Shock tunnel force measurement signal frequency domain analysis method based on deep learning

A technology of shock wave wind tunnel and deep learning, which is applied in the testing of machines/structural components, measuring devices, aerodynamic tests, etc., can solve problems such as inability to effectively filter out interference signals and affect the accuracy of aerodynamic measurement, and achieve Effect of Improving Reliability and Accuracy Indicators

Active Publication Date: 2022-01-25
INST OF MECHANICS - CHINESE ACAD OF SCI
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Problems solved by technology

[0004] The purpose of the present invention is to provide a frequency-domain analysis method for shock tunnel force measurement signals based on deep learning, so as to solve the technical problem that the prior art cannot effectively filter out interference signals, thereby affecting the accuracy of aerodynamic measurement

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  • Shock tunnel force measurement signal frequency domain analysis method based on deep learning
  • Shock tunnel force measurement signal frequency domain analysis method based on deep learning
  • Shock tunnel force measurement signal frequency domain analysis method based on deep learning

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Embodiment Construction

[0054] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. 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.

[0055] Such as figure 1 As shown, the present invention provides a frequency-domain analysis method based on deep learning for the shock wave wind tunnel force measurement signal. This embodiment reproduces the balance output signal of the force measurement system of the wind tunnel, and converts it into a frequency domain through the frequency domain analysis method Signal data, train the CNN intelligent model that can accurately identify the dynamic characte...

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Abstract

The invention discloses a shock tunnel force measurement signal frequency domain analysis method based on deep learning. The method comprises the steps of: building a shock tunnel aerodynamic force measurement system, and collecting a plurality of balance sample signals in a time domain based on an SVDC technology; decomposing the balance sample signal by adopting wavelet transform to obtain sub-signals, and performing time-frequency conversion on the sub-signals to obtain effective characteristic signals; performing fast Fourier transform on the effective feature signals in the time domain to obtain frequency domain signals converted to a spectrogram, and performing dimensionless processing on the frequency domain signals; training a convolutional neural network model, and performing intelligent modeling on the frequency domain signals by using the convolutional neural network model to obtain effective output signals after convolution circulation; and performing dimensionalization processing and inverse fast Fourier transform on the effective output signals to obtain filtered aerodynamic force signals in a time domain. Inertial vibration signals are filtered, real aerodynamic force signals are obtained, and reliability and precision indexes of pulse wind tunnel force measurement results are improved.

Description

technical field [0001] The invention relates to the technical field of wind tunnel force measurement signal test, in particular to a frequency domain analysis method for shock wave wind tunnel force measurement signal based on deep learning. Background technique [0002] The measurement method of the pulse strain balance is mostly to measure the voltage change of the strain gauge caused by the deformation of the fast response model under the impact load, and then reflect the model load, because of its large overall structure rigidity, low interference between components, high output sensitivity, The characteristics of strong stability and high precision are widely used in hypersonic vehicle force testing and so on. During the dynamometric test, the dynamometric system generates inertial vibration under the impulse excitation of the instantaneous start of the wind tunnel flow field. Due to the limitation of the effective running time of the wind tunnel and the complexity of t...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M9/06
CPCG01M9/065
Inventor 汪运鹏聂少军姜宗林
Owner INST OF MECHANICS - CHINESE ACAD OF SCI
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