• DocumentCode
    359001
  • Title

    Application of COTS for early, low cost, avionics system testbed

  • Author

    Graves, D. Ricky

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    1
  • fYear
    2000
  • fDate
    2000
  • Firstpage
    413
  • Abstract
    The use of flight hardware breadboards to construct an avionics subsystem testbed has been very successfully used on past Jet Propulsion Laboratory (JPL) projects. These testbeds provide valuable early integration experience with the flight hardware and software operating together. Commercial off the shelf (COTS) based test systems are integrated with the flight hardware, breadboards to create an Avionics testbed platform. The breadboard system has typically consisted of custom-built hardware that was quite expensive and time consuming to build and maintain. With level or decreasing NASA budgets, and faster, better, cheaper project mentality, the flight hardware breadboard has become a target of Federal budget cuts. Since the custom breadboards are not financially feasible, but the need for an early development avionics testbed still apparent, the role of the COTS hardware was expanded to include flight avionics functions. As an added benefit, the COTS hardware can be used as the basis for the flight hardware design
  • Keywords
    avionics; design for testability; economics; electronic design automation; electronic equipment testing; COTS hardware; JPL projects; NASA; avionics; avionics subsystem testbed; cost; flight avionics functions; flight hardware; flight hardware breadboards; flight hardware design; off the shelf test systems; Aerospace electronics; Aerospace engineering; Aerospace testing; Costs; Hardware; Laboratories; Propulsion; Software testing; Space vehicles; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2000 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-5846-5
  • Type

    conf

  • DOI
    10.1109/AERO.2000.879422
  • Filename
    879422