Abstract
In this paper we present a fault-tolerant, reliable flight control scheme for Bell-205 Helicopter for the lateral dynamics case. The scheme is featured by integration of an Artificial Neural Network (ANN) based fault detection, isolation, and accommodation (FDIA) system and an H∞ mixed-sensitivity robust controller. The delay problem caused by the computational overhead of ANNs is addressed in the design. The robustness of the system is analyzed using Small Gain Theorem and μ J.L analysis
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