A safety dynamic evaluation method for missile mission based on multi-layered safety control structure model

被引:3
|
作者
Chen, Jiayu. [1 ]
Yao, Boqing [1 ]
Lu, Qinhua [1 ]
Wang, Xuhang [1 ]
Yu, Pingchao [1 ]
Ge, Hongjuan [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Civil Aviat, Nanjing 210016, Jiangsu, Peoples R China
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
Long-term storage; Man-machine-environment coupling; Dynamic evaluation; Accurate quantification; THEORETIC ACCIDENT MODEL; SIMULATION;
D O I
10.1016/j.ress.2023.109678
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The multi -mission environment and complex working conditions of long-term storage put forward strict requirements on the effective risk suppression and accurate safety evaluation of missile equipment. This paper proposes a safety dynamic evaluation method based on a multi -layered safety control structure model to realize accurate safety evaluation for missile missions. Firstly, according to the missile mission profile characteristics, a multi -view architecture is constructed to achieve the accurate description of mission process as well as their relationships and interactions. Secondly, a multi -layered safety control structure model is proposed to determine the accident causal factors and accident chain of the targeted mission. Meanwhile, oriented to the long-term storage complex and volatile environment, a human performance and risk evaluation system is built to realize the effective evaluation of human factor error rate under the man -machine -environment coupling condition. Then, a safety dynamic feedback evaluation method integrating STAMP and CREAM is proposed to obtain the accident rates of the missile mission. Finally, a case study of the missile test mission is carried out, and 6 typical accident scenarios are studied. The results show that the overall accident rate accuracy is improved by 70.08%, which verifies the effectiveness and superiority of the proposed method.
引用
收藏
页数:14
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