Design of control laws for flutter suppression based on the aerodynamic energy concept and comparisons with other design methods
Open Access
- 3 April 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
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- Reduced-Order Optimal Feedback Control Law Synthesis for Flutter SuppressionJournal of Guidance, Control, and Dynamics, 1982
- Practical gust load alleviation and flutter suppression control laws based on a LQG methodologyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Active Controls for Flutter Suppression and Gust Alleviation in Supersonic AircraftJournal of Guidance and Control, 1980
- Comparative Study Between Two Different Active Flutter Suppression SystemsJournal of Aircraft, 1978