• DocumentCode
    2062212
  • Title

    The unique aspects of simulation verification and validation

  • Author

    Thomas, Danny ; Joiner, Alexia ; Lin, Wei ; Lowry, Michael ; Pressburger, Tom

  • Author_Institution
    AEgis Technol. Group, Huntsville, AL, USA
  • fYear
    2010
  • fDate
    6-13 March 2010
  • Firstpage
    1
  • Lastpage
    7
  • Abstract
    Models and simulations (M&S) will be employed to support important design decisions and verification of system requirements in the development of NASA´s Orion Crew Exploration Vehicle. Most simulations are implemented in software. For developed software, NASA´s software engineering procedural guideline NPR 7150.2 and safety standard NASA-STD-8719.13B apply. Recognizing the need for critical M&S to be validated to be credible for their intended uses, NASA developed a Modeling and Simulation Standard, NASA-STD-7009. This paper analyzes the requirements specified by these standards and their role in test, validation and certification of modeling and simulation software. It discusses simulation validation as a distinct instance of software validation with corresponding unique requirements. Simulation-specific validation concerns include fit to intended use, validation against experimental data, uncertainty quantification, and sensitivity analysis. The paper also describes the Orion M&S verification, validation, and accreditation (VV&A) process.
  • Keywords
    digital simulation; formal verification; software engineering; spacecraft computers; standards; NASA-STD-8719.13B safety standard; NPR 7150.2 guideline; Orion crew exploration vehicle; simulation validation; simulation verification; software engineering; Analytical models; Certification; Guidelines; NASA; Software engineering; Software safety; Software standards; Software testing; Standards development; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2010 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-3887-7
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2010.5446785
  • Filename
    5446785