• DocumentCode
    1090386
  • Title

    Crashproof codes [flight software]

  • Author

    Hess, Ronald K. ; Bass, David I. ; Baca, John B.

  • Volume
    41
  • Issue
    9
  • fYear
    2004
  • Firstpage
    48
  • Lastpage
    53
  • Abstract
    Boeing Co. and NASA have joined forces for the Active Aeroelastic Wing (AAW) Project to test the way a modified F/A-18 strike fighter uses its wings. The AAW was designed to be flexible enough to be twisted on demand in flight and it could herald nothing less than a revolution in aviation. The twisting can be used to control the plane´s roll, reducing and ultimately eliminating the need for ailerons and flaps and their associated hardware. AAW-equipped planes would result to increased fuel efficiency and improved maneuverability, able to execute sharper turns at higher speeds. A special flight software was developed to keep track of the plane´s speed, altitude, and attitude while monitoring the pilot´s controls for commands. Based on a set of rules known as control laws, the software must then translate any commands from the pilot into movements of the aircraft´s various control surfaces such as the rudders or, most significantly, the flaps that flex the AAWs. Despite its complex and critical job, the flight software is compact, consisting of only about 13,000 lines of source code written in the Ada language.
  • Keywords
    aerospace computing; aerospace control; aerospace testing; avionics; military aircraft; program testing; Active Aerolastic Wing project; aviation; flight software; supersonic aircraft; Computer crashes; Vehicle crash testing;
  • fLanguage
    English
  • Journal_Title
    Spectrum, IEEE
  • Publisher
    ieee
  • ISSN
    0018-9235
  • Type

    jour

  • DOI
    10.1109/MSPEC.2004.1330810
  • Filename
    1330810