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A Dynamic Calibration Method of High Frequency Base Force Balance

A calibration method and balance technology, applied in aerodynamic tests, machine/structural component testing, instruments, etc., can solve problems such as rough approximation, modal damping ratio recognition error, and influence on signal separation effect, so as to simplify the test steps , Good power calibration effect, reliable separation effect

Active Publication Date: 2018-02-23
SOUTH CHINA UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] Among the above methods, the BMS natural frequency and damping ratio identified by the conventional tapping method in method 1 cannot reflect the influence of wind-structure interaction (WSI). This problem also exists in method 2. Ignoring the WSI effect will lead to the BMS natural frequency In particular, the error in the identification of the modal damping ratio will affect the correction effect of the measurement signal at the cross-resonance peak, so that the signal cannot be effectively corrected across the resonance region; method 2 uses a preconceived method to assume the mode shape of the BMS, This is equivalent to thinking that the signal separation matrix of the BMS is assumed. This method obviously violates the basic principles of parameter identification. When the assumed mode shape does not match the mode shape of the actual model, it will affect the separation effect of the signal, and then affect the natural frequency. And the correct identification of the damping ratio, in the end, it is also impossible to effectively correct the signal across the resonance region; method 3 is only a rough approximation when no reasonable solution is found
In summary, the existing methods have a certain positive effect on the correction of the distortion degree of the measured signal within a certain frequency range, but there are still deficiencies.

Method used

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  • A Dynamic Calibration Method of High Frequency Base Force Balance
  • A Dynamic Calibration Method of High Frequency Base Force Balance
  • A Dynamic Calibration Method of High Frequency Base Force Balance

Examples

Experimental program
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Embodiment 1

[0069] A dynamic calibration method for high-frequency base force balances for proportional damping, such as figure 1 , including the following steps:

[0070] Step 1: Whiten the measured signal x(t) to obtain the whitened signal z(t);

[0071] Step 2: Seek the orthogonal matrix V so that z(t)=Vq(t), and then calculate the separation signal q(t);

[0072] Step 3: Under the modal coordinates, identify the natural frequency and modal damping ratio of the separated signal;

[0073] Step 4: Correct the separation signal according to the identified parameters;

[0074] Step 5: Inversely infer from the corrected separation signal to obtain the corrected aerodynamic load.

[0075] Specifically, let the mixed model be

[0076] x(t)=Φq(t) (1)

[0077] where x(t), Φ and q(t) are the model base load (overturning moment, torque and shear force), mixing matrix and source signal (ie, modal response signal) measured by HFFB, respectively. The source signal q(t) obtains the observed sig...

Embodiment 2

[0145] A method for dynamic calibration of high-frequency base force balances for non-proportional damping, such as figure 2 , including the following steps:

[0146] Step 1: Signal preprocessing: shift the phase of the measurement signal x(t) by 90° to get x 90 (t), and then assemble the two into a complex signal;

[0147] Step 2: Whiten the assembled complex signal;

[0148] Step 3: Find the orthogonal matrix V, calculate the complex mixing matrix Φ and the complex separation matrix B, and then obtain the complex separation signal q(t);

[0149] Step 4: Under the modal coordinates, perform modal parameter identification on the complex separation signal;

[0150] Step 5: Correct the complex separation signal according to the identified parameters;

[0151] Step 6: Inversely infer from the corrected complex separation signal to obtain the corrected aerodynamic load.

[0152] For non-proportional damping, some improvements need to be made on the basis of the method in Exa...

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Abstract

The invention discloses a dynamic calibration method for a high-frequency base force balance, which comprises the following steps: whitening a measurement signal x(t) to obtain a whitened signal z(t); seeking an orthogonal matrix V such that z(t)= Vq(t), and then obtain the separation signal q(t); under the modal coordinates, identify the natural frequency and modal damping ratio of the separation signal; modify the separation signal according to the parameters obtained by identification; inversely deduce from the separation signal , to get the corrected aerodynamic load. The invention separates the coupling signal, and uses the curve fitting method to identify the natural frequency and modal damping ratio of the separated signal one by one for the independent components obtained by the separation, combined with the aerodynamic characteristics, and then corrects and eliminates the modal coupling system. The dynamic amplification effect of the method can finally obtain the real aerodynamic load spectral density matrix, which can maximize the reliability of parameter identification and corresponding HFFB dynamic signal calibration, and lay an important foundation for the subsequent accurate estimation of wind-induced response of high-rise building prototypes.

Description

technical field [0001] The invention belongs to the technical field of instrument calibration, and in particular relates to a dynamic calibration method of a high-frequency base force balance. Background technique [0002] The high-frequency base force balance (HFFB) technology is widely used in the wind resistance test research of super high-rise buildings due to its simple model making and short test period. HFFB belongs to the category of multi-component (usually five-component or six-component) balances. Multi-component balances will have problems of mutual interference or coupling between components to varying degrees. Usually, it is necessary to calibrate before leaving the factory to determine the simulation of each component and the corresponding sensor output. The transformation matrix of the signal finally achieves decoupling. Strictly speaking, this calibration technique is only suitable for static measurement. When the balance is installed on the measured model,...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06K9/00G01M9/06
CPCG01M9/06G06F2218/00
Inventor 张乐乐谢壮宁余先锋石碧青
Owner SOUTH CHINA UNIV OF TECH
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