TY - GEN
T1 - Integrating design for performance and reliability
AU - Yunxia, Chen
AU - Rui, Kang
AU - Yufeng, Sun
PY - 2006
Y1 - 2006
N2 - The traditional reliability methodology considers the failure time of product is uncertain, and the probability is used to express the failure of product. The current reliability methodology considers the uncertainty is occurred in failure-process of product, and the failure-process analysis is concerned more than failure-time analysis. In this situation, we propose the technique of Integrating Design for Performance and Reliability (IDPaR), which is an effective method for reliability design and analysis of product or system. The concept and meaning of IDPaR. are described, and the definition and expression of performance-reliability are given. The theory of performance-reliability based on multistate structure function is introduced and presented. In the case study of a type of missile's flight control system, the main interrelated factors of the system failure are analyzed, the performance-reliability model is deduced and established, and the algorithm flow of performance-reliability is represented.
AB - The traditional reliability methodology considers the failure time of product is uncertain, and the probability is used to express the failure of product. The current reliability methodology considers the uncertainty is occurred in failure-process of product, and the failure-process analysis is concerned more than failure-time analysis. In this situation, we propose the technique of Integrating Design for Performance and Reliability (IDPaR), which is an effective method for reliability design and analysis of product or system. The concept and meaning of IDPaR. are described, and the definition and expression of performance-reliability are given. The theory of performance-reliability based on multistate structure function is introduced and presented. In the case study of a type of missile's flight control system, the main interrelated factors of the system failure are analyzed, the performance-reliability model is deduced and established, and the algorithm flow of performance-reliability is represented.
KW - Flight control system
KW - Integrating design
KW - Performance-reliability
KW - Reliability modeling
KW - Reliability simulation
UR - https://www.scopus.com/pages/publications/34250208059
U2 - 10.1109/RAMS.2006.1677398
DO - 10.1109/RAMS.2006.1677398
M3 - 会议稿件
AN - SCOPUS:34250208059
SN - 1424400074
SN - 9781424400072
T3 - Proceedings - Annual Reliability and Maintainability Symposium
SP - 343
EP - 348
BT - Annual Reliability and Maintainability Symposium, RAMS'06 - 2006 Proceedings
T2 - 2006 Annual Reliability and Maintainability Symposium, RAMS'06
Y2 - 23 January 2006 through 26 January 2006
ER -