Finite Element Modeling and Robust Vibration Control of Two-Hinged Plate Using Bonded Piezoelectric Sensors and Actuators
暂无分享,去创建一个
[1] P. Khargonekar,et al. State-space solutions to standard H/sub 2/ and H/sub infinity / control problems , 1989 .
[2] Yildirim Hurmuzlu,et al. Theoretical and experimental study of efficient control of vibrations in a clamped square plate , 2005 .
[3] P. Khargonekar,et al. State-space solutions to standard H2 and H∞ control problems , 1988, 1988 American Control Conference.
[4] Lei Yong-jun. Uncertainty modeling of structural dynamics for robust vibration control , 2009 .
[5] Shigemune Taniwaki,et al. Dynamic simulation of stick–slip motion of a flexible solar array , 2008 .
[6] P. Alan Jones,et al. Spacecraft solar array technology trends , 2011 .
[7] Lei Yong-jun. Structural dynamics modeling for robust vibration control in consideration of uncertainties , 2009 .
[8] Yong Xie,et al. Model Reduction and Active Control for a Flexible Plate , 2011 .
[9] Xianmin Zhang,et al. Optimal placement and active vibration control for piezoelectric smart flexible cantilever plate , 2007 .
[10] Indra Narayan Kar,et al. Bending and torsional vibration control of a flexible plate structure using H∞-based robust control law , 2000, IEEE Trans. Control. Syst. Technol..
[11] K. Chandrashekhara,et al. Active buckling control of smart composite plates-finite-element analysis , 1993 .
[12] Liang Wang,et al. Active H∞ control of the vibration of an axially moving cantilever beam by magnetic force , 2011 .
[13] J. N. Reddy,et al. A finite-element model for piezoelectric composite laminates , 1997 .
[14] Jian-Ping Jiang,et al. Optimal placement and decentralized robust vibration control for spacecraft smart solar panel structures , 2010 .
[15] M. Naushad Alam,et al. Finite element analysis of actively controlled smart plate with patched actuators and sensors , 2010 .