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Aircraft fault diagnosis model generation method based on multi-sensor data driving

A fault diagnosis model and multi-sensor technology, applied in neural learning methods, biological neural network models, instruments, etc., can solve complex fault diagnosis and other problems, and achieve the effect of flexible use and small calculation amount

Pending Publication Date: 2022-04-15
CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP OF CHINA
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Problems solved by technology

[0007] Purpose of the present invention: In order to solve the complex fault diagnosis problem of the fighter system, according to the multi-dimensional data composed of data collected by multiple sensors of the fighter system, the present invention provides a method for generating an aircraft fault diagnosis model driven by multi-sensor data. Convolutional Neural Networks Extract Fault Features from Sensor Data

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  • Aircraft fault diagnosis model generation method based on multi-sensor data driving
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  • Aircraft fault diagnosis model generation method based on multi-sensor data driving

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Embodiment Construction

[0050] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0051] The present invention proposes a method for generating an aircraft fault diagnosis model driven by multi-sensor data, such as figure 1 As shown, the implementation of this method can be divided into three stages. The first stage is mainly to select the sensors that can be used for the fault diagnosis of the fighter jet system, collect the sensor data corresponding to different fault modes, store the sensor data in a two-dimensional forma...

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Abstract

The invention belongs to the technical field of aircraft fault diagnosis, and discloses an aircraft fault diagnosis model generation method based on multi-sensor data driving. The method comprises the steps of 1, selecting a sensor group capable of being used for aircraft fault diagnosis, and collecting historical acquisition data of the sensor group corresponding to various fault modes; preprocessing the collected data of the sensor group corresponding to each type of fault mode in one time period, and storing the preprocessed data as a two-dimensional multi-sensor data matrix, thereby obtaining T * Q two-dimensional multi-sensor data matrixes of the T types of fault modes in Q time periods; 2, randomly selecting the two-dimensional multi-sensor data matrixes and the corresponding fault modes as training samples, and taking the rest two-dimensional multi-sensor data matrixes and the corresponding fault modes as test samples; 3, establishing a convolutional neural network model; 4, training the convolutional neural network by using the training sample through a small-batch gradient descent method until a training condition is met; and 5, verifying a training result.

Description

technical field [0001] The invention belongs to the technical field of aircraft fault diagnosis, and in particular relates to an aircraft fault diagnosis model generation method driven by multi-sensor data. Background technique [0002] In order to improve flight safety and mission reliability, a large number of advanced technologies are adopted in the design of modern fighter jet systems, and the complexity and integration of the system are increasing day by day, which makes the fault diagnosis of fighter jet systems face more severe challenges. Once a fighter system fails, if it cannot be detected and dealt with in time, it will pose a serious threat to flight safety and mission reliability. [0003] In order to improve the health monitoring capability of fighter jets, a large number of sensors are arranged in the system design of modern fighter jets to monitor the working status of the system, and a large amount of monitoring data will be generated during the operation of...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/16G06F30/27G06K9/62G06N3/04G06N3/08
Inventor 何勃解海涛林健冯力
Owner CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP OF CHINA
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