A direct method for synthesizing low-order optimal feedback control laws with application to flutter suppression
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1980-1613
Reference26 articles.
1. tical Flutter Suppression Control Laws Using Results of Optimal Control Theory. NASA TP-1471, August 1979. Gangsaas, Dagfinn; and Ly, Uy-Loi : Applica
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