Effective Selection of Piezoceramic Actuators for an Experimental Flexible Wing
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[1] Wodek Gawronski,et al. Actuator and Sensor Placement for Control of Flexible Structures , 1993 .
[2] W. Gawronski,et al. Balanced actuator and sensor placement for flexible structures , 1996 .
[3] K. Lim. Method for Optimal Actuator and Sensor Placement for Large Flexible Structures , 1992 .
[4] M. Phan,et al. Identification of observer/Kalman filter Markov parameters: Theory and experiments , 1993 .
[5] B. Moore. Principal component analysis in linear systems: Controllability, observability, and model reduction , 1981 .
[6] Stephen P. Boyd,et al. Linear controller design: limits of performance , 1991 .
[7] P. Khargonekar,et al. State-space solutions to standard H/sub 2/ and H/sub infinity / control problems , 1989 .
[8] Jer-Nan Juang,et al. An eigensystem realization algorithm for modal parameter identification and model reduction. [control systems design for large space structures] , 1985 .
[9] K B Lim. A Disturbance Rejection Approach to Actuator and Sensor Placement , 1997 .
[10] Gregory W. Reich,et al. Design and modeling of an active aeroelastic wing , 1994 .
[11] C. Gregory. Reduction of large flexible spacecraft models using internal balancing theory , 1984 .
[12] K B Lim,et al. Hankel Singular Values of Flexible Structures in Discrete Time , 1996 .
[13] David E. Cox,et al. Band-Limited Actuator and Sensor Selection for Disturbance Rejection , 1999 .