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Fly-By-Wire Systems for Military High Performance Aircraft

  • D. Langer
  • J. Rauch
  • M. Rößler
Part of the The Springer International Series in Engineering and Computer Science book series (SECS, volume 167)

Abstract

In the early times of aviation, aircraft flight controls were purely mechanical systems comprised of pulleys and cables deflecting the aircraft’s control surfaces about their hinges. The control stick/pedal inputs applied by the pilot counteracted the aerodynamic forces acting upon the control surfaces.

Keywords

Flight Control Multiprocessor System Inertial Coordinate System Flight Control System Body Coordinate System 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. [1]
    Normenstelle Luftfahrt, (1970) LN 9300 (1970).Google Scholar
  2. [2]
    McRuer, D. et al., “Aircraft Dynamics and Automatic Control”, Princeton University Press, Princteon, New Jersey, 1973Google Scholar
  3. [3]
    Andrew S. Tannenbaum, “Operating Systems: Design and Implementation”, Prentice-Hall, New York, 1987Google Scholar
  4. [4]
    Gary L. Hartmann, Joseph E. Wall, Edward R. Rang, “Design Validation of Fly-By-Wire Flight Control Systems”, AGARD, Lecture Series Nr.143 Google Scholar
  5. [5]
    Michel Muenier, “Testing Embedded Software”, AGARD, Lecture Series Nr. 158 Google Scholar
  6. [6]
    Karl N. Levitt, “Software Validation and Verification Techniques”, AGARD, Lecture Series Nr. 109 Google Scholar

Copyright information

© Kluwer Academic Publishers 1992

Authors and Affiliations

  • D. Langer
    • 1
  • J. Rauch
    • 1
  • M. Rößler
    • 1
  1. 1.MESSERSCHMITT-BÖLKOW-BLOHM GmbH Aircraft DivisionMünchen 80

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