Title :
Active vibration control of a fully clamped laminated composite plate subjected to impulsive pressure loadings
Author_Institution :
Turkish Air Force Acad., Istanbul, Turkey
Abstract :
In this numerical study vibrations of a fully clamped composite plate subjected to impulsive pressure loadings are controlled by using piezoelectric patches. Finite element methods are preferred for numerical solutions. For obtaining finite element model of the smart plate structure, semiloof shell finite element including piezoelectric effects is used. Mode summation method is used for reducing the degrees of freedom of the finite element model and state-space equations are obtained from the reduced finite element model for determining appropriate control strategies. Optimal linear quadratic regulator (LQR) approach has been used to determine the feedback gain matrix and vibrations of the plate suppressed successfully.
Keywords :
feedback; finite element analysis; intelligent structures; laminates; linear quadratic control; matrix algebra; piezoelectric materials; piezoelectricity; plates (structures); vibration control; active vibration control; feedback gain matrix; finite element methods; fully clamped laminated composite plate; impulsive pressure loadings; mode summation method; optimal linear quadratic regulator approach; piezoelectric effects; piezoelectric patches; semiloof shell finite element; smart plate structure; state-space equations; Aerospace industry; Aerospace materials; Composite materials; Equations; Finite element methods; Force control; Piezoelectric effect; Pressure control; Structural shells; Vibration control; blast load; component; piezoelectric; semiloof shell element; vibration control;
Conference_Titel :
Recent Advances in Space Technologies, 2009. RAST '09. 4th International Conference on
Conference_Location :
Istanbul
Print_ISBN :
978-1-4244-3627-9
Electronic_ISBN :
978-1-4244-3628-6
DOI :
10.1109/RAST.2009.5158190