固体力学与飞行器总体设计

面向测试性虚拟验证的功能-故障-行为-测试-环境一体化模型

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  • 国防科学技术大学 机电工程与自动化学院 装备综合保障技术重点实验室, 湖南 长沙 410073
张勇 男,博士研究生.主要研究方向:测试性设计、分析与评估. Tel: 0731-84573397 E-mail: zhangy21cn@126.com
邱静 男,博士,教授,博士生导师.主要研究方向:测试性设计、分析与评估,装备综合保障等. Tel: 0731-84573307 E-mail: qiujing@nudt.edu.cn

收稿日期: 2011-04-29

  修回日期: 2011-06-15

  网络出版日期: 2012-02-24

基金资助

国家自然科学基金(51105369)

Integrated Function-Fault-Behavior-Test-Environment Model for Virtual Testability Verification

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  • Laboratory of Science and Technology on Integrated Logistics Support, College of Mechatronic Engineering and Automation, National University of Defense Technology, Changsha 410073, China

Received date: 2011-04-29

  Revised date: 2011-06-15

  Online published: 2012-02-24

摘要

由于测试性预计和测试性试验验证客观存在的困难及问题,测试性虚拟验证将在测试性工程领域发挥重要作用.根据测试性虚拟验证对模型的需求,针对传统测试性模型存在的定量特征少、导致测试性评估结果不准确等问题,提出一种功能-故障-行为-测试-环境一体化模型.首先,分析并指出该一体化模型由功能、故障、行为、测试、环境5大类要素构成.然后,在数学上对该一体化模型及其子模型进行定义和描述,分析并建立各子模型之间的关联关系.最后以某导弹及其测试系统为案例进行实验和应用研究.结果表明,在建模信息量充足的情况下,基于该一体化模型得到的测试性虚拟试验验证与评估结果较准确,能较好地支持装备测试性摸底、鉴定与验收等.

本文引用格式

张勇, 邱静, 刘冠军, 杨鹏 . 面向测试性虚拟验证的功能-故障-行为-测试-环境一体化模型[J]. 航空学报, 2012 , 33(2) : 273 -286 . DOI: CNKI:11-1929/V.20110831.1320.004

Abstract

Virtual testability verification tests play an important role in testability engineering owing to the existence of many difficulties and problems involved in testability prediction and physical testability verification tests. Traditional testability models merely describe the qualitative relationship between faults and tests, while the quantitative characteristics of faults and tests are ill-considered. This leads to large modeling errors which result in inaccurate testability analysis and evaluation results. According to the requirements of the virtual testability verification test, an integrated function-fault-behavior-test-en- vironment model (FFBTEM) is proposed. First, the constituents of the FFBTEM are analyzed and discussed. Then, the mathematical definition and description of the FFBTEM and its submodels are provided. The relationships among the submod- els are established and analyzed. Finally, the FFBTEM is applied to a missile and its test system. The application example indicates that this model is more accurate with the premise of sufficient modeling information, and that it can be applied to testability analysis, virtual experiment and evaluation.
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