Fault-tolerant pitch-rate control augmentation system design for asymmetric elevator failures in a combat plane

DOI10.14736/kyb-2020-4-0767zbMath1474.93049OpenAlexW3092614869MaRDI QIDQ5140472

İlkay Gümüşboğa, Altuğ İftar

Publication date: 15 December 2020

Published in: Kybernetika (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/10338.dmlcz/148383

zbMATH Keywords

robust controlfault-tolerant controlflight controlasymmetric elevator failurescontrol augmentation system

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Application models in control theory (93C95)

Uses Software

• Matlab
• Simulink

Cites Work

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• Adaptive actuator failure compensation for nonlinear MIMO systems with an aircraft control application
• Robust optimal PID controller design for attitude stabilization of flexible spacecraft

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