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航天器数字化综合测试状态管理系统设计

张威 张强 胡骏 潘顺良 李鸿飞 杨枫

航天器工程2017,Vol.26Issue(4):109-115,7.
航天器工程2017,Vol.26Issue(4):109-115,7.DOI:10.3969/j.issn.1673-8748.2017.04.017

航天器数字化综合测试状态管理系统设计

Digital System Design for Spacecraft Integration Test State Management

张威 1张强 1胡骏 1潘顺良 1李鸿飞 1杨枫1

作者信息

  • 1. 中国空间技术研究院载人航天总体部,北京100094
  • 折叠

摘要

Abstract

Papyraceous forms are used for spacecraft integration test state management,but this method leads to the state management data jumbled,approval procedures complicated,the state management data enquiry difficult,and the management efficiency is low.A service-and-proce dure-orienteddigital method is proposed based on the research of the existing problems,and the digital system for integration test state management is developed with using this method.In this system,the function is regarded as service,the approval process is regarded as procedure.The system makes the state management and data archiving standard.And kings of state management information are saved as institution data,which can be read,used,inquired and analyzed easily.The system's application in a certain manned spaceship proves that the management efficiency is greatly increased,and the system provides technical basis for remote test in the future.

关键词

航天器测试/测试状态管理/数字化系统

Key words

spacecraft test/test state management/digital system

分类

航空航天

引用本文复制引用

张威,张强,胡骏,潘顺良,李鸿飞,杨枫..航天器数字化综合测试状态管理系统设计[J].航天器工程,2017,26(4):109-115,7.

基金项目

国家重大科技专项工程 ()

航天器工程

OA北大核心CSCDCSTPCD

1673-8748

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