Abstract:In actual operating of the aircraft hydraulic system, the frequency of occurrence of the fault status is much lower than that of the normal status. The faults of the aircraft hydraulic system are very expensive to replicate, making it unrealistic to conduct a real fault simulation experiment of the aircraft hydraulic system. Hence, a large number of data samples related to the normal status of the aircraft hydraulic system is available but very few data samples related to the fault status. This causes a severe… Show more
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