2014
DOI: 10.1016/s0894-9166(14)60025-2
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Finite element modeling and robust vibration control of two-hinged plate using bonded piezoelectric sensors and actuators

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Cited by 10 publications
(6 citation statements)
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“…Based on Timoshenko beam theory and the Hamilton principle, the vibration control equation of a beam with distributed internal viscous damping was established in paper [ 27 ], and the frequency equation of the beam was gained by using transfer matrix method. There are some papers [ 28 , 29 , 30 , 31 ] which carried out a further exploration in improving and optimizing the active passive constrained layer damping structure. The purpose of these papers was to select the optimal parameters of an ACLD structure through the research and simulation, so that the vibration performance of the structure can reach the optimal state.…”
Section: Introductionmentioning
confidence: 99%
“…Based on Timoshenko beam theory and the Hamilton principle, the vibration control equation of a beam with distributed internal viscous damping was established in paper [ 27 ], and the frequency equation of the beam was gained by using transfer matrix method. There are some papers [ 28 , 29 , 30 , 31 ] which carried out a further exploration in improving and optimizing the active passive constrained layer damping structure. The purpose of these papers was to select the optimal parameters of an ACLD structure through the research and simulation, so that the vibration performance of the structure can reach the optimal state.…”
Section: Introductionmentioning
confidence: 99%
“…19 Chen 20 utilized shape memory alloy wires as actuator and investigated vibration control of solar array by introducing classic linear optimal control theory. Abdeljaber et al 21 and Qiu et al 2225 presented an active vibration control method subjected to plate-type flexible structure on the spacecraft by piezoelectric actuator and sensor as well as nonlinear adaptive golden section controller or intelligent neural network controller. Hu 26 simplified solar array as a cantilever beam, and discussed the coupling control problem of the attitude motion of spacecraft and the vibration of solar array by pasting piezoelectric actuators and sensors.…”
Section: Introductionmentioning
confidence: 99%
“…Among these, optimal control techniques (LQR, LQG, H∞, etc) offer several advantages, such as possibility of trade-off between achievable vibration attenuation and required control inputs, simultaneous suppression of multiple modes, unified and systematic controller design procedure for MIMO systems. Although optimal control techniques offer obvious advantages and have been used for active vibration control (Chang et al., 2002; Iorga et al., 2008, 2009; Jiang and Li, 2011; Kumar, 2013; Qiu and Ling, 2014; Sethi et al., 2011; Vasques and Dias Rodrigues, 2006; Xie et al., 2004), a major limitation in their application has been the phenomena of spillover (Preumont, 2011; Vasques and Dias Rodrigues, 2006). Unlike some control techniques (velocity feedback, positive position feedback, etc) for which asymptotic stability against spillover can be guaranteed by using collocated actuator/sensor pairs; use of collocated actuator/sensor pairs doesn’t offer any distinguished advantage for avoiding spillover with optimal controllers.…”
Section: Introductionmentioning
confidence: 99%