Multi-degree of freedom micro-vibrating environment simulating method

An environmental simulation and micro-vibration technology, applied in vibration testing, measuring devices, testing of machine/structural components, etc., can solve the problems of time-consuming, complex versatility, single experimental object, etc., achieving less time-consuming and strong versatility , the effect of improving efficiency

Active Publication Date: 2018-01-05
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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Problems solved by technology

[0003] However, regardless of the method of installing the disturbance source or the installation of the exciter, a complex test system needs to be built during the test; and for different test objects, the types and models of the disturbance source and the exciter used are different
Therefore, these two methods generally have the problems of time-consuming, complex and poor versatility
However, the method of simulating the micro-vibration envir

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[0025] A multi-degree-of-freedom micro-vibration environment simulation method of the present invention will be further described below.

[0026] figure 1 Shown is a flow chart of the multi-degree-of-freedom micro-vibration environment simulation method of the present invention. This method is mainly realized through three steps.

[0027] (1) Foretell the multi-degree-of-freedom micro-vibration environment;

[0028] The main purpose of predicting the micro-vibration environment is to obtain the micro-vibration environment at the installation interface of the payload, that is, to obtain the required simulated micro-vibration time-domain acceleration curve. Predicting the micro-vibration environment mainly adopts the method of modeling and simulating to predict the micro-vibration environment.

[0029] The step of modeling and simulating to predict the micro-vibration environment further includes establishing a geometric model of the entire spacecraft, including a structural ...

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Abstract

The invention provides a multi-degree of freedom micro-vibrating environment simulating method. The method includes the following steps: forecasting micro-vibrating environment conditions; identifyinga multiple-input-multiple-output system transfer function matrix; and conducting multi-degree of freedom micro-vibrating signal simulation control. The method herein conducts closed-loop control on the multiple-input-multiple-output system based on a multi-degree of freedom reference signal, the transfer function of the system and a multi-degree of freedom response signal that are configured, drives a micro-vibrating excitation system to move, and simulates the multi-degree of freedom micro-vibrating environment. According to the invention, the method herein has excellent universality and high efficiency, and better addresses the technical problems of micro-vibrating tests.

Description

technical field [0001] The invention belongs to the field of spacecraft mechanics environment test, and in particular relates to a multi-degree-of-freedom micro-vibration environment simulation method. Background technique [0002] At present, the simulation of micro-vibration environment mainly adopts the method of installing disturbing source equipment, installing vibration exciter equipment and using excitation system. The method of installing the disturbing source equipment is to generate a real micro-vibration environment by making the disturbing source equipment work normally; the method of installing the vibrator is to simulate the micro-vibration environment by using the exciter to generate an excitation signal similar to the real disturbance source; In a systematic approach, a micro-vibration excitation system is used to generate a micro-vibration signal to simulate a micro-vibration environment. For example, the micro-vibration environment simulation system based ...

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Application Information

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IPC IPC(8): G01M7/02
Inventor 冯咬齐赵越阳何玲邱汉平樊世超李栋武耀
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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