• DocumentCode
    2635690
  • Title

    The dynamical response analysis of piezoelectric flexible structures based on model reduction

  • Author

    Zhang, Jingjun ; He, Lili ; Gao, Ruizhen

  • Author_Institution
    Dept. of Sci. Res., Hebei Univ. of Eng., Handan
  • fYear
    2008
  • fDate
    10-12 Dec. 2008
  • Firstpage
    1
  • Lastpage
    5
  • Abstract
    Piezoelectric materials are finding increasing applications in active vibration control of structures. A widely used modeling technique for piezoelectric flexible structures is the assumed modes method which results in an infinite dimensional model of the composite structure. The paper builds the model of piezoelectric flexible structures and calculates the modal frequency by the application of ANSYS software, extracts the required modes according to the method of model reduction based on the spatial H2 norms of modes. The optimal location of the piezoelectric patches is ascertained by applying the D-optimal design principle, which avoids the locationpsilas randomicity as well as reduces the number of sensors/actuators in terms of not affect the controlling effect. Finally, the paper takes a piezoelectric cantilever beam as an example and gives the step response curve of the system. The results show that this method has more superiority than the ordinary modes truncation.
  • Keywords
    beams (structures); cantilevers; flexible structures; piezoelectricity; structural engineering; vibration control; ANSYS software; composite structure; dynamical response analysis; infinite dimensional model; ordinary modes truncation; piezoelectric cantilever beam; piezoelectric flexible structures; piezoelectric materials; structures active vibration control; Application software; Ceramics; Flexible structures; Frequency; Helium; Piezoelectric actuators; Piezoelectric materials; Reduced order systems; Sensor phenomena and characterization; Vibration control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aerospace and Astronautics, 2008. ISSCAA 2008. 2nd International Symposium on
  • Conference_Location
    Shenzhen
  • Print_ISBN
    978-1-4244-3908-9
  • Electronic_ISBN
    978-1-4244-2386-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2008.4776140
  • Filename
    4776140