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Machine learning sample generation method for aircraft thrust fault on-line identification

A machine learning and aircraft technology, applied in instruments, general control systems, electrical testing/monitoring, etc., can solve problems such as large gaps with real data, affecting flight identification accuracy, and limited real data, so as to achieve improved identification accuracy and real data. Credibility, the effect of improving the accuracy of fault identification

Active Publication Date: 2020-06-05
BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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AI Technical Summary

Problems solved by technology

[0002]Due to limited real data, aircraft fault identification technology based on machine learning mostly relies on aircraft simulation models to generate a large number of machine learning samples. If the model is inaccurate or far from the real model , it will greatly affect the actual flight identification accuracy
Existing machine learning fault identification can achieve high accuracy in simulation tests, but the effect is often not good in practical applications, mostly due to the large gap between machine learning sample data and real data
Moreover, the current machine learning sample data is large in scale, takes up large computing resources, affects computing efficiency, and is not suitable for computing hardware with limited computing power

Method used

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  • Machine learning sample generation method for aircraft thrust fault on-line identification
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  • Machine learning sample generation method for aircraft thrust fault on-line identification

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Embodiment Construction

[0043] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0044]The invention relates to a machine learning sample generation method for online identification of aircraft thrust faults, which is suitable for the field of online identification of typical power system faults during aircraft flight. Carry out data fusion generation for the flight motion information of the control system (such as flight position, speed, acceleration, attitude angle, angular velocity, etc.), and intercept the corresponding data according to the design method of the present invention as machine learning training and testing samples. The invention considers factors such as center-of-mass motion, center-of-disturbance motion, structural interference, aerodynamic force, moment, etc. of the aircraft, and introduces deviation combination cycles into the simulation model to generate data, so that the data is more authentic and r...

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Abstract

The invention relates to a machine learning sample generation method for aircraft thrust fault on-line identification, and the method is suitable for the field of typical power system fault on-line identification in the aircraft flight process. Data fusion generation is carried out on flight motion information (such as flight position, speed, acceleration, attitude angle and angular speed) of a control system, and corresponding data is intercepted as a machine learning training and testing sample according to the design method provided by the invention. Factors such as mass center motion, disturbance center motion, structural disturbance, aerodynamic force and moment of force of the aircraft are considered, deviation combination circulation is introduced into the simulation model to generate data, the data is more real and credible, and improvement of actual fault identification precision is facilitated. According to the method, the fault mode is refined, related data with relatively fine granularity of the fault mode is generated, and the identification precision is improved.

Description

technical field [0001] The invention relates to a machine learning sample generation method for online identification of aircraft thrust faults, which is suitable for the field of online identification of faults during the flight of launch vehicles. Background technique [0002] Due to limited real data, aircraft fault identification technology based on machine learning mostly relies on aircraft simulation models to generate a large number of machine learning samples. If the model is inaccurate or has a large gap with the real model, it will greatly affect the accuracy of actual flight identification. Existing machine learning fault identification can achieve high accuracy in simulation tests, but the effect is often not good in practical applications, mostly because of the large gap between machine learning sample data and real data. Moreover, the current machine learning sample data is large in scale, takes up large computing resources, affects computing efficiency, and is...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B23/02
CPCG05B23/0256G05B2219/24065Y02T90/00
Inventor 郜诗佳柳嘉润翟雯婧徐颂施健峰胡任祎潘豪张惠平禹春梅马卫华
Owner BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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