Title of article
A novel approach of testability modeling and analysis for PHM systems based on failure evolution mechanism
Author/Authors
Tan، نويسنده , , Xiaodong and Qiu، نويسنده , , Jing and Liu، نويسنده , , Guanjun and Lv، نويسنده , , Kehong and Yang، نويسنده , , Shuming and Wang، نويسنده , , Chao، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2013
Pages
11
From page
766
To page
776
Abstract
Prognostics and health management (PHM) significantly improves system availability and reliability, and reduces the cost of system operations. Design for testability (DFT) developed concurrently with system design is an important way to improve PHM capability. Testability modeling and analysis are the foundation of DFT. This paper proposes a novel approach of testability modeling and analysis based on failure evolution mechanisms. At the component level, the fault progression-related information of each unit under test (UUT) in a system is obtained by means of failure modes, evolution mechanisms, effects and criticality analysis (FMEMECA), and then the failure-symptom dependency can be generated. At the system level, the dynamic attributes of UUTs are assigned by using the bond graph methodology, and then the symptom-test dependency can be obtained by means of the functional flow method. Based on the failure-symptom and symptom-test dependencies, testability analysis for PHM systems can be realized. A shunt motor is used to verify the application of the approach proposed in this paper. Experimental results show that this approach is able to be applied to testability modeling and analysis for PHM systems very well, and the analysis results can provide a guide for engineers to design for testability in order to improve PHM performance.
Keywords
Design for Testability , Failure evolution mechanism , Symptom-test dependency , Failure-symptom dependency , Prognostics and health management , Unit under test , Testability modeling and analysis
Journal title
Chinese Journal of Aeronautics
Serial Year
2013
Journal title
Chinese Journal of Aeronautics
Record number
2265301
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