• DocumentCode
    181202
  • Title

    Simulating faults in integrated systems and their impact on the aircraft

  • Author

    Kansal, Aparna ; Pritchett, Amy

  • Author_Institution
    Georgia Institute of Technology, Atlanta, GA
  • fYear
    2014
  • fDate
    5-9 Oct. 2014
  • Firstpage
    1
  • Lastpage
    20
  • Abstract
    Outcomes from Case Study • Component failures can be simulated by violating component axioms to identify their impact on the integrated system and the aircraft. • Such simulations can identify requirements for other components • The timing of components executing a task is an important criteria to consider WMC Simulation Environment • Ability to allow a range of component models • Allows each component to specify its own update time • Using shared format for storing data as resources allows for simple models to be generated quickly • Incorporating simple representations of component models is sufficient to obtain an initial understanding of the effects of violating axioms • Its streamlined form allows for a large number of runs examining a number of test cases in lesser time • As the design and test program progresses, potential also exists to include progressively detailed — and ultimately complete — models of the components
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference (DASC), 2014 IEEE/AIAA 33rd
  • Conference_Location
    Colorado Springs, CO, USA
  • Print_ISBN
    978-1-4799-5002-7
  • Type

    conf

  • DOI
    10.1109/DASC.2014.6979578
  • Filename
    6979578