System States Transition Safety Analysis Method Based on FSM and NuSMV

Author:

Ding Yuxin1,Li Weigang2,Zhong Deming1,Huang Hao2,Zhao Yukun1,Xu Zhi1

Affiliation:

1. Beihang University, BeiHang University XueYuan, BeiJing, China

2. Aviation Control System Institute, JiangSu, China

Funder

Ministry of Industry and Information Technology of China

Major State Basic Research Development Program of China

Civil Aviation Joint Funds Established by National Nature Science Foundation of China and Civil Aviation Administration of China

Publisher

ACM Press

Reference23 articles.

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Complex physical-model based dynamic system safety analysis of Aviation Piston Engine considering hybrid uncertainty of fault;Engineering Failure Analysis;2023-10

2. System verification via Model‐Checking: A case study of an autonomous multi‐differential drive robot;INCOSE International Symposium;2023-07

3. Synthesis of a Controller Algorithm for Safety-Critical Systems;IEEE Access;2022

4. Optimizing Hierarchical, Concurrent State Machines in Umple for Model Checking;2019 ACM/IEEE 22nd International Conference on Model Driven Engineering Languages and Systems Companion (MODELS-C);2019-09

5. An Airborne Software FMEA Application Method Based on ARP4761;Proceedings of the 2019 3rd International Conference on Management Engineering, Software Engineering and Service Sciences - ICMSS 2019;2019

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