• DocumentCode
    2839282
  • Title

    Digital flight control systems: some new commercial twists

  • Author

    Todd, John R. ; Yount, Larry J.

  • Author_Institution
    McDonnell Douglas Corp., Long Beach, CA, USA
  • fYear
    1991
  • fDate
    14-17 Oct 1991
  • Firstpage
    79
  • Lastpage
    84
  • Abstract
    The exponential increase in the number and complexity of aircraft digital electronic systems over the last decade has brought to light a number of fault and failure mechanisms not encountered with traditional mechanical and analog systems. One approach to handling these problems on future commercial aircraft is through the use of integrated modular avionics (IMAs). The issues and concepts associated with commercial IMAs are discussed. Some integration concepts for future fly-by-wire/fly-by-light commercial aircraft are considered. It is likely that highly integrated commercial modular avionics systems will be in service by the late 1990s or early twenty first century. It is expected that the extent and rapidity of modular avionics applications on commercial transport will depend largely on the flexibility and fault tolerance achievable at a reasonable cost as well as on the need for incorporation of new highly integrated systems
  • Keywords
    aircraft control; aircraft instrumentation; digital control; modules; aircraft digital electronic systems; digital flight control systems; failure mechanisms; fault mechanisms; fly-by-light commercial aircraft; fly-by-wire aircraft; integrated modular avionics; Aerospace control; Aerospace electronics; Aircraft propulsion; Certification; Computer architecture; Costs; Failure analysis; Fault tolerance; Glass; Military aircraft;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 1991. Proceedings., IEEE/AIAA 10th
  • Conference_Location
    Los Angeles, CA
  • Type

    conf

  • DOI
    10.1109/DASC.1991.177147
  • Filename
    177147