Active aeroelastic flutter analysis and vibration control of supersonic composite laminated plate

Song, Zhiguang; Li, Fengming

doi:10.1016/j.compstruct.2011.09.005

Cited by 126 publications

(37 citation statements)

References 40 publications

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“…Also, Lee and Kim [16] studied the stability and flutter behaviors for P-, S-and E-FGMs. While, active aeroelastic control of the plates using piezoelectric actuator and sensor have been investigated to suppress the nonlinear flutter behavior [17,18]. Further, a few research works have been performed static behaviors of FGM in the hygrothermal environments.…”

Section: Introductionmentioning

confidence: 99%

Aero-hygrothermal effects on stability regions for functionally graded panels

Lee

Kim

2015

Composite Structures

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Section: Introductionmentioning

confidence: 99%

Aero-hygrothermal effects on stability regions for functionally graded panels

Lee

Kim

2015

Composite Structures

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“…Numerical results demonstrated that the residual vibration was effectively eliminated and the desired antenna pointing was achieved in a much shorter duration. Song et al [16] studied the active vibration control of composite laminated plates through analysis of active aeroelastic flutter, besides, the dynamical model of the structural system is established by using Hamilton's principle with the assumed mode method.…”

Section: Introductionmentioning

confidence: 99%

Experimental Study of Flexible Plate Vibration Control by Using Two-Loop Sliding Mode Control Strategy

Yang

Lin

Liu

et al. 2016

J. Inst. Eng. India Ser. C

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It is well known that intelligent control theory has been used in many research fields, novel modeling method (DROMM) is used for flexible rectangular active vibration control, and then the validity of new model is confirmed by comparing finite element model with new model. In this paper, taking advantage of the dynamics of flexible rectangular plate, a two-loop sliding mode (TSM) MIMO approach is introduced for designing multiple-input multiple-output continuous vibration control system, which can overcome uncertainties, disturbances or unstable dynamics. An illustrative example is given in order to show the feasibility of the method. Numerical simulations and experiment confirm the effectiveness of the proposed TSM MIMO controller.

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“…Hua-ping et al [22] presented a kind of active vibration control method based on active damping and optimization design for driving load of multibody system. Song and Li [23] studied the active aeroelastic flutter analysis and vibration control with the piezoelectric patches. Shah and Ray [24] performed analysis of active control of vibration of thin laminated composite truncated circular conical shells.…”

Section: Introductionmentioning

confidence: 99%

Active vibration control of composite shallow shells: An integrated approach

Rahman¹,

Alam²,

Junaid³

2018

J. MECH. ENG. SCI.

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Active vibration control of smart composite shallow shells with distributed piezoelectric sensors and actuators is presented in this work. An integrated approach is used for recording the uncontrolled and controlled vibration response under pressure impulse load. The FE model developed in ABAQUS is utilized to generate the global mass, stiffness and load matrices of the system. The system matrices are arranged in statespace format and the dynamic equations of the system are obtained. The controlled responses are achieved using the inputs from FE model in ABAQUS in conjunction with the developed MATLAB codes for Constant Gain Velocity Feedback (CGVF) and Linear Quadratic Regulator (LQR) control strategies. The method is first validated by comparing the natural frequencies obtained using the ABAQUS generated matrices with that obtained using an FE model with four noded quadrilateral shallow shell element based on efficient zigzag theory. The shell element uses the concept of electric nodes to satisfy the equipotential condition of electrode surface. An 8-noded linear piezoelectric brick element is used for piezoelectric layers and an 8-noded quadrilateral continuum shell element is used for the elastic layers of hybrid shells for making the finite element mesh in ABAQUS. The non-dimensional natural frequencies and active vibration control responses for hybrid composite cylindrical and spherical shells are presented for clamped-clamped and cantilever boundary conditions. Boundary conditions have significant effect on vibration amplitude, control voltage and settling time. In comparison to CGVF controller, a better control in lesser time is achieved with LQR controller for a shell with similar boundary conditions. Larger gain values (G) are required for vibration control of thick shells.

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Active aeroelastic flutter analysis and vibration control of supersonic composite laminated plate

Cited by 126 publications

References 40 publications

Aero-hygrothermal effects on stability regions for functionally graded panels

Aero-hygrothermal effects on stability regions for functionally graded panels

Experimental Study of Flexible Plate Vibration Control by Using Two-Loop Sliding Mode Control Strategy

Active vibration control of composite shallow shells: An integrated approach

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