지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 저널정보
- 한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.15 Number.1
- 발행연도
- 2014.3
- 수록면
- 1 - 19 (19page)
이용수
초록· 키워드
오류제보하기
Attaching a piezoelectric transducer to a vibrating structure, and shunting it with an electric circuit, gives rise to different passive, semi-passive, and semi-active control techniques. This paper attempts to review the research related to structural vibration control, via passive, semi-passive, and semi-active control methods. First, the existing electromechanical modeling is reviewed, along with the modeling methods. These range from lumped parameters, to distributed parameters modeling of piezostructural systems shunted by electrical networks. Vibration control laws are then discussed, covering passive, semi-passive, and semi-active control techniques, which are classified according to whether external power is supplied to the piezoelectric transducers, or not. Emphasis is placed on recent articles covering semi-passive and semi-active control techniques, based upon switched shunt circuits. This review provides the necessary background material for researchers interested in the growing field of vibration damping and control, via shunted piezostructural systems.
목차
Abstract
1. Introduction
2. Modeling of Shunted Piezostructural Systems
3. Control Laws for Shunted Piezostructural Systems
4. Conclusion and Future Direction
References
참고문헌 (86)
참고문헌 신청
Hopkins, M. A. / 1998 / Active vibrationsuppression systems applied to twin-tail buffering / Proc. SPIE Smart Structures and Materials: Industrial and Commercial Application of Smart Structures Technologies 3326:27~33
Simpson, J. / 1998 / Industrial approach to piezoelectric damping of large fighter aircraft components / Proc. SPIE Smart Structures and Materials: Industrial and Commercial Application of Smart Structures Technologies 3326:34~46
Kim, S. / 1999 / Improvement of aeroelastic stability of hingeless helicopter rotor blade by passive piezoelectric damping / Proc. SPIE Smart Structures and Materials: Passive Damping and Isolation 3672:131~141
Wu, S. / 2000 / Piezoelectric shunt vibration damping of an F-15 panel under high-acoustic excitation / Proc. SPIE Smart Structures and Materials:Damping and Isolation 3989:276~287
Sheta, E. F. / 2006 / Active smart material control system for buffet alleviation / Journal of Sound and Vibration 292(3-5):854~868
Simpson, J. / 1998 / Industrial approach to piezoelectric damping of large fighter aircraft components / Proc. SPIE Smart Structures and Materials: Industrial and Commercial Application of Smart Structures Technologies 3326:34~46
Kim, S. / 1999 / Improvement of aeroelastic stability of hingeless helicopter rotor blade by passive piezoelectric damping / Proc. SPIE Smart Structures and Materials: Passive Damping and Isolation 3672:131~141
Wu, S. / 2000 / Piezoelectric shunt vibration damping of an F-15 panel under high-acoustic excitation / Proc. SPIE Smart Structures and Materials:Damping and Isolation 3989:276~287
Sheta, E. F. / 2006 / Active smart material control system for buffet alleviation / Journal of Sound and Vibration 292(3-5):854~868
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