Aircraft fault diagnosis method, model training method, device and computer equipment

By constructing an atmospheric parameter model and a traceless Kalman filtering model, extracting multi-dimensional new information and residual sequences, and calling a pre-trained aircraft fault diagnosis model, the accuracy and reliability problems of aircraft atmospheric data system fault diagnosis in the existing technology are solved, and timely and accurate diagnosis of aircraft faults is achieved.

CN118839260BActive Publication Date: 2025-03-18NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Patent Information

Application Number
CN202410844381.5
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2024-06-27
Publication Date
2025-03-18
Estimated Expiration
2044-06-27

AI Technical Summary

Technical Problem

The prior art is difficult to accurately diagnose the faults of the aircraft atmospheric data system in harsh flight environments, especially small-scale faults and fault diagnosis in uncertain flight conditions.

Method used

By obtaining the measurement information of the atmospheric data system and inertial navigation system in the aircraft system, an atmospheric parameter model is constructed, and a traceless Kalman filtering model is established based on this, multi-dimensional new information and residual sequences are extracted as input, and a pre-trained aircraft fault diagnosis model is called for diagnosis.

Benefits of technology

It realizes accurate diagnosis of the aircraft's atmospheric data system faults, improves the fault detection capability in harsh environments and uncertain states, and ensures the safe flight of the aircraft.

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Abstract

The present application relates to an aircraft fault diagnosis method, a model training method, an apparatus, a computer device and a storage medium. The method comprises: obtaining the measurement information and other auxiliary information of the atmospheric data system and the inertial navigation system in the aircraft system, and constructing an atmospheric parameter model; constructing an unscented Kalman filter model of the atmospheric data system based on the atmospheric parameter model, and estimating the state of the atmospheric data system according to the unscented Kalman filter model; extracting the multidimensional new information and residual sequence of the unscented Kalman filter model; calling the pre-trained aircraft fault diagnosis model, and taking the multidimensional new information and residual sequence as input parameters to obtain the aircraft fault diagnosis result. The combination of model and data is conducive to timely and accurate diagnosis of aircraft atmospheric data system faults, and provides guarantee for the safe flight of the aircraft.
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