DocumentCode
2682467
Title
An approach for improvement of avionics reliability assessment based on copula theory
Author
Huang, Mingsheng ; Wang, Qihua ; Li, Yonghong ; Ao, Liang
Author_Institution
Quality Eng. Technol. Center, China Aero-Polytechnology Establ., Beijing, China
fYear
2011
fDate
12-15 June 2011
Firstpage
179
Lastpage
183
Abstract
This paper seeks to address the drawbacks of the traditional reliability assessment model of avionics products based on failure dependent supposition and the classical reliability assessment method, which is based on copula theory when taking into account the difficulty of calculating and the accuracy of the model. An improved reliability assessment model based on copula theory is proposed to prioritize reliability assessment algorithm when concerned with the situation of correlative failures. In this paper, Cumbel-Hougaard copulas is used to prioritize the model when the failure time variables of avionics products were as the law of Weibull or Exponential distribution, the advantage of this method is also described in this paper. Finally, a case study is presented in this paper. It´s obviously that the new reliability assessment approach can resolves the limitations of traditional method and increase the efficiency of the algorithm which based on copula theory. So the new method can increase the precision of reliability analysis and provide more effective data for verification of reliability indicators and design optimization.
Keywords
Weibull distribution; avionics; reliability; Cumbel-Hougaard copula theory; Weibull distribution; avionics reliability assessment; copula theory; design optimization; exponential distribution; Aerospace electronics; Correlation; Distribution functions; Joints; Reliability engineering; Reliability theory; copula theory; failure dependent; reliability assessment;
fLanguage
English
Publisher
ieee
Conference_Titel
Reliability, Maintainability and Safety (ICRMS), 2011 9th International Conference on
Conference_Location
Guiyang
Print_ISBN
978-1-61284-667-5
Type
conf
DOI
10.1109/ICRMS.2011.5979258
Filename
5979258
Link To Document