Linear optimal theory applied to active structural bending control.
- 1 September 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 5 (5), 479-485
- https://doi.org/10.2514/3.43970
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- On cancellations, controllability and observabilityIEEE Transactions on Automatic Control, 1964