Towards integrated multidisciplinary synthesis of actively controlled fiber composite wings
Author:
Affiliation:
1. University of California, Los Angeles, Los Angeles, California 90024
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45972
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1. Design of control laws for flutter suppression based on the aerodynamic energy concept and comparisons with other design methods
2. Design of a multivariable flutter suppression/gust load alleviation system
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