Fusion of expert uncertain assessment in FMEA based on the negation of basic probability assignment and evidence distance
被引:13
作者:
Yuan, Yusong
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机构:
Chongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R ChinaChongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R China
Yuan, Yusong
[1
]
Tang, Yongchuan
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机构:
Chongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R China
Northwestern Polytech Univ, Sch Microelect, Xian 710072, Shaanxi, Peoples R ChinaChongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R China
Tang, Yongchuan
[1
,2
]
机构:
[1] Chongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R China
[2] Northwestern Polytech Univ, Sch Microelect, Xian 710072, Shaanxi, Peoples R China
Failure mode and effects analysis (FMEA) has been widely used for potential risk modeling and management. Expert evaluation is used to model the risk priority number to determine the risk level of different failure modes. Dempster-Shafer (D-S) evidence theory is an effective method for uncertain information modeling and has been adopted to address the uncertainty in FMEA. How to deal with conflicting evidence from different experts is an open issue. At the same time, different professional backgrounds of experts may lead to different weights in modeling the evaluation. How to model the relative weight of an expert is an important problem. We propose an improved risk analysis method based on triangular fuzzy numbers, the negation of basic probability assignment (BPA) and the evidence distance in the frame of D-S evidence theory. First, we summarize and organize the expert's risk analysis results. Then, we model the expert's assessments based on the triangular fuzzy numbers as BPAs and calculate the negation of BPAs. Third, we model the weight of expert based on the evidence distance in the evidence theory. Finally, the Murphy's combination rule is used to fuse the risk assessment results of different experts and calculate the new risk priority number (RPN). At the end of this paper, we apply the proposed method to analyze seventeen failure modes of aircraft turbine blades. The experimental results verify the rationality and effectiveness of this method.
机构:
Chongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R ChinaChongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R China
Chen, Yong
Tang, Yongchuan
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机构:
Chongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R ChinaChongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R China
Tang, Yongchuan
Lei, Yan
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机构:
Chongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R ChinaChongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R China
机构:
Chongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R ChinaChongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R China
Chen, Yong
Tang, Yongchuan
论文数: 0引用数: 0
h-index: 0
机构:
Chongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R ChinaChongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R China
Tang, Yongchuan
Lei, Yan
论文数: 0引用数: 0
h-index: 0
机构:
Chongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R ChinaChongqing Univ, Sch Big Data & Software Engn, Chongqing 401331, Peoples R China