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Publishing Language: Chinese

A dynamic evaluation method for mission safety of missile equipment based on hierarchical safety control structure

Boqing YAO1, Jiayu CHEN1( ), Changchao GU2, Qinhua LU1, Xuhang WANG1, Hongjuan GE1
College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China
China Academy of Launch Vehicle Technology, Beijing 100076, China
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Abstract

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. However, missile equipment is a typical man-machine-environment coupling complex system. Traditional safety analysis and evaluation methods cannot meet the requirements of its dynamic change and accurate quantification. Therefore, this paper proposes a safety dynamic evaluation method for missile equipment based on hierarchical safety control structure model to realize accurate safety evaluation under the long-term storage mission situation. First, according to the mission profile characteristics of missile equipment, a multi-view architecture model of process, mission, function, information and organization is constructed to achieve the accurate description of mission process and resource. Then, a hierarchical safety control structure model is proposed to determine the accident causal factors and accident chain of the targeted mission. Meanwhile, based on the mission characteristics of missile equipment, a human performance evaluation system is constructed for long-term storage in a complex and changeable environment, achieving accurate evaluation of human error rate under the man-machine-environment coupling condition. Moreover, a safety dynamic feedback evaluation method integrating STAMP and CREAM is proposed to obtain the accident rate of the missile mission through simulation. Finally, a case study of the missile test mission is performed. The proposed method specifies 6 typical accident chains of 3 categories of coordination, control and feedback in the man-machine-environment coupling scenario. Meanwhile, the accuracy of the accident rate is improved by 70. 08%, which verifies the effectiveness and superiority of the proposed method.

CLC number: V37; TJ76 Document code: A

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Acta Aeronautica et Astronautica Sinica
Article number: 228858

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Cite this article:
YAO B, CHEN J, GU C, et al. A dynamic evaluation method for mission safety of missile equipment based on hierarchical safety control structure. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 228858. https://doi.org/10.7527/S1000-6893.2023.28858

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Received: 11 April 2023
Revised: 08 June 2023
Accepted: 20 July 2023
Published: 31 July 2023
© 2024 The Journal of Acta Aeronautica et Astronautica Sinica