Design of control laws for flutter suppression based on the aerodynamic energy concept and comparisons with other design methods
Author:
Affiliation:
1. NASA, Flight Research Center, Edwards, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-1212
Reference36 articles.
1. "Reduced-OrderOptimalFeedbackControlLawSynthesis for Flutter Suppression,''J. Guidance,Vol.5, No.4, July-Aug. 1982.
2. 'Gangsaas, D., Ly, U., and Norman, D.C. "Practical Gust Load Alleviation and Flutter Suppression Control LawsBasedon aLQGMethodology,"AIAA81-0021, 1981.
3. Application of matrix singular value properties for evaluating gain and phase margins of multiloop systems
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