Application of optimal control techniques to aircraft flutter suppression and load alleviation
- 10 May 1982
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Test demonstration of digital control of wing/store flutterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Practical gust load alleviation and flutter suppression control laws based on a LQG methodologyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- A direct method for synthesizing low-order optimal feedback control laws with application to flutter suppressionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Active flutter suppression control law definition via least squares synthesisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Recent development of the YF-17 active flutter suppression systemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Robustness with observersIEEE Transactions on Automatic Control, 1979
- Active flutter suppression - A flight test demonstrationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- A Feasibility Study of Active Wing/Store Flutter ControlJournal of Aircraft, 1972