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

İlkay Gümüşboğa, Altuğ İftar (2020)

Kybernetika

Combat planes are designed in a structured relaxed static stability to meet maneuver requirements. These planes are unstable in the longitudinal axis and require continuous active control systems with elevator control. Therefore, failures in the elevator can have vital consequences for flight safety. In this work, the performance of classical control approach against asymmetric elevator failures is investigated and it is shown that this approach is insufficient in the case of such a failure. Then,...

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