• DocumentCode
    133131
  • Title

    Reduced order flutter modeling based on the Hammerstein model with μ-Markov structure and correlation identification method

  • Author

    Kai-Yew Lum ; Kwok-Leung Lai

  • Author_Institution
    Dept. of Electr. Eng., Nat. Chi Nan Univ., Puli, Taiwan
  • fYear
    2014
  • fDate
    9-12 Sept. 2014
  • Firstpage
    1691
  • Lastpage
    1697
  • Abstract
    This paper presents an approach for reduced order flutter modeling based on the Hammerstein model and system identification. The Hammerstein model considered is prescribed a μ-Markov structure in the linear block, and its identification employs a correlation-based method for separable input processes. This combination of model and identification method has been shown in a previous work to accurately identify the linear block, which is vital to bifurcation analysis. Using computational fluid dynamics data and an experimental benchmark, it is shown that the proposed approach yields better accuracy relative to the benchmark as well as by model validation.
  • Keywords
    Markov processes; aerodynamics; aerospace components; computational fluid dynamics; reduced order systems; Hammerstein model; Markov structure; computational fluid dynamics; correlation identification method; reduced order flutter modeling; wing aerodynamic response; Aerodynamics; Atmospheric modeling; Benchmark testing; Computational modeling; Correlation; Mathematical model; Read only memory; Hammerstein model; System identification; aerodynamics; reduced-order modeling;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    SICE Annual Conference (SICE), 2014 Proceedings of the
  • Conference_Location
    Sapporo
  • Type

    conf

  • DOI
    10.1109/SICE.2014.6935293
  • Filename
    6935293