Skip to main content

Technical Preliminaries

  • Chapter
  • 273 Accesses

Part of the book series: Advances in Industrial Control ((AIC))

Abstract

This chapter provides background information and describes the tools that are available to the designer of multivariable flight control laws. The fundamentals of aircraft dynamics are reviewed, the basics of flying qualities requirements are discussed, uncertainty models and analysis techniques are presented, and compensator design and order reduction methods are addressed. Because of the wide range of technologies that are considered, it is impossible to present complete details on all of these areas within a reasonable volume. This chapter should therefore be treated as a overview or as a springboard into a more detailed examination of each topic. A list of references is given to facilitate such an effort.

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

Buying options

Chapter
USD   29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD   39.99
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD   54.99
Price excludes VAT (USA)
  • Compact, lightweight 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

Learn about institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. J. H. Blakelock, Automatic Control of Aircraft and Missiles, John Wiley & Sons, New York, 1965.

    Google Scholar 

  2. D. McRuer, I. Ashkenas, and D. Graham, Aircraft Dynamics and Automatic Control, Princeton University Press, Princeton, NJ, 1973.

    Google Scholar 

  3. J. Roskam, Airplane Flight Dynamics and Automatic Flight Controls, Part 1, Roskam Aviation and Engineering Corporation, Ottawa, KA, 1982.

    Google Scholar 

  4. “Military Specification - Flying Qualities of Piloted Vehicles,” MIL-STD-1797A, March 1987.

    Google Scholar 

  5. J. M. Maciejowski, Multivariable Feedback Design, Addison-Wesley, New York, 1989.

    MATH  Google Scholar 

  6. J. C. Doyle, “Analysis of Feedback Systems with Structured Uncertainties,” IEEE Proceedings, vol. 129, Part D, No. 6, pp. 242–250, Nov. 1982.

    MathSciNet  Google Scholar 

  7. J.C. Doyle, J. Wall, and G. Stein, “Performance and Robustness Analysis for Structured Uncertainty,” Proc. 21th IEEE Conf Decision Contr., Dec. 1982.

    Google Scholar 

  8. J.E. Slotine and W. Li, Applied Nonlinear Control, Prentice Hall, Englewood Cliffs, 1991.

    MATH  Google Scholar 

  9. S. H. Lane and R.F. Stengel, “Flight Control Design Using Non-linear Inverse Dynamics,” Automatica, vol. 24, pp. 471–483, 1988.

    Article  MathSciNet  MATH  Google Scholar 

  10. A.N. Andry, E.Y. Shapiro, and J.C. Chung, “Eigenstructure Assignment for Linear Systems,” IEEE Trans. Aerospace and Electronic Systems, vol. 19, No. 5, pp. 711–728.

    Google Scholar 

  11. J. C. Doyle, K. Glover, P. Khargonekar, and B. Francis, “State Space Solutions to Standard H2 and H∞ Control Problems,” IEEE Trans. Automat. Contr., vol. AC-34, pp. 831–847, Aug. 1989

    Article  MathSciNet  Google Scholar 

  12. K. Glover and J. C. Doyle, “State-Space Formulae for all Stabilizing Controllers that Satisfy an H∞, Norm Bound and Relations to Risk Sensitivity,” Systems and Control Letters, vol. 11, pp. 167–172, 1988.

    Article  MathSciNet  MATH  Google Scholar 

  13. M.G. Safonov, D.J. Limebeer, and R.Y. Chiang, “Simplifying the H∞ Theory via Loop Shifting, Matrix Pencil, and Descriptor Concepts,” International Journal of Control, Vol. 50, No. 6, pp. 2467–2488, 1989.

    Article  MathSciNet  MATH  Google Scholar 

  14. H. H. Yeh, J. L. Rawson, and S. S. Banda, “Robust Control Design with Real-Parameter Uncertainties,” Proc. 1992 American Control Conf, Chicago IL, Jun. 1992.

    Google Scholar 

  15. J. M. Buffington, H. H. Yeh, and S. S. Banda, “Robust Control Design for an Aircraft Gust Attenuation Problem,” Proc. 31st Conf. on Decision and Control, Tucson AZ, Dec. 1992.

    Google Scholar 

  16. J. C. Doyle, “Structured Uncertainty in Control System Design,” Proc. 24th IEEE Conf. Decision Contr., Ft. Lauderdale FL, Dec. 1985.

    Google Scholar 

  17. G. J. Balas, A. K. Packard, J. C. Doyle, K. Glover, and R. S. R. Smith, “Development of Advanced Control Design Software for Researchers and Engineers,” Proc. 1991 American Control Conf., Boston MA, June 1991.

    Google Scholar 

  18. B. C. Moore, “Principal Component Analysis in Linear Systems: Controllability, Observability, and Model Reduction,” IEEE Trans. Automat. Contr., vol. AC-26, pp. 17–32, Feb. 1981.

    Article  Google Scholar 

  19. K. Glover, “All Optimal Hankel-Norm Approximations of Linear Multivariable Systems and Their L∞ Error Bounds,” International Journal of Control, vol. 39, pp. 1115–1193, 1984.

    Article  MathSciNet  MATH  Google Scholar 

  20. D. Enns, “Model Reduction for Control System Design,” Doctoral Dissertation, Stanford University, 1984.

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

Copyright information

© 1994 Springer-Verlag London Limited

About this chapter

Cite this chapter

Adams, R.J., Buffington, J.M., Sparks, A.G., Banda, S.S. (1994). Technical Preliminaries. In: Robust Multivariable Flight Control. Advances in Industrial Control. Springer, London. https://doi.org/10.1007/978-1-4471-2111-4_2

Download citation

  • DOI: https://doi.org/10.1007/978-1-4471-2111-4_2

  • Publisher Name: Springer, London

  • Print ISBN: 978-1-4471-2113-8

  • Online ISBN: 978-1-4471-2111-4

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics