Selective modal space control approach for smart composite cylindrical shell structure

Kumar, GV and Rao, KM and Kumar, JS and Raja, S (2011) Selective modal space control approach for smart composite cylindrical shell structure. ARPN Journal of Engineering and Applied Sciences, 6 (3). pp. 67-74. ISSN 1819-6608

Full text available as:
[img] PDF
Restricted to Registered users only

Download (438Kb) | Request a copy

    Abstract

    This paper presents selective modal space control approach (SMSC) to address the vibration suppression of critical elastic modes of composite cylindrical shell, using collocated/non collocated sensor/actuator. A four node, electro-mechanically coupled field consistent facet shell finite element is used to model the shell vibration. Subsequently, a linear quadratic regulator (LQR) is designed in modal domain to conduct the vibration control simulation studies. The results of active vibration control (AVC) of a laminated composite cylindrical shell, equipped with piezoelectric composite actuators i.e., Macro Fiber Composite (MFC) and PZT sensors are presented. The effectiveness of MFC in controlling shell vibration is evaluated. An effort has been made to addresses the question of whether performance is affected by the collocation/non-collocation of the sensors and actuator.

    Item Type: Journal Article
    Additional Information: Copyright for this article belongs to M/s. Asian Research Publishing Network (ARPN)
    Uncontrolled Keywords: Selective modal space control;Composite cylindrical shell; sensors;Actuators;Vibration control;MFC actuator
    Subjects: AERONAUTICS > Aeronautics (General)
    CHEMISTRY AND MATERIALS > Composite Materials
    ENGINEERING > Structural Mechanics
    Division/Department: Other, Other, Other, Structures Division
    Depositing User: Ms. Alphones Mary
    Date Deposited: 26 Mar 2012 10:27
    Last Modified: 26 Mar 2012 10:27
    URI: http://nal-ir.nal.res.in/id/eprint/10396

    Actions (login required)

    View Item