Rotorcraft Control System Design for Uncertain Vehicle Dynamics Using Quantitative Feedback Theory
- 1 April 1994
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 39 (2) , 47-55
- https://doi.org/10.4050/jahs.39.47
Abstract
No abstract availableKeywords
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