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Fly-by-Wire Flight Control

  • R. P. G. Collinson
Chapter

Abstract

The introduction of fly-by-wire (FBW) flight control systems has been a watershed development in aircraft evolution as it has enabled technical advances to be made which were not possible before. One of the unique benefits of a FBW system is the ability to exploit aircraft configurations which provide increased aerodynamic efficiency, like more lift and lower drag, but at a cost of reduced natural stability. This can include negative stability, that is the aircraft is unstable over part of the range of speed and height conditions (or flight envelope).

Keywords

Control Surface Sensor Output Flight Control Loop Gain Roll Rate 
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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Further Reading

  1. Barnes, J.G.P., Programming in Ada, Addison Wesley.Google Scholar
  2. Brire, D., Favre, C. and Traverse, P., A Family of Fault-Tolerant Systems: Electrical Flight Controls, from Airbus A320/330/340 to Future Military Transport Aircraft, ERA Avionics Conference, 1993.Google Scholar
  3. Coad, P. and Yourden, E., Object Oriented Analysis, Yourdon Press/Prentice Hall, 1991.Google Scholar
  4. Davis, A.M., Software Requirements – Analysis and Specification, Prentice Hall, 1990.Google Scholar
  5. D’Azzo, J.J. and Houpus, C.H., Linear Control System Analysis and Design, McGraw-Hill.Google Scholar
  6. DeMarco, T., Structured Analysis and Design, Yourdon Press Computing Press, 1978.Google Scholar
  7. Hatley, D.J. and Pirbhai, I.A., Strategies for Real-Time System Specification, Dorset House, 1988.Google Scholar
  8. IEE Control Engineering Theory 57; Flight Control Systems – Practical Issues in Design and Implementation, R.W. Pratt (Ed.), 2000.Google Scholar
  9. Ince, D.C., An Introduction to Discrete Mathematics and Formal System Specification, Oxford University Press, 1988.Google Scholar
  10. Interim Defence Standard DEF STAN OO-55, The Procurement of Safety Critical Software in Defence Equipment, 5 April 1991.Google Scholar
  11. McLean, D., Automatic Flight Control Systems, Prentice Hall.Google Scholar
  12. Military Standard DOD-STD-2167A, Defense System Software Development, 29 February 1988.Google Scholar
  13. Mirza, N.A., Primary Flight Computers for the Boeing 777, ERA Avionics Conference 1992 ERA Report 92–0809.Google Scholar
  14. Ramage, J.K., AFTI/F16 Automated Maneuvering Attack System Configuration and Integration, in Proceedings of the IEEE 1986 National Aerospace and Electronics Conference, Dayton, Ohio.Google Scholar
  15. RTCA-EUROCAE DO178B/ED-12B, Software Considerations in Airborne Systems and Equipment Certification: December 1992.Google Scholar
  16. Rushby, J., Formal Methods and the Certification of Critical Systems, Technical report CSL-93-7 December 1993 Computer Science Laboratory SRI International.Google Scholar

Copyright information

© Springer Science+Business Media B.V. 2011

Authors and Affiliations

  • R. P. G. Collinson
    • 1
  1. 1.Formerly of GEC Avionics (now part of BAE Systems)KentUK

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