TY - GEN
T1 - The Structural Reliability Analysis Method of Electronic System Based on the Dependent Failure Processes
AU - Wang, Yanfang
AU - Chen, Ying
AU - Li, Yingyi
N1 - Publisher Copyright:
© 2025 IEEE.
PY - 2025
Y1 - 2025
N2 - Structural failure is a critical failure mode in electronic systems. However, existing reliability analysis methods struggle to comprehensively evaluate the structural performance of such systems. This paper models the structural damage process with the influence of wear-out mechanisms and the structural shock process with the influence of overstress mechanisms. Furthermore, it defines the Dependent Competing Failure Process (DCFP) group to characterize the structural performance of electronic systems from two perspectives: structural durability and ultimate tolerance. The structural reliability of the system is then analyzed under three types of DCFP groups: joint effect type, unilateral dependency type, and bilateral dependency type. Building on this framework, the study further considers the phenomenon of multi-point concurrent structural degradation within electronic systems. Using the unmanned aircraft drive control circuit as a case study, the proposed method is implemented to demonstrate its effectiveness.
AB - Structural failure is a critical failure mode in electronic systems. However, existing reliability analysis methods struggle to comprehensively evaluate the structural performance of such systems. This paper models the structural damage process with the influence of wear-out mechanisms and the structural shock process with the influence of overstress mechanisms. Furthermore, it defines the Dependent Competing Failure Process (DCFP) group to characterize the structural performance of electronic systems from two perspectives: structural durability and ultimate tolerance. The structural reliability of the system is then analyzed under three types of DCFP groups: joint effect type, unilateral dependency type, and bilateral dependency type. Building on this framework, the study further considers the phenomenon of multi-point concurrent structural degradation within electronic systems. Using the unmanned aircraft drive control circuit as a case study, the proposed method is implemented to demonstrate its effectiveness.
KW - dependency
KW - electronic system
KW - modeling method
KW - structural reliability
UR - https://www.scopus.com/pages/publications/105036281668
U2 - 10.1109/ICSRS68021.2025.11422143
DO - 10.1109/ICSRS68021.2025.11422143
M3 - 会议稿件
AN - SCOPUS:105036281668
T3 - 2025 9th International Conference on System Reliability and Safety, ICSRS 2025
SP - 163
EP - 169
BT - 2025 9th International Conference on System Reliability and Safety, ICSRS 2025
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 9th International Conference on System Reliability and Safety, ICSRS 2025
Y2 - 26 November 2025 through 28 November 2025
ER -