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• W2069181866 abstract "This paper presents the design of fault tolerant flight control (FTC) law to deal with actuators loss of effectiveness. A Linear Quadratic Regulator (LQR) approach was considered as a baseline controller augmented with tracking equations to follow command reference inputs. Fault-compensation-based approach was applied to act against actuator faults. The designed FTC law was examined by analysing the aircraft's motion and the changes in actuators deflections. A mathematical model of the lateral motion of a DC-8 aircraft was used in this experiment. Simulation results showed that this technique is very effective to deal with actuator faults and to maintain the stability of the closed-loop system." @default.
• W2069181866 created "2016-06-24" @default.
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• W2069181866 date "2014-06-01" @default.
• W2069181866 modified "2023-09-26" @default.
• W2069181866 title "Fault tolerant flight control design against actuator impairments using optimal control and fault compensation" @default.
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• W2069181866 doi "https://doi.org/10.1109/icca.2014.6870947" @default.
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