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航空复杂装备测试目标设计方法

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为了保证航空装备的可靠性、安全性,提升系统的测试、维修与保障能力,对系统测试性提出了更高的需求.通过系统测试性问题分析,综合考虑系统功能重要度、失效率、故障风险影响、可测试性等要素,建立系统测试性目标函数模型;研究基于功能重要度分析、功能失效风险与失效率分析、故障树分析和可测试性技术在复杂系统测试性目标确定中的方法应用.通过航空辅助动力装置控制系统测试性目标选取表明,所提出的方法可以实现动力控制系统中的功能重要度与风险项分析,并且能够指导开展高风险项的测试性设计.
Test Object Design Method for Aviation Complex Equipment
In order to ensure the reliability and safety of aviation equipment and improve the testing,maintenance and support capa-bilities of the system,higher requirements were proposed for system testability.The testability objective function model of the system was established by analyzing the testability problem of the system,considering the system function importance,failure rate,failure risk effect,testability and other factors.The application of functional importance analysis,functional failure risk and failure rate analysis,fault tree analysis and testability technology in the determination of testability targets for complex systems was studied.Through the analysis and calculation of testability target selection in auxiliary power unit(APU)control system,it is show that the proposed method can realize the analysis of functional importance and risk items in the power control system,and can guide the testability design of high risk items.

testability objectimportance degreefailure mode and effects analysis(FMEA)fault tree

杨恒辉、常博博、黄新阳、林清

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西安航空计算技术研究所,西安 710065

测试性对象 重要度 故障模式影响分析(FMEA) 故障树

工信部民机专项航空科学基金

M-2017-D-28

2024

科学技术与工程
中国技术经济学会

科学技术与工程

CSTPCD北大核心
影响因子:0.338
ISSN:1671-1815
年,卷(期):2024.24(20)
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