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Vibration Control of a Composite Beam Using Self-sensing Semi-active Approach

         

摘要

Structural vibration control was an active research area for the past twenty years because of their potential applications in aerospace structures,civil structures,naval structures,etc.Semi-active vibration control methods based on piezoelectric actuators and synchronized switch damping on inductance(SSDI) techniques attract the attention of many researchers recently due to their advantages over passive and active methods.In the SSDI method,a switch shunt circuit is connected to the piezoelectric patch to shift the phase and amplify the magnitude of the voltage on the piezoelectric patch.The most important issue in SSDI method is to control the switching actions synchronously with the maximum vibration displacement or maximum strain.Hence,usually a displacement sensor is used to measure the vibration displacement or a collocated piezoelectric sensor is needed to measure the strain of the structure near the piezoelectric actuator.A self-sensing SSDI approach is proposed and applied to the vibration control of a composite beam,which avoids using a separate sensor.In the self-sensing technique,the same piezoelectric element functions as both a sensor and an actuator so that the total number of required piezoelectric elements can be reduced.One problem in the self-sensing actuator,which is the same as that in the traditional collocated piezoelectric sensors,is the noise generated in the sensor signal by the impact of voltage inversion,which may cause extra switching actions and deteriorate control performance.In order to prevent the shunt circuit from over-frequent on-and-off actions,a simple switch control algorithm is proposed.The results of control experiments show that the self-sensing SSDI approach combined with the improved switch control algorithm can effectively suppress over-frequent switching actions and gives good control performance by reducing the vibration amplitude by 45%,about 50% improvement from the traditional SSDI with a separate piezoelectric element and a classical switch.

著录项

  • 来源
    《中国机械工程学报》 |2010年第5期|663-670|共8页
  • 作者单位

    The Key Laboratory of Aircraft Structural Mechanics and Control of Ministry of Education,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

    The Key Laboratory of Aircraft Structural Mechanics and Control of Ministry of Education,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

    The Key Laboratory of Aircraft Structural Mechanics and Control of Ministry of Education,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

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