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基于STPA的多电飞机大功率机电驱动控制系统安全性分析

张建科 葛红娟 罗宇洲 潘旷明 王煜杰 刘宇轩

测控技术2025,Vol.44Issue(10):29-36,8.
测控技术2025,Vol.44Issue(10):29-36,8.DOI:10.19708/j.ckjs.2025.09.248

基于STPA的多电飞机大功率机电驱动控制系统安全性分析

Safety Analysis of STPA-Based High-Power Electromechanical Drive Control System for More Electric Aircraft

张建科 1葛红娟 1罗宇洲 1潘旷明 1王煜杰 1刘宇轩1

作者信息

  • 1. 南京航空航天大学民航学院,江苏南京 211106
  • 折叠

摘要

Abstract

The common motor starter controller(CMSC)is an important equipment in the electromechanical drive control system of more electric aircraft,and improving its safety is of great significance for ensuring the continuous airworthiness of the aircraft.Taking the electric pump mode of the CMSC as the research object,an analysis of working principles and module division are conducted,formal modeling is carried out using UP-PA AL software,and system-theoretic process analysis(STPA)is implemented.The unsafe control behaviors and potential hazards causes between subsystems are identified,and based on model liveness verification and fault injection experiments,correction of causal scenarios is performed to ultimately construct a relatively compre-hensive safety control constraint list.Experimental results demonstrate that the proposed method facilitates the safety analysis of the CMSC,and formal modeling is used to help to reduce the interference of subjective human factors.The model exhibits high operational efficiency,while causal scenario analysis results indicate that the established safety control constraint list is accurate and can effectively cover failure scenarios.

关键词

通用电机起动控制器/系统理论过程分析/不安全控制行为/UPPAAL/安全控制约束清单

Key words

CMSC/STPA/unsafe control behavior/UPPAAL/safety control constraint list

分类

航空航天

引用本文复制引用

张建科,葛红娟,罗宇洲,潘旷明,王煜杰,刘宇轩..基于STPA的多电飞机大功率机电驱动控制系统安全性分析[J].测控技术,2025,44(10):29-36,8.

基金项目

国家自然科学基金民航联合基金(U2233205,U2133203) (U2233205,U2133203)

测控技术

1000-8829

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