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弹箭与制导学报 >

2019 , Vol. 39 >Issue 3: 53 - 57,68

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2019.03.013

导弹攻击过程的STAMP/STPA任务失效及仿真研究

  • 李俊 ,
  • 胡剑波 ,
  • 王应洋 ,
  • 邢晓波
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  • 空军工程大学装备管理与无人机工程学院,西安 710051

李俊(1991-),男,江苏盐城人,硕士研究生,研究方向:先进控制理论与应用、飞行器适航性管理与验证。

收稿日期: 2018-04-11

  网络出版日期: 2025-05-20

基金资助

国家重点基础研究发展计划(2014CB744900);国家社会科学基金(17GGL270)

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Missile Attack Process STAMP/STPA Mission Failure and Simulation Research

  • LI Jun ,
  • HU Jianbo ,
  • WANG Yingyang ,
  • XING Xiaobo
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  • Equipment Management and Unmanned Aerial Vehicle Engineering College, Air Force Engineering University, Xi'an 710051, China

Received date: 2018-04-11

  Online published: 2025-05-20

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摘要

在采用传统的安全分析方法进行安全性分析时,常常关注系统的组件可靠性,很难避免由于组件交互、软件设计缺陷等引起事故的发生。STAMP把安全问题看作是控制问题,认为事故是由于控制不足导致的。文中以导弹攻击过程为例,建立导弹攻击过程的STAMP模型,采用STPA方法识别了导致导弹攻击任务失效的不安全控制行为,同时进行关键原因分析,最后对其中部分不安全控制行为进行仿真分析,为减少导弹攻击任务失效和导弹设计提供了参考。

关键词： 安全性; STAMP; 导弹攻击过程; STPA; 任务失效; 不安全控制行为; 关键原因; 仿真分析

本文引用格式

李俊 , 胡剑波 , 王应洋 , 邢晓波 . 导弹攻击过程的STAMP/STPA任务失效及仿真研究[J]. 弹箭与制导学报, 2019 , 39(3) : 53 -57,68 . DOI: 10.15892/j.cnki.djzdxb.2019.03.013

Abstract

When using traditional safety analysis methods for safety analysis, it is often concerned about the reliability of the components of the system, it is difficult to avoid the occurrence of accidents due to component interactions, software design defects, etc. STAMP regards safety issues as control problems and considers accidents. It is due to lack of control. In this paper, the missile attack process is taken as an example to establish the STAMP model of the missile attack process. The STPA method is used to identify the unsafe control actions that lead to missile attack failure and analyze the key cause. Finally, some of the unsafe control actions are simulated and analyzed. It provides a reference for reducing missile mission failures and missile design.

Key words： safety; STAMP; missile attack process; STPA; mission failure; unsafe control behavior; key cause; simulation analysis

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参考文献

[1]
LEVESON N G．Engineering a safer world: systems thinking applied to safety[M]．London: The MIT Press，2011: 18-26．
[2]
RAO K D，GOPIKA V，RAO V V S S，et al．Dynamic fault tree analysis using monte carlo simulation in probabilistic safety assessment[J]．Reliability Engineering & System Safety，2009，94(4) : 872-883．
[3]
胡剑波，庄开宇．高级变结构控制理论及应用[M]．西安: 西北工业大学出版社，2008．
[4]
刘东，武杰，杨朋松．不确定非线性系统的自适应反推终端滑模控制[J]．空军工程大学学报 (自然科学版)，2012，13(5) : 14-19．
[5]
LI Qingchun，ZHANG Wensheng，HAN Gang，et al．Fuzzy sliding mode control guidance law with terminal impact angle and acceleration constraints[J]．Journal of Systems Engineering and Electronics，2016，27(3) : 664-679．
[6]
ISHIMATSU T，LEVESON N G，THOMAS J，et al．Modeling and hazard analysis using STPA[C]//MIT．Proceedings of the 4th IAASS Conference on Making Safety Matter．[S．l．]: IAASS，2010: 1-10．
[7]
LEVESON N，DAOUK M，DULAC N，et al．A systems theoretic approach to safety engineering[D]．Cambridge: Massachusetts Institute of Technology，2003．
[8]
胡剑波，李俊，郑磊．航空四站气体保障过程的 STAMP建模与 STPA 安全性分析[J]．航空工程进展，2017，8(4) : 408-415．
[9]
郑磊，胡剑波．基于 STAMP /STPA 的机轮刹车系统安全性分析[J]．航空学报，2017，38(1) : 241-251．
[10]
LIU Jintao，TANG Tao，ZHAO Lin，et al．Functional safety analysis of CTCS-3 train control system based on control relationship model[J]．Journal of the China Railway Society，2015，37(8) : 36-43．
[11]
CHIESI S S．STPA application for safety assessment of generic missile systems[C]//IEEE．Proceedings of 2016 Annual Reliability and Maintainability Symposium．[S．l．]: IEEE，2016: 1-7．
[12]
LARACY J R．A systems theoretic accident model applied to biodefense[J]．Defense and Security Analysis，2006，22(3) : 301-310．
[13]
KUMAR S R，RAO S，GHOSE D．Nonsingular terminal sliding mode guidance with impact angle constraints[J]．Journal of Guidance Control & Dynamics，2014，37 (4): 1114-1130．
[14]
杨锁昌，张宽桥，陈鹏．带攻击角度约束的自适应终端滑模导引律[J]．北京航空航天大学学报，2016，42(8): 1566-1574．
[15]
吴鹏, 杨明. 带终端攻击角度约束的变结构制导律. 固体火箭技术, 2008, 31 (2): 116– 120.
[16]
ZHOU HB, SONGS M, XU MY, et al. Design of terminal sliding-mode guidance law with attack angle constraints[C]// Proceedings of 2013 25th Chinese Controland Decision Conference. [S.1.]: IEEE, 2013: 556– 560.
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