• DocumentCode
    2514917
  • Title

    Lifecycle software support for the C-17 Globemaster III

  • Author

    Liosis, Andy

  • Author_Institution
    Transp. Aircraft, McDonnell Douglas Corp., Long Beach, CA, USA
  • fYear
    1994
  • fDate
    20-22 Sep 1994
  • Firstpage
    571
  • Lastpage
    574
  • Abstract
    The advanced avionics computer systems of the C-17 Globemaster III contain operational flight program software which requires a life cycle support system to accommodate user mission changes and aircraft upgrades. Building upon its C-17 avionics development experience, McDonnell Douglas has developed an integration support facility concept which will substantially reduce the costs of maintaining the C-17 flight software over its projected life cycle. The concept unites the benefits of open architecture, distributed processing, and advanced UNIX-based workstations, as well as the cost advantages of available commercial off-the-shelf software and equipment
  • Keywords
    automatic test software; military avionics; military computing; software tools; C-17 Globemaster III; C-17 avionics development; C-17 flight software; McDonnell Douglas; UNIX-based workstations; aircraft upgrades; avionics computer; commercial off-the-shelf software; costs; distributed processing; integration support facility; lifecycle software support; off-the-shelf equipment; open architecture; operational flight program software; user mission changes; Aerospace electronics; Aircraft manufacture; Computer architecture; Costs; Military aircraft; Military computing; Proposals; Software testing; System testing; Workstations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    AUTOTESTCON '94. IEEE Systems Readiness Technology Conference. 'Cost Effective Support Into the Next Century', Conference Proceedings.
  • Conference_Location
    Anaheim, CA
  • Print_ISBN
    0-7803-1910-9
  • Type

    conf

  • DOI
    10.1109/AUTEST.1994.381567
  • Filename
    381567