Single modal vibration control of laminated plates based on the optimal placement of a sensor and an actuator

Masaki Kameyama, Hisao Fukunaga

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The present paper treats structural vibration control for a specific single mode using the modal sensor and actuator. A modal sensor system for identifying the specific vibration mode, which is mechanically simple, is developed by one point sensor and one band-pass filter so as to be easily equipped to the structures. A sensor and actuator pair is optimally placed so that the best accuracy of measurement of modal velocity and the maximal control effect can be acquired. The proposed vibration control system is effective for suppression of single modal vibration as shown through experimental results.

Original languageEnglish
Title of host publication18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings
PublisherIFAC Secretariat
Pages235-240
Number of pages6
EditionPART 1
ISBN (Print)9783902661968
Publication statusPublished - 2010 Jan 1
Event18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Nara, Japan
Duration: 2010 Sep 62010 Sep 10

Publication series

NameIFAC Proceedings Volumes (IFAC-PapersOnline)
NumberPART 1
Volume18
ISSN (Print)1474-6670

Other

Other18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010
CountryJapan
CityNara
Period10/9/610/9/10

Keywords

  • Active control
  • Actuators
  • Band-pass filter
  • Composite materials
  • Optimal placement
  • Sensors
  • Vibration

ASJC Scopus subject areas

  • Control and Systems Engineering

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  • Cite this

    Kameyama, M., & Fukunaga, H. (2010). Single modal vibration control of laminated plates based on the optimal placement of a sensor and an actuator. In 18th IFAC Symposium on Automatic Control in Aerospace, ACA 2010 - Proceedings (PART 1 ed., pp. 235-240). (IFAC Proceedings Volumes (IFAC-PapersOnline); Vol. 18, No. PART 1). IFAC Secretariat.