基于模型的推进系统故障识别及建模方法

doi:10.12305/j.issn.1001-506X.2024.12.15

系统工程与电子技术 ›› 2024, Vol. 46 ›› Issue (12): 4062-4073.doi: 10.12305/j.issn.1001-506X.2024.12.15

• 系统工程 • 上一篇

基于模型的推进系统故障识别及建模方法

戚亚群¹^,², 金平¹^,³^,*, 彭祺擘⁴, 张海联², 蔡国飙¹^,³

1. 北京航空航天大学宇航学院, 北京 102206
2. 中国载人航天工程办公室, 北京 100071
3. 航天液体动力全国重点实验室, 北京 102206
4. 中国航天员科研训练中心, 北京 100094

收稿日期:2024-01-22 出版日期:2024-11-25 发布日期:2024-12-30
通讯作者: 金平
作者简介:戚亚群(1993—), 女, 博士, 主要研究方向为液体火箭发动机可靠性、基于模型的系统工程
金平(1979—), 女, 副教授, 博士, 主要研究方向为液体火箭发动机总体设计、可重复使用火箭发动机寿命与可靠性
彭祺擘(1982—), 男，研究员，博士，主要研究方向为载人月球探测任务分析与设计、基于模型的系
张海联(1974—), 男，研究员，博士，主要研究方向为载人航天总体技术、基于模型的系统工程、固体力学
蔡国飙(1967—), 男, 教授, 博士, 主要研究方向为液体火箭发动机多学科优化与重复使用技术、真空羽流效应及防护技术、固液混合动力火箭技术
基金资助:
载人航天工程科技创新

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

Yaqun QI¹^,², Ping JIN¹^,³^,*, Qibo PENG⁴, Hailian ZHANG², Guobiao CAI¹^,³

1. School of Astronautics, Beihang University, Beijing 102206, China
2. China Manned Space Agency, Beijing 100071, China
3. National Key Laboratory of Aerospace Liquid Propulsion, Beijing 102206, China
4. China Astronaut Research and Training Center, Beijing 100094, China

Received:2024-01-22 Online:2024-11-25 Published:2024-12-30
Contact: Ping JIN

摘要/Abstract

摘要：

为全面识别复杂系统故障模式, 根据基于模型的系统工程(model-based systems engineering, MBSE) 的思想, 提出在复杂系统正向化设计与建模过程中, 同步从功能、性能、结构3个维度识别潜在故障的方法; 并依据系统建模语言(system modeling language, SysML)的扩展机制建立相对应的故障基础模型, 用于对故障模式及相关要素进行建模。以新一代载人飞船推进系统为例, 详述故障识别与建模流程。所提方法基于MBSE规范化、标准化、全维度的建模过程, 用于实现对复杂系统潜在故障的全面识别及建模, 避免以往依赖个人经验和能力、难以全面识别故障的问题, 为基于模型的复杂系统可靠性分析、安全性分析提供基础。

关键词: 基于模型的系统工程, 故障识别, 故障建模, 可靠性分析, 安全性分析, 推进系统

Abstract:

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.

Key words: model-based system engineering (MBSE), fault identification, fault modeling, reliability analysis, safety analysis, propulsion system

中图分类号:

V434.1

戚亚群, 金平, 彭祺擘, 张海联, 蔡国飙. 基于模型的推进系统故障识别及建模方法[J]. 系统工程与电子技术, 2024, 46(12): 4062-4073.

Yaqun QI, Ping JIN, Qibo PENG, Hailian ZHANG, Guobiao CAI. Model-based fault identification and modeling method for space propulsion system[J]. Systems Engineering and Electronics, 2024, 46(12): 4062-4073.

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基础模型层	扩展包		库
基础模型层	类	关系	类	关系
核心层	状态	违反、相关	任意状态	因果
通用层	失效模式、功能故障、结构失效、性能偏差	-	功能故障、结构失效、性能偏差、后果、原因	导致、偏差传递
方法层	FMEA条目、树、事件、门、转向符号	-	FMEA条目、故障树元素、故障树、事件、门	RPN、门约束

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基于模型的推进系统故障识别及建模方法

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

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