Skip to main content
  • 368 Accesses

Abstract

This chapter presents some of the foremost applications of rate gyros and other forms of angular rate sensors in flight control, guidance, and automatic navigation systems. In the following description and analysis, the effects of imperfections on overall system performance are presentedm, especially those due to dynamical errors, noise, offsets, and resolution.

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. Blakelock, J.H., Automatic Control of Aircraft and Missiles, John Wiley & Sons, New York, 1991.

    Google Scholar 

  2. Murtaugh, S.A., and Criei, H.E., “Fundamentals of Proportional Navigation,” IEEE Spectrum, Vol. 3, 1966, pp. 75–85.

    Article  Google Scholar 

  3. McRuer, D.T., Graham, D., and Krendel, E., “Manual Control of Single-Loop Systems,” Pts. I and II, Journal of the Franklin Institute, Vol. 238, No. 1, January, 1967, and No. 2, February 1967.

    Google Scholar 

  4. Hudson, R.D. Jr., Infrared System Engineering, John Wiley & Sons, New York, 1969.

    Google Scholar 

  5. Leondes, C.T., Editor, Guidance and Control of Aerospace Vehicles, McGraw-Hill, New York, 1963.

    Google Scholar 

  6. Garg, S.C., Morrow, L.D., and Mamen, R., “Strapdown Navigation Technology: A Literature Survey,” AIAA Journal of Guidance and Control, Vol. 1, No. 3, May-June 1978, pp. 161–172.

    Article  Google Scholar 

  7. McLean, D., “Automatic Flight Control Systems,” Prentice-Hall, Englewood Cliffs, 1990.

    MATH  Google Scholar 

  8. Nesline, F.W., and Zarchan, P., “Why Modern Controllers Can Go Unstable,” AIAA Journal of Guidance, Control, and Dynamics, Vol. 7, No. 4, July-August, 1984, pp. 495–500.

    Article  MATH  Google Scholar 

  9. Farrell, J.L., Integrated Aircraft Navigation, Academic Press, New York, 1976.

    Google Scholar 

  10. Siouris G.M., Aerospace Avionics Systems—A Modern Synthesis, Academic Press, New York, 1993

    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). Applications of Rate Gyros. In: Aerospace Sensor Systems and Applications. Springer, New York, NY. https://doi.org/10.1007/978-1-4612-3996-3_6

Download citation

  • DOI: https://doi.org/10.1007/978-1-4612-3996-3_6

  • 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