Stabilization via dynamic output feedback - A numerical approach
- 1 September 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 14 (5) , 1083-1086
- https://doi.org/10.2514/3.20760
Abstract
No abstract availableKeywords
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