Application of formal methods to fault-tolerant flight control systems

被引:0
|
作者
Xue, L [1 ]
Chen, ZJ [1 ]
机构
[1] Beijing Univ Aeronaut & Astronaut, Beijing 100083, Peoples R China
来源
FIFTH INTERNATIONAL SYMPOSIUM ON INSTRUMENTATION AND CONTROL TECHNOLOGY | 2003年 / 5253卷
关键词
formal method; fault-tolerant flight control system; extended duration calculus; hybrid system;
D O I
10.1117/12.522119
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper is concerned with the application of formal methods to fault-tolerant flight control systems. The analysis, design and verification of a fault-tolerant flight control system have been performed in the theoretical framework of the extended duration calculus, which is a popular formal method to handle highly complex real-time hybrid systems. The theoretical results in this paper show that the proposed approach can ensure the flight control system to work properly even after a fault happens.
引用
收藏
页码:774 / 778
页数:5
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