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INTEGRATED FAULT TOLERANT FLIGHT CONTROL DESIGN WITH APPLICATION TO AN F-16 AIRCRAFT - MaRDI portal

INTEGRATED FAULT TOLERANT FLIGHT CONTROL DESIGN WITH APPLICATION TO AN F-16 AIRCRAFT

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Publication:3099454

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DOI10.2316/JOURNAL.201.2011.3.201-2208zbMath1237.93045OpenAlexW2060258990MaRDI QIDQ3099454

Publication date: 1 December 2011

Published in: Control and Intelligent Systems (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2316/journal.201.2011.3.201-2208

zbMATH Keywords

adaptive control robust control actuator faults fault tolerant control (FTC)aircraft systems

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Application models in control theory (93C95) Adaptive control/observation systems (93C40)

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