The invention discloses an airborne integrated task processor I / O interface module fault diagnosis method and
system, and relates to the technical field of
avionics equipment fault diagnosis. The method comprises the following steps of: acquiring partial analog quantity and digital quantity information from an I / O (Input / Output) interface module of an airborne integrated task processor, and acquiring corresponding temperature and vibration information through a temperature sensor and a
vibration sensor; after preprocessing and labeling, constructing a combined model based on an
attention network and a depth separable
convolution strategy; and training the combined model, and performing real-time fault diagnosis on the I / O interface module. Hardware protection is triggered for a permanent fault, and replacement of a fault module is prompted; for intermittent faults, fault types and
occurrence time are recorded, a degradation trend report is generated, and follow-up key monitoring is facilitated; according to the invention, additional acquisition equipment is reduced, the fault diagnosis accuracy of the I / O interface module of the IMP is improved, accurate fault positioning and targeted
processing are realized, and the reliability and
maintainability are improved.