A New Approach for Active Control of Rotorcraft Vibration
- 1 March 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 5 (2), 143-150
- https://doi.org/10.2514/3.56151
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Frequency-shaped cost functionals - Extension of linear-quadratic-Gaussian design methodsJournal of Guidance and Control, 1980