• DocumentCode
    1613837
  • Title

    Determination of Flutter Boundary by Robust Flutter Margin Method

  • Author

    Fucun, Qu

  • Author_Institution
    Control Eng. Coll., Chengdu Univ. of Inf. Technol., Chengdu, China
  • fYear
    2012
  • Firstpage
    1061
  • Lastpage
    1063
  • Abstract
    A new method, robust flutter margin method, of determining flutter boundary was introduced. Leverages the structured singular value theory will flutter model combining organically flight test data, prediction of flutter boundary. Simulation results show that the method is feasible.
  • Keywords
    aerospace testing; singular value decomposition; flight test data; flutter boundary determination; robust flutter margin method; structured singular value theory; Aerodynamics; Aircraft; Atmospheric modeling; Damping; Data models; Robustness; Uncertainty; Flight test; Flutter boundary; Structured singular value;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Industrial Control and Electronics Engineering (ICICEE), 2012 International Conference on
  • Conference_Location
    Xi´an
  • Print_ISBN
    978-1-4673-1450-3
  • Type

    conf

  • DOI
    10.1109/ICICEE.2012.280
  • Filename
    6322569
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1613837