The Missile Flight Control System Reliability Analysis Based on Hybrid fault Trees
被引:2
作者:
Yuan Jing
论文数: 0引用数: 0
h-index: 0
机构:
Xian Res Inst Hitech Hongqing Town, Xian 710025, Peoples R ChinaXian Res Inst Hitech Hongqing Town, Xian 710025, Peoples R China
Yuan Jing
[1
]
Long Yong
论文数: 0引用数: 0
h-index: 0
机构:
Xian Res Inst Hitech Hongqing Town, Xian 710025, Peoples R ChinaXian Res Inst Hitech Hongqing Town, Xian 710025, Peoples R China
Long Yong
[1
]
机构:
[1] Xian Res Inst Hitech Hongqing Town, Xian 710025, Peoples R China
来源:
2010 2ND INTERNATIONAL ASIA CONFERENCE ON INFORMATICS IN CONTROL, AUTOMATION AND ROBOTICS (CAR 2010), VOL 3
|
2010年
关键词:
Missile flight control system;
Reliability;
hybrid fault tree;
D O I:
10.1109/CAR.2010.5456653
中图分类号:
TP [自动化技术、计算机技术];
学科分类号:
0812 ;
摘要:
As Missile Flight Control System (MFCS) is a typical complex and high reliable system, its safety and reliability has been turn into an all-important problem. MFCS is frequently employed high level of redundancy for achieving high level of reliability. Dynamic redundancy employed in MFCS can realize complex fault and error diagnosis, recovery and reconfiguration. It is very difficult to analyze the reliability of MFCS by traditional Fault Tree Analysis (FTA) methods. This paper analyzes the weakness of FTA and induces a method of Hybrid FTA that combine dynamic fault tree. Accordingly, static FTA uses binary decision diagrams and dynamic FTA uses Markov Chains. At last, an example is proposed to prove academic analysis.