• DocumentCode
    232452
  • Title

    Sensitivity analysis based model validation for Hypersonic Vehicle model

  • Author

    Zeng Fanlin ; Zong Qun ; Zhang Xibin ; You Ming

  • Author_Institution
    Sch. of Autom. & Electr. Eng., Tianjin Univ. of Technol. & Educ., Tianjin, China
  • fYear
    2014
  • fDate
    28-30 July 2014
  • Firstpage
    6287
  • Lastpage
    6292
  • Abstract
    This paper presents a novel model validation methodology based on sensitivity analysis method. Uncertain parameters of the Hypersonic Vehicle model are considered as risk factors. Validation method is composed of parameter sensitivity analysis and uncertainty quantification. Quantitative evaluation of the accuracy and reliability of model are given from the user´s point of view with validation metrics. The new model validation method was then used to evaluate the quality of the Hypersonic Vehicle model. Simulation results are provided to demonstrate that the new model validation method provides a highly efficient and powerful new method for Hypersonic Vehicle model validation.
  • Keywords
    aircraft control; risk analysis; sensitivity analysis; hypersonic vehicle model; parameter sensitivity analysis; quantitative evaluation; reliability; risk factors; sensitivity analysis based model validation method; uncertain parameters; uncertainty quantification; Analytical models; Computational modeling; Predictive models; Sensitivity analysis; Uncertainty; Vehicles; Hypersonic vehicle; Model validation; Risk factor; Security metrics; Sensitivity analysis;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2014 33rd Chinese
  • Conference_Location
    Nanjing
  • Type

    conf

  • DOI
    10.1109/ChiCC.2014.6896022
  • Filename
    6896022