• DocumentCode
    3512853
  • Title

    Model-Based Verification and Validation of Component Structures for RF and Optical Experimental Systems

  • Author

    Norton, Charles D. ; Fang, Houfei ; Michel, Thierry ; Moussessian, Alina ; Schiermeier, John ; Springer, Paul ; Otero, Richard

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
  • fYear
    2008
  • fDate
    1-8 March 2008
  • Firstpage
    1
  • Lastpage
    20
  • Abstract
    Future large aperture systems will depend on integrated modeling to assess key performance parameters for designs that cannot be fully tested and verified before flight. Achieving this goal will require integrating component models, results from numerical simulations, and physical tests to predict the performance and prove the viability of such systems within numerous model and measurement uncertainties. We will describe the use of JPL´s precision environment test enclosure (PETE) with integrated modeling for radar component and optical metrology experiments to validate models for predictive analysis of large aperture systems. Capabilities of the CIELO software, developed at JPL for integrated structural-thermal-optical modeling, will be presented along with analysis from other traditional tools such as NASTRAN, ANSYS, and FEM tools. We will conclude with the benefits of having the PETE lab for component testing compared to a high-bay environment.
  • Keywords
    finite element analysis; radar computing; CIELO software; FEM tools; aperture systems; integrated structural-thermal-optical modeling; model-based verification; numerical simulations; precision environment test enclosure; predictive analysis; radar component; Apertures; Integrated optics; Laser radar; Measurement uncertainty; Numerical models; Numerical simulation; Optical devices; Predictive models; Radio frequency; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2008 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-1487-1
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2008.4526379
  • Filename
    4526379