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A Verification Platform for Aerospace Components Application Based on Equivalent Stimulus Test Module

A technology for testing modules and verification platforms, applied in electrical testing/monitoring, testing/monitoring control systems, instruments, etc., can solve problems such as waste of resources, development progress, poor compatibility and versatility, and difficulty in upgrading and improving, so as to improve coverage. and reliability, platformization, and full flexibility

Active Publication Date: 2021-02-09
CHINA ACADEMY OF SPACE TECHNOLOGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The design of most aerospace component application verification devices is related to specific verification components. Once developed, it is difficult to upgrade and improve. Therefore, the compatibility and versatility between different devices is poor, resulting in waste of resources and delays in research and development progress.

Method used

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  • A Verification Platform for Aerospace Components Application Based on Equivalent Stimulus Test Module
  • A Verification Platform for Aerospace Components Application Based on Equivalent Stimulus Test Module
  • A Verification Platform for Aerospace Components Application Based on Equivalent Stimulus Test Module

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Embodiment Construction

[0028] Based on the traditional application verification scheme, the present invention combines the characteristics of the aerospace single machine, builds an application verification platform based on the on-board bus protocol, and improves the coverage and reliability of the application verification conclusion. The platform has sufficient flexibility, openness and scalability, and can Through hardware configuration, it meets the needs of application verification of various aerospace components. The present invention is an aerospace component application verification platform based on an equivalent excitation test module, including a control computer, an equivalent excitation test module, and a verification object, and the equivalent excitation test module includes a verification control board, a verification bottom board, and a circuit established by a verification sub-board The environmental equivalent simulates the on-board circuit environment, and generates corresponding e...

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PUM

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Abstract

The invention provides a space navigation component and part application verification platform based on an equivalent excitation testing module. The space navigation component and part application verification platform comprises a control computer, an equivalent excitation testing module and a verification target. The equivalent excitation testing module equivalently simulates an on-board circuitenvironment under the control of the control computer and generates different equivalent excitation signals which are sent to the verification target; the verification target is placed in the equivalently-simulated on-board system circuit environment; the control computer controls the equivalent excitation testing module to equivalently simulate the on-board circuit environment according to external instructions to generate different equivalent excitation signals which are sent to the verification target, and monitors and reads verification target data in real time and sends the data to the outside for storage and analysis.

Description

technical field [0001] The invention relates to an aerospace component application verification platform based on an equivalent excitation test module, and belongs to the technical field of aerospace component application verification. Background technique [0002] Aerospace engineering is a high-tech, high-risk, and high-cost special project. Since its success or failure is related to national security and the development of the aerospace industry, reliability is of utmost importance. It is necessary to pass the implementation of aerospace component application verification to promote the development of aerospace engineering components. The standard selection of aerospace components promotes the improvement of application reliability of aerospace components, thereby improving the reliability of aerospace system engineering as a whole. [0003] In the investigation of selecting the application verification system architecture of aerospace components, it is found that the Eur...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B23/02
CPCG05B23/0213G05B2219/24065
Inventor 张洪伟肖爱斌张雷浩王喆刘辉丁丽娜刘艳秋王文炎
Owner CHINA ACADEMY OF SPACE TECHNOLOGY
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