• DocumentCode
    2588554
  • Title

    Model-based adaptation of flight-critical systems

  • Author

    Ray, Sumit ; Karsai, Gabor ; McNeill, Kevin M.

  • Author_Institution
    BAE Syst., Johnson City, NY, USA
  • fYear
    2009
  • fDate
    23-29 Oct. 2009
  • Abstract
    In this paper we describe our experience applying the Producible Adaptive Model-based Software (PAMS) technology to the development of safety critical flight control software. PAMS is based on the state of the art Model Integrated Computing (MIC) environment from Vanderbilt University and represents a highly evolvable model-based software development methodology and tool suite that is revolutionary in its ability to address software adaptation. In particular, PAMS is an adaptation framework that introduces support for model transformations, co-evolution of models and modeling tools, and self-adaptation of systems. Analogous to delayed binding in compiler technology, PAMS enables binding software updates statically at design-time, on a configuration basis at load-time, and dynamically at run-time. The focus of this paper will be the application of PAMS to designtime evolution.
  • Keywords
    aerospace control; safety-critical software; software engineering; flight critical systems; model based adaptation; model based software development; model integrated computing environment; model transformation; producible adaptive model-based software; safety critical flight control software; software adaptation; Adaptation model; Adaptive control; Aerospace control; Aerospace safety; Delay systems; Microwave integrated circuits; Programmable control; Programming; Software safety; Software tools;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 2009. DASC '09. IEEE/AIAA 28th
  • Conference_Location
    Orlando, FL
  • Print_ISBN
    978-1-4244-4078-8
  • Type

    conf

  • DOI
    10.1109/DASC.2009.5347443
  • Filename
    5347443