• DocumentCode
    1630941
  • Title

    Neural Network Integration Fusion Model and Application

  • Author

    Zhang, Xiaodan ; Niu, Zhendong

  • Author_Institution
    Sch. of Comput. Sienstist & Technol., Beijing Inst. of Technol., Beijing
  • Volume
    1
  • fYear
    2008
  • Firstpage
    213
  • Lastpage
    215
  • Abstract
    A new fusion model is proposed, which is the combination of BP neural networks and rough set algorithm, to solve the problems of low precision rate in aircraft engine fault diagnosis by traditional methods. The method realizes feature level fusion of all subjective data and expert experiments on different parts of engine, and the predominance compensation of different models. In simulation experiment, the method proposed in the paper can improve diagnosis precision 5.0% more than expert system.
  • Keywords
    aerospace computing; aerospace engines; backpropagation; fault diagnosis; neural nets; rough set theory; BP neural networks; aircraft engine fault diagnosis; feature level fusion; neural network integration fusion model; rough set algorithm; Aircraft propulsion; Algorithm design and analysis; Application software; Computer networks; Diagnostic expert systems; Fault diagnosis; Intelligent networks; Intelligent systems; Neural networks; Uncertainty;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Systems Design and Applications, 2008. ISDA '08. Eighth International Conference on
  • Conference_Location
    Kaohsiung
  • Print_ISBN
    978-0-7695-3382-7
  • Type

    conf

  • DOI
    10.1109/ISDA.2008.331
  • Filename
    4696205