Reduced-Order Optimal Feedback Control Law Synthesis for Flutter Suppression
- 1 July 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 5 (4), 389-395
- https://doi.org/10.2514/3.56187
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Robustness with observersIEEE Transactions on Automatic Control, 1979
- Optimal limited state variable feedback controllers for linear systemsIEEE Transactions on Automatic Control, 1971