CN114754973A - Wind tunnel force measurement test data intelligent diagnosis and analysis method based on machine learning - Google Patents

Wind tunnel force measurement test data intelligent diagnosis and analysis method based on machine learning Download PDF

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CN114754973A
CN114754973A CN202210561316.2A CN202210561316A CN114754973A CN 114754973 A CN114754973 A CN 114754973A CN 202210561316 A CN202210561316 A CN 202210561316A CN 114754973 A CN114754973 A CN 114754973A
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刘博雅
王建锋
刘明远
谭浩
刘实
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Abstract

The invention discloses a wind tunnel force measurement test data intelligent diagnosis and analysis method based on machine learning, and belongs to the field of aerodynamics. The method is used for carrying out intelligent auxiliary analysis such as result prediction, abnormity early warning and the like on test data in the front, middle and rear stages of a large-scale low-speed wind tunnel force measurement test. The method is characterized in that a plurality of algorithms adapted to the wind tunnel force measurement test are combined, fitting degree and error evaluation indexes of each algorithm in the wind tunnel force measurement test are automatically compared, an optimal algorithm adapted to current test data is selected, and intelligent technical auxiliary analysis is further provided for reliability and stability of the pneumatic test. The method can accurately predict and analyze the hexatomic force coefficient of the large-scale low-speed wind tunnel force test, and provides an intelligent technical auxiliary analysis means for the reliability and stability of the large-scale low-speed wind tunnel pneumatic test.

Description

Wind tunnel force measurement test data intelligent diagnosis and analysis method based on machine learning
Technical Field
The invention belongs to the field of aerodynamics, and particularly relates to an intelligent diagnosis and analysis method for wind tunnel force measurement test data based on machine learning.
Background
With the continuous development and growth of aviation industry in China, the demand for aircraft development is continuously increased, so that higher requirements are put forward on the development period and the research and development efficiency of the aircraft. The wind tunnel test is taken as a key link in the research and development process of the aircraft, and the intelligent level of the wind tunnel test influences the research and development efficiency of the whole aviation model. The artificial intelligence technology is applied to the wind tunnel test, so that the model development efficiency and the wind tunnel test level can be greatly improved. The conventional wind tunnel force measurement test prediction algorithm adopts a machine learning or deep learning algorithm to predict wind tunnel test data, and although the method can reach a certain precision level, the selected algorithm is not the optimal algorithm although the precision meets the requirement due to different algorithm space complexity degrees and possibly the selected algorithm which is not the most suitable for the current data, and a large amount of time is consumed in the algorithm selection. Therefore, an intelligent diagnosis and analysis method for wind tunnel force measurement test data based on machine learning is needed.
Disclosure of Invention
Based on the defects, the invention aims to provide the intelligent diagnosis and analysis method for the wind tunnel force measurement test data based on machine learning, which combines a plurality of algorithms adapted to the wind tunnel force measurement test, automatically compares the fitting degree and the error evaluation index of each algorithm in the wind tunnel force measurement test, selects the optimal algorithm adapted to the current test data, and further provides intelligent technical auxiliary analysis for the reliability and the stability of the pneumatic test.
The technical scheme adopted by the invention is as follows: a wind tunnel force measurement test data intelligent diagnosis and analysis method based on machine learning comprises the following steps:
the method comprises the following steps: identifying all characteristic variables influencing the six-element force coefficient of the model according to the aerodynamic characteristics of the large-scale low-speed wind tunnel force test, extracting a large amount of historical wind tunnel test data, and processing the data to be used as training data of an algorithm;
step two: establishing a prediction learning machine of a large-scale low-speed wind tunnel test based on a deep learning algorithm of machine learning by utilizing the processed historical data;
step three: and the prediction learning machine is used for carrying out result prediction and intelligent analysis of abnormal early warning on the wind tunnel test result.
Further, the step (1) is specifically as follows: according to the aerodynamic characteristics of a large-scale low-speed wind tunnel force measurement test, test parameters are identified, the incidence angle, the sideslip angle, the aileron, the flap, the slat, the horizontal tail, the elevator and the rudder are determined as input characteristics of an algorithm, the six-membered force coefficients of the lift force, the resistance, the pitching moment, the lateral force, the yawing moment and the rolling moment of a model are determined as output characteristics of a prediction learning machine, training data of the prediction learning machine are obtained from a test historical database according to the identified algorithm input and output variables, data processing operation is carried out on an obtained historical training data set, the training data are divided and combined into a training data set according to input and output, data standardization analysis is adopted to carry out preprocessing on required data, and the formula is as follows:
Figure BDA0003656403090000021
in the formula:
Figure BDA0003656403090000022
representing the production parameters of the kth sample under n-dimensional data normalization,
Figure BDA0003656403090000023
representing that the kth sample arranges N-dimensional metadata according to time series, wherein K is the number of data sets, and N is the number of samples; and then performing data cleaning on the data processing data, including missing value processing and abnormal value processing.
Further, the step (2) is specifically as follows: selecting a support vector machine, a Lasso regression, a Gaussian process regression, a ridge regression and a deep neural network, and establishing a prediction learning machine by using the five machine learning algorithms; training the algorithm in the prediction learning machine by using the processed data, wherein the prediction learning machine forms five different algorithm models when algorithm training is carried out; the mean square error is used as an error evaluation index, and the formula is as follows:
Figure BDA0003656403090000031
in the formula: i is a training sample label, n is the number of training sample instances, yiFor the training set output value, xijFor the training set input value, betajIs a regression coefficient, and p is the number of the training set features;
selecting the fitting degree as a fitting degree evaluation index output by the algorithm, wherein the formula is as follows:
Figure BDA0003656403090000032
in the formula: ESS is the regression sum of squares, TSS is the total dispersion sum of squares,
Figure BDA0003656403090000033
in order to predict the output for the algorithm,
Figure BDA0003656403090000034
to train sample mean, yiIs a training sample; and (4) sorting the five groups of fitness and mean square error evaluation indexes output by the prediction learning machine, autonomously judging the statistical index of the fitness and the root mean square error by the learning machine, and preferentially selecting the algorithm with the highest fitness and the smallest error as the final prediction algorithm.
Further, the method of step (3) is specifically as follows: and (3) inputting algorithm input data acquired and identified in real time, transmitting the algorithm input data to a prediction learning machine for real-time prediction operation, comparing a real-time prediction value of the prediction learning machine with a real acquisition value of a sensor, and triggering fault early warning by a system when a difference value outside an error allowable range occurs.
The invention has the advantages that: the method is used for carrying out intelligent auxiliary analysis such as result prediction, abnormity early warning and the like on the test data in the front, middle and rear stages of the wind tunnel test, can more clearly and quickly find a more accurate prediction algorithm which is adaptive to the current test data, and provides intelligent technical auxiliary analysis for the reliability and stability of the large-scale low-speed wind tunnel pneumatic test.
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FIG. 1 is an overall flow chart of the analytical method of the present invention;
FIG. 2 is a data processing flow diagram of the present invention;
FIG. 3 is a flow chart of data cleansing according to the present invention;
Detailed Description
The invention is further illustrated by way of example in the accompanying drawings of the specification:
example 1
The embodiment provides an intelligent diagnosis and analysis method for wind tunnel force measurement test data based on machine learning according to existing large-scale low-speed wind tunnel force measurement test data. The overall working flow of the method is shown in figure 1, and the specific steps are as follows:
step (1): the method comprises the following steps of identifying and processing test parameters of a large-scale low-speed wind tunnel force measurement test, and specifically comprising the following steps:
step (1.1): according to the aerodynamic characteristics of a large-scale low-speed wind tunnel force measurement test, identifying test parameters, determining an attack angle, a sideslip angle, an aileron, a flap, a slat, a horizontal tail, an elevator and a rudder as input characteristics of an algorithm, and determining six-element force coefficients of a lift force, a resistance force, a pitching moment, a lateral force, a yawing moment and a rolling moment of a model as output characteristics of a prediction learning machine;
step (1.2): acquiring training data of a prediction learning machine from a test historical database according to the algorithm input and output variables identified in the step (1.1), performing data processing operation on the acquired historical training data set, and dividing the training data according to input and output to synthesize a training data set;
because the dimensions and units of the data vectors output by simulation are different, the flow chart is shown in fig. 2, and data standardization analysis is adopted to preprocess the required data, and the formula is as follows:
Figure BDA0003656403090000051
in the formula:
Figure BDA0003656403090000052
representing the production parameters of the kth sample under n-dimensional data normalization,
Figure BDA0003656403090000053
it means that the kth sample arranges N-dimensional metadata in time series, K is the number of data sets, and N is the number of samples.
Step (1.3): and (3) performing data cleaning on data processing data, wherein a flow chart is shown in fig. 3, and comprises missing value processing and abnormal value processing, and a mean value/median/mode, a regression method, a lagrange interpolation/newton interpolation method are adopted for interpolation of missing values.
Step (2): establishing a large-scale low-speed wind tunnel test prediction learning machine based on machine learning and deep learning algorithms by utilizing the processed historical data, and specifically comprising the following steps of:
step (2.1): selecting a support vector machine, a Lasso regression, a Gaussian process regression, a ridge regression and a deep neural network, and constructing and combining the five machine learning algorithms by using a Python language and a TensorFlow2.0 frame to form a prediction learning machine for a large-scale low-speed wind tunnel force measurement test;
step (2.2): training an algorithm in a prediction learning machine by using the data processed in the step (1), wherein the prediction learning machine forms five different algorithm models when algorithm training is carried out;
step (2.3): the mean square error is used as an error evaluation index, and the formula is as follows:
Figure BDA0003656403090000061
in the formula: i is a training sample label, n is the number of training sample instances, yiFor the training set output value, xijFor the training set input value, betajIs a regression coefficient, and p is the number of the training set features;
selecting the fitting degree as a fitting degree evaluation index output by the algorithm, wherein the formula is as follows:
Figure BDA0003656403090000062
in the formula: ESS is the regression sum of squares, TSS is the total dispersion sum of squares,
Figure BDA0003656403090000063
in order to predict the output for the algorithm,
Figure BDA0003656403090000064
to train sample mean, yiAre training samples.
Step (2.4): and (4) sorting the five groups of fitness and mean square error evaluation indexes output by the prediction learning machine, autonomously judging the statistical index of the fitness and the root mean square error by the learning machine, and preferentially selecting the algorithm with the highest fitness and the smallest error as the final prediction algorithm.
And (3): the intelligent analysis and early warning method for the large-scale low-speed wind tunnel force measurement test comprises the following concrete implementation steps:
step (3.1): collecting the identified algorithm input data in real time, and transmitting the algorithm input data to a large low-speed wind tunnel prediction learning machine for real-time prediction operation;
step (3.2): and comparing the real-time predicted value of the prediction learning machine with the real acquisition value of the sensor, and triggering fault early warning by the system when a difference value outside an error allowable range occurs.
According to the method, the aerodynamic characteristics of the existing large-scale low-speed wind tunnel force test are comprehensively considered, advanced means such as machine learning and deep learning are combined, the model six-element force coefficient of the force test is predicted and analyzed, accurate prediction and analysis can be carried out on the six-element force coefficient of the large-scale low-speed wind tunnel force test, and intelligent technical auxiliary analysis is provided for the reliability and stability of the large-scale low-speed wind tunnel pneumatic test.

Claims (4)

1. A wind tunnel force measurement test data intelligent diagnosis and analysis method based on machine learning is characterized by comprising the following steps:
the method comprises the following steps: identifying all characteristic variables influencing the six-element force coefficient of the model according to the aerodynamic characteristics of the large-scale low-speed wind tunnel force test, extracting a large amount of historical wind tunnel test data, and processing the data to be used as training data of an algorithm;
step two: establishing a prediction learning machine of a large-scale low-speed wind tunnel test based on a deep learning algorithm of machine learning by utilizing the processed historical data;
step three: and the prediction learning machine is used for carrying out result prediction and intelligent analysis of abnormal early warning on the wind tunnel test result.
2. The wind tunnel force measurement test data intelligent analysis and early warning method based on machine learning as claimed in claim 1, wherein the step (1) is as follows: according to the aerodynamic characteristics of a large-scale low-speed wind tunnel force measurement test, test parameters are identified, the incidence angle, the sideslip angle, the aileron, the flap, the slat, the horizontal tail, the elevator and the rudder are determined as input characteristics of an algorithm, the six-membered force coefficients of the lift force, the resistance, the pitching moment, the lateral force, the yawing moment and the rolling moment of a model are determined as output characteristics of a prediction learning machine, training data of the prediction learning machine are obtained from a test historical database according to the identified algorithm input and output variables, data processing operation is carried out on an obtained historical training data set, the training data are divided and combined into a training data set according to input and output, data standardization analysis is adopted to carry out preprocessing on required data, and the formula is as follows:
Figure FDA0003656403080000011
in the formula:
Figure FDA0003656403080000012
representing the production parameters of the kth sample under n-dimensional data normalization,
Figure FDA0003656403080000013
representing that the kth sample arranges N-dimensional metadata according to time series, wherein K is the number of data sets, and N is the number of samples; and then performing data cleaning on the data processing data, wherein the data cleaning comprises missing value processing and abnormal value processing.
3. The wind tunnel dynamometry test data intelligent analysis and early warning method based on machine learning as claimed in claim 2, wherein step (2) is as follows: selecting a support vector machine, a Lasso regression, a Gaussian process regression, a ridge regression and a deep neural network, and establishing a prediction learning machine by using the five machine learning algorithms; training an algorithm in the prediction learning machine by using the processed data, wherein the prediction learning machine forms five different algorithm models when algorithm training is carried out; the mean square error is used as an error evaluation index, and the formula is as follows:
Figure FDA0003656403080000021
in the formula: i is a training sample label, n is the number of training sample instances, yiFor the training set output value, xijFor the training set input value, betajIs a regression coefficient, and p is the number of the training set features;
selecting the fitting degree as a fitting degree evaluation index output by the algorithm, wherein the formula is as follows:
Figure FDA0003656403080000022
in the formula: ESS isAnd returning to the sum of squares, TSS is the sum of squared deviations,
Figure FDA0003656403080000023
in order to predict the output for the algorithm,
Figure FDA0003656403080000024
to train sample mean, yiIs a training sample; and (4) sorting the five groups of fitness and mean square error evaluation indexes output by the prediction learning machine, autonomously judging the statistical index of the fitness and the root mean square error by the learning machine, and preferentially selecting the algorithm with the highest fitness and the smallest error as the final prediction algorithm.
4. The machine learning-based wind tunnel force measurement test data intelligent analysis and early warning method according to claim 3, wherein the step (3) is as follows: and (3) inputting algorithm input data acquired and identified in real time, transmitting the algorithm input data to a prediction learning machine for real-time prediction operation, comparing a real-time prediction value of the prediction learning machine with a real acquisition value of a sensor, and triggering fault early warning by a system when a difference value outside an error allowable range occurs.
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