Volume 33 Issue 03
Mar.  2007
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Xu Ping, Kang Rui. Concept of testability determine test and relative method for FDR[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(03): 357-360. (in Chinese)
Citation: Xu Ping, Kang Rui. Concept of testability determine test and relative method for FDR[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(03): 357-360. (in Chinese)

Concept of testability determine test and relative method for FDR

  • Received Date: 08 May 2006
  • Publish Date: 31 Mar 2007
  • To solve absence problem of the method in determining the product-s testability level and find the difference between the practical testability situation and the requirements, the concepts of testability test and testability determine test was proposed. With the only consideration of fault detection rate (FDR), the method to establish fault character model (FCM) was given, which is based on the fault-function relation matrix and fault weightiness. Two-tuples FCM was illustrated and the flow to select sample based on two-tuples FCM in testability determine test was given. To simplify the workload and the complexity of the fault injection test, the equivalent relation between test samples were researched. The equivalent set and the equivalent injection sample (EIS) were defined. The relative method of result evaluation for FDR was researched. An example on a control system in some missile was illustrated, and the results show that the methods introduced are correct and feasible.

     

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  • [1] MIL-STD-2165A, Testability program for systems and equipments[S] [2] GJB2547-95,装备测试性大纲[S] GJB2547-95,Testability program for material [S] (in Chinese) [3] 徐萍. 测试性试验方法与试验平台研究 . 北京:北京航空航天大学工程系统工程系,2006 Xu Ping. The method and platform in testability test . Beijing:Department of System Engineering of Engineering Technology, Beijing University of Aeronautics and Astroanutics, 2006(in Chinese) [4] 石君友,康锐. 基于通用充分性准则的测试性试验方案研究[J]. 航空学报,2005,26(6):691-695 Shi Junyou, Kang Rui. Study on plan of testability demonstration based on the general adequacy criterion[J]. ACTA Aeronautica Et Astronautica Sinica, 2005,26(6):691-695(in Chinese)
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