference, paper AIAA-92–4414-CP, Hilton Head, SC, August 1992, pp. 566–574.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

Copyright information

© 1996 Springer-Verlag New York, Inc.

About this chapter

Cite this chapter

Merhav, S. (1996). Coriolis Angular Rate Sensors. In: Aerospace Sensor Systems and Applications. Springer, New York, NY. https://doi.org/10.1007/978-1-4612-3996-3_7

Download citation

  • DOI: https://doi.org/10.1007/978-1-4612-3996-3_7

  • Publisher Name: Springer, New York, NY

  • Print ISBN: 978-1-4612-8465-9

  • Online ISBN: 978-1-4612-3996-3

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics