• DocumentCode
    1701803
  • Title

    Wavelet coherence analysis approach to model validation of the hypersonic vehicle model

  • Author

    Zhang Xi Bin ; Zong Qun

  • Author_Institution
    Sch. of Electr. Eng. & Autom., Tianjin Univ., Tianjin, China
  • fYear
    2013
  • Firstpage
    768
  • Lastpage
    772
  • Abstract
    A simplified hypersonic vehicle(HSV) model, which would be applied for control design, could be obtained by decoupling the rigid-elastic modes and neglecting certain weak couplings. The credibility of simplified model of HSV should be effectively verified. By comparing the output time series of the true model and simplified model, which is usually non-stationary, a quantitative assessment method based on wavelet coherence is presented. In comparison to the traditional methods in time or frequency domain, the wavelet coherence analysis approach could quantitatively test the simplified model at each time and frequency (scale). Monte Carlo simulations are used to assess the critical value against red noise backgrounds. The simulations show the wavelet coherence analysis validation methods effectiveness.
  • Keywords
    Monte Carlo methods; aircraft control; control system synthesis; missile control; vehicle dynamics; wavelet transforms; HSV model; Monte Carlo simulations; air vehicle control system; certain weak couplings; control design; frequency domain methods; hypersonic vehicle model; output time series; quantitative assessment method; red noise backgrounds; rigid-elastic modes; time domain method; true model; wavelet coherence analysis validation method; Aerodynamics; Analytical models; Atmospheric modeling; Coherence; Time series analysis; Vehicle dynamics; Vehicles; hypersonic vehicle; model validation; significant test; simplified model; wavelet coherence;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2013 32nd Chinese
  • Conference_Location
    Xi´an
  • Type

    conf

  • Filename
    6639531