Robust integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques
- 31 January 1993
- journal article
- Published by Elsevier in Automatica
- Vol. 29 (1) , 129-145
- https://doi.org/10.1016/0005-1098(93)90177-u
Abstract
No abstract availableKeywords
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