Model-based fault identification and modeling method for space propulsion System

被引:0
作者
Qi, Yaqun [1 ,2 ]
Jin, Ping [1 ,3 ]
Peng, Qibo [4 ]
Zhang, Hailian [2 ]
Cai, Guobiao [1 ,3 ]
机构
[1] School of Astronautics, Beihang University, Beijing
[2] China Manned Space Agency, Beijing
[3] National Key Laboratory of Aerospace Liquid Propulsion, Beijing
[4] China Astronaut Research and Training Center-, Beijing
来源
Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics | 2024年 / 46卷 / 12期
关键词
fault identification; fault modeling; model-based System engineering (MBSE); propulsion System; reliability analysis; safety analysis;
D O I
10.12305/j.issn.1001-506X.2024.12.15
中图分类号
学科分类号
摘要
To comprehensively identify the fault modes of complex Systems, a method based on model-based Systems engineering (MBSE) principles is proposed to synchronously identify potential faults from the three dimensions of functionality, Performance, and structure in the forward design and modeling process of complex Systems. Utilizing the extension mechanism of the System modeling language (SysML), the corresponding fault base models are developed for modeling fault modes and associated elements. Taking the propulsion System of the new generation manned spacecraft as an example, the process of fault identification and modeling is described in detail. The proposed method, rooted in the standardized, normalized, and multi-dimensional fault modeling process of MBSE, enables thorough identification and modeling of potential faults in complex Systems, avoiding the problem of previous methods that heavily relied on individual expertise and judgment, which provides a foundation for reliability and safety analysis in model-based complex System domains. © 2024 Chinese Institute of Electronics. All rights reserved.
引用
收藏
页码:4062 / 4073
页数:11
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