Single Modal Vibration Control of Laminated Plates based on the Optimal Placement of a Sensor and an Actuator
暂无分享,去创建一个
[1] Edward F. Crawley,et al. Intelligent structures for aerospace - A technology overview and assessment , 1994 .
[2] Richard W. Longman,et al. Active Control Technology for Large Space Structures , 1993 .
[3] 成之 川畑,et al. センサ・アクチュエータの最適配置に基づくCFRP積層板の振動計測・振動制御 第1報 数値シミュレーション , 2004 .
[4] H. Tzou,et al. Collocated independent modal control with self-sensing orthogonal piezoelectric actuators (theory and experiment) , 1994 .
[5] Liyong Tong,et al. Vibration Control of Plates Using Discretely Distributed Piezoelectric Quasi-Modal Actuators/Sensors , 2001 .
[6] Fu-Kuo Chang,et al. Manufacturing of composite structures with a built-in network of piezoceramics , 1998 .
[7] Marcelo A. Trindade,et al. Optimization of modal filters based on arrays of piezoelectric sensors , 2009 .
[8] Suhuan Chen,et al. Integrated structural and control optimization of intelligent structures , 1999 .
[9] Francis C. Moon,et al. Modal Sensors/Actuators , 1990 .
[10] William W. Clark,et al. A Novel Semi-Active Multi-Modal Vibration Control Law for a Piezoceramic Actuator , 2003 .