Nonlinear response of asymmetrically laminated plates in cylindricalbending
Author:
Affiliation:
1. DIAS-Politecnico di Torino, Torino 10129, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference26 articles.
1. Experimental research on flexible beam modal control
2. 2Parks, T. R., and Pak, H. A., Journal of Dynamic Systems,Measurement, and Control, Vol.113, 1991,pp.409-418.
3. Feedback control of flexible systems
4. Control-augmented structural synthesis with dynamic stability constraints
5. Experiments in control of flexible structures with noncolocated sensors and actuators
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