A linearized force correction iterative mixed test method for nonlinear models

A nonlinear model and hybrid experiment technology, applied in the field of iterative hybrid experiment, can solve the problems of low computational efficiency of numerical substructure, difficulty in real-time experiment, slow iterative convergence speed, etc., so as to improve the iterative convergence speed and avoid real-time performance. problem, the effect of improving iterative convergence efficiency

Active Publication Date: 2022-04-05
HEILONGJIANG UNIVERSITY OF SCIENCE AND TECHNOLOGY
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Problems solved by technology

[0005] In order to solve the low calculation efficiency of the numerical substructure in the current real-time hybrid test, it is difficult to achieve real-time performance of the test. At the same time, the traditional time course level iterative hybrid test method has a round difference between the specimen reaction force and the obtained equation when the motion equation is solved, resulting in iterative To solve the problem of slow convergence speed, the present invention proposes a nonlinear model linearization force correction iterative mixed test method, the specific scheme is as follows:

Method used

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  • A linearized force correction iterative mixed test method for nonlinear models
  • A linearized force correction iterative mixed test method for nonlinear models
  • A linearized force correction iterative mixed test method for nonlinear models

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specific Embodiment approach 1

[0044] Embodiment 1: Divide the overall structure into a numerical substructure and an experimental substructure, and establish a numerical model of the numerical substructure and a linear numerical model of the experimental substructure respectively;

[0045] Input the initial value of structural response and external excitation, and perform full-time pure numerical calculation on the overall structure to obtain the full-time displacement and velocity response of the test substructure;

[0046] Perform full-time servo loading on the test substructure to obtain the full-time reaction force response of the test substructure under the corresponding displacement and velocity response;

[0047] Enter the next round, and gradually integrate to solve the displacement and velocity response of the test substructure in this round. The required motion equation is:

[0048]

[0049] In the formula: M N 、C N 、K N —mass matrix, damping matrix, stiffness matrix of the numerical subst...

specific Embodiment approach 2

[0068] Specific implementation mode two: the present invention is applied to other research objects with similar basic principles; taking the iterative hybrid test of the high-speed train anti-snake shock absorber as an example, the basic principle of applying the present invention to carry out the nonlinear model linearization force correction iterative hybrid test :

[0069] When a high-speed train is running, it will produce lateral motion along the train, which is called snake vibration. Snaking vibration will lead to unstable running of the train, which is the main factor for the speed of the train. By installing anti-snaking shock absorbers, snaking motion can be effectively suppressed. Therefore, it is of great significance to carry out tests on the anti-snaking damper and study the effect of the anti-snaking damper during the operation of the train to improve the smooth running of the train and further increase the running speed of the train.

[0070] There are two c...

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Abstract

The invention relates to a nonlinear model linearization force correction iterative mixed test method, in particular to an iterative mixed test method with repeatability in application and test loading, and belongs to the application field of structural mixed test technology. The purpose is to solve the problem of slow iterative convergence due to the round difference between the reaction force of the specimen and the equation to be obtained when the equation of motion is solved in the traditional time course level iterative hybrid test method. The invention divides the overall structure into a test substructure and a numerical substructure, and simultaneously establishes a linear numerical model of the test substructure according to prior knowledge. The full-time response of the test substructure is obtained by numerical calculation of the overall structure, the full-time reaction force is obtained by full-time servo loading of the test substructure, and the displacement and velocity responses of the test substructure of two adjacent iterations are used to bring in It is assumed that the linearized model performs force correction on the reaction force, and the correction force is brought into the motion equation to participate in the numerical calculation, so as to improve the solution accuracy of the motion equation, thereby increasing the iterative convergence speed.

Description

technical field [0001] An iterative hybrid test method based on nonlinear model linearization force correction, which relates to a repeatable iterative hybrid test method applied to the test loading part, specifically involving fields including but not limited to civil engineering, transportation, bridges, Aerospace field, mechanical field, etc. For example, the method can be used for force-corrected iterative hybrid tests of high-speed train shock absorbers, force-corrected iterative hybrid tests based on concrete structures equipped with various dampers, and so on. Background technique [0002] The hybrid test method is a new type of seismic test method that combines physical loading of real specimens and computer numerical simulation. By loading real specimens, more accurate test results can be obtained, and computer numerical simulation can greatly reduce test costs. , to improve the applicability of the test, and to carry out real-time calculation by establishing data ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/15G06F30/20G06F119/14
CPCG06F30/15G06F30/20G06F2119/14
Inventor 王涛郑欢王贞孟丽岩许国山杨格
Owner HEILONGJIANG UNIVERSITY OF SCIENCE AND TECHNOLOGY
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