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Complete machine test monitoring device and method based on multi-source data fusion

A monitoring device and multi-source data technology, applied in the direction of measuring device, video data retrieval, video data indexing, etc., can solve the problems of multi-type data fusion and display in the test site, so as to improve the test monitoring ability and improve the whole state monitoring The effect of the system

Pending Publication Date: 2021-01-15
CHINA AIRPLANT STRENGTH RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At this stage, the machine strength test monitoring can only realize discrete test data monitoring, and does not yet have multi-type data fusion display on the test site

Method used

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  • Complete machine test monitoring device and method based on multi-source data fusion
  • Complete machine test monitoring device and method based on multi-source data fusion
  • Complete machine test monitoring device and method based on multi-source data fusion

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Embodiment Construction

[0033] The technical solutions of the present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0034] In order to obtain more comprehensive aircraft strength test status information, the embodiment of the present invention provides a whole machine test monitoring device and method based on multi-source data fusion, which is mainly realized through the following technical solutions:

[0035] The embodiment of the present invention provides a whole machine test monitoring device based on multi-source data fusion, such as figure 1 As shown, the monitoring device includes: a data acquisition unit, a data fusion unit, a data storage unit and a data display unit;

[0036] Wherein, the data collection unit is used to collect the structural strain information of the testing machine, the structural displacement and deformation information of the testing machine, and the video information of the testing environment in th...

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Abstract

The invention belongs to the technical field of airplane complete machine strength tests, and discloses a complete machine test monitoring device and method based on multi-source data fusion, and thedevice comprises a data acquisition unit, a data fusion unit, a data storage unit, and a data display unit. The data acquisition unit is used for acquiring structural strain information of a testing machine, structural displacement deformation information of the testing machine and video information of a testing environment in a complete machine test; the data fusion unit is used for fusing the structural strain information of the testing machine and the structural displacement deformation information of the testing machine into the video information of the testing environment to obtain fusedvideo information; the data storage unit is used for storing the fused video information; and the data display unit is used for displaying the fused video information in real time and providing technical support for realizing full-state monitoring of a test site.

Description

technical field [0001] The invention belongs to the technical field of aircraft strength test, and in particular relates to a monitoring device and method for a complete aircraft test based on multi-source data fusion. Background technique [0002] In the aircraft development industry chain, the strength test of the whole aircraft is an indispensable and important part, and it is the most comprehensive and realistic ground verification for the entire aircraft design. [0003] As the structure of the aircraft becomes more and more complex, the strength test of the whole machine is becoming more and more complicated at this stage. Therefore, the intuitive full-state monitoring of the test site can meet the needs of the whole machine strength test personnel for the three-dimensional control visualization of the test site and test safety. , which can effectively control the risk points of the test, which is of great significance to improving the quality of the test. At this sta...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60G01D21/02G06F16/71G06F16/73G06F16/74H04L29/08H04N5/262H04N5/268H04N7/18
CPCB64F5/60G01D21/02G06F16/71G06F16/73G06F16/74H04N5/262H04N5/268H04N7/18H04L67/06
Inventor 刘冰张建锋王孟孟牧彬郭琼杨凡王彬
Owner CHINA AIRPLANT STRENGTH RES INST