• DocumentCode
    1967132
  • Title

    LXI addresses aircraft flight control system simulation test

  • Author

    Chaoyou, Zhi ; Zhenshui, Li ; Xia, Li

  • Author_Institution
    First Aircraft Inst., Xi´´an
  • fYear
    2007
  • fDate
    17-20 Sept. 2007
  • Firstpage
    511
  • Lastpage
    516
  • Abstract
    The increase for requirements in reusability and flexibility has created new challenge in the development of aircraft flight control system simulation test. Incorporating LXI devices as a part of a system not only can provide an additional level of flexibility and capability for the specific application, but also can support custom requirements with minimal cost and testing time. This paper describes our research and development efforts in the application of LXI devices in aircraft flight control system simulation test, the paper specifies the measurement and test system hardware architecture and software architecture. The interchangeable virtual instruments (IVI) tools and architectural elements enable user to develop software systems that is independent of the underlying instruments. The paper also described how IVI drivers and associated IVI shared components are used to develop a system. An example program using instruments based on LXI to acquisition data is presented.
  • Keywords
    aerospace computing; aerospace simulation; aircraft control; control engineering computing; virtual instrumentation; LXI devices; aircraft flight control system simulation test; interchangeable virtual instruments; Aerospace control; Aerospace simulation; Aircraft; Application software; Costs; Instruments; Research and development; Software measurement; Software testing; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Autotestcon, 2007 IEEE
  • Conference_Location
    Baltimore, MD
  • ISSN
    1088-7725
  • Print_ISBN
    978-1-4244-1239-6
  • Electronic_ISBN
    1088-7725
  • Type

    conf

  • DOI
    10.1109/AUTEST.2007.4374261
  • Filename
    4374261