• DocumentCode
    1568261
  • Title

    The simulation for damage identification of wing model basis on PNN

  • Author

    Zhao, Jianbin ; Yuan, Mei ; You, Qiang

  • Author_Institution
    Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
  • fYear
    2009
  • Abstract
    Based on the finite element wing model of a certain UAV, neural network approach is used to identify the location and degree of damage. First of all, the theory, characteristics and structure of probabilistic neural network (PNN) is introduced. Then, the one-dimensional and two-dimensional simplified finite element damage models of the wing are established. By the extraction and processing of their natural frequencies and vibration modes from damaged wing structure with different damage position and different damage degree, the trained PNN have the ability of damage identification. Simulation shows that, the model based on PNN can effectively identify the location and degree of damage.
  • Keywords
    aerospace components; finite element analysis; probability; remotely operated vehicles; structural engineering computing; vibrations; 2D simplified finite element damage model; PNN; UAV; damage identification; damaged wing structure; finite element wing model; natural frequencies; neural network approach; probabilistic neural network; vibration modes; Automation; Electric variables measurement; Extraterrestrial measurements; Finite element methods; Frequency; Instruments; Mathematical model; Neural networks; Shape measurement; Unmanned aerial vehicles; PNN; damage identification; natural frequency; vibration mode;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electronic Measurement & Instruments, 2009. ICEMI '09. 9th International Conference on
  • Conference_Location
    Beijing
  • Print_ISBN
    978-1-4244-3863-1
  • Electronic_ISBN
    978-1-4244-3864-8
  • Type

    conf

  • DOI
    10.1109/ICEMI.2009.5274844
  • Filename
    5274844