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A Fault Sample Simulation Approach for Virtual Testability Demonstration Test
  • ISSN号:1000-9361
  • 期刊名称:Chinese Journal of Aeronautics
  • 时间:2012.8
  • 页码:598-604
  • 分类:O211[理学—概率论与数理统计;理学—数学] TV698.11[水利工程—水利水电工程]
  • 作者机构:[1]Science and Technology on Integrated Logistics Support Laboratory,National University of Defense Technology,Changsha 410073, China, [2]College of Mechatronic Engineering and Automation,National University of Defense Technology, Changsha 410073, China
  • 相关基金:Acknowledgements The authors are grateful to the anonymous reviewers for their critical review and constructive comments on the manuscript. They also thank the managing editor for the work on the man- uscript, This study was co-supported by the National Natural Science Foundation of China (No. 51105369) and Shanghai Aerospace Science and Technology Foundation (No. SAST201313).
  • 相关项目:面向测试性虚拟验证的故障-测试-环境相关性建模方法
中文摘要:

Testability plays an important role in improving the readiness and decreasing the lifecycle cost of equipment. Testability demonstration and evaluation is of significance in measuring such testability indexes as fault detection rate(FDR) and fault isolation rate(FIR), which is useful to the producer in mastering the testability level and improving the testability design, and helpful to the consumer in making purchase decisions. Aiming at the problems with a small sample of testability demonstration test data(TDTD) such as low evaluation confidence and inaccurate result, a testability evaluation method is proposed based on the prior information of multiple sources and Bayes theory. Firstly, the types of prior information are analyzed. The maximum entropy method is applied to the prior information with the mean and interval estimate forms on the testability index to obtain the parameters of prior probability density function(PDF), and the empirical Bayesian method is used to get the parameters for the prior information with a success-fail form. Then, a parametrical data consistency check method is used to check the compatibility between all the sources of prior information and TDTD. For the prior information to pass the check, the prior credibility is calculated. A mixed prior distribution is formed based on the prior PDFs and the corresponding credibility. The Bayesian posterior distribution model is acquired with the mixed prior distribution and TDTD, based on which the point and interval estimates are calculated.Finally, examples of a flying control system are used to verify the proposed method. The results show that the proposed method is feasible and effective.

英文摘要:

Testability plays an important role in improving the readiness and decreasing the lifecycle cost of equipment. Testability demonstration and evaluation is of significance in measuring such testability indexes as fault detection rate(FDR) and fault isolation rate(FIR), which is useful to the producer in mastering the testability level and improving the testability design, and helpful to the consumer in making purchase decisions. Aiming at the problems with a small sample of testability demonstration test data(TDTD) such as low evaluation confidence and inaccurate result, a testability evaluation method is proposed based on the prior information of multiple sources and Bayes theory. Firstly, the types of prior information are analyzed. The maximum entropy method is applied to the prior information with the mean and interval estimate forms on the testability index to obtain the parameters of prior probability density function(PDF), and the empirical Bayesian method is used to get the parameters for the prior information with a success-fail form. Then, a parametrical data consistency check method is used to check the compatibility between all the sources of prior information and TDTD. For the prior information to pass the check, the prior credibility is calculated. A mixed prior distribution is formed based on the prior PDFs and the corresponding credibility. The Bayesian posterior distribution model is acquired with the mixed prior distribution and TDTD, based on which the point and interval estimates are calculated.Finally, examples of a flying control system are used to verify the proposed method. The results show that the proposed method is feasible and effective.

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期刊信息
  • 《中国航空学报:英文版》
  • 中国科技核心期刊
  • 主管单位:中国航空工业第一集团公司
  • 主办单位:中国航空学会
  • 主编:朱自强
  • 地址:北京学院路37号中国航空学报:英文版编辑部
  • 邮编:100083
  • 邮箱:caifei@buaa.edu.cn
  • 电话:010-82317058 82318016
  • 国际标准刊号:ISSN:1000-9361
  • 国内统一刊号:ISSN:11-1732/V
  • 邮发代号:
  • 获奖情况:
  • 国内外数据库收录:
  • 被引量:393