Response Performance Based Reliability Analysis of Aircraft Fault-tolerant Control system

被引：0
|
作者：
Wang, Jun [1 ]
Wang, Shaoping [1 ,2 ]
Cui, Xiaoyu [1 ]
Wang, Xingjian [1 ,2 ,3 ]
Shi, Cun [1 ]
机构：
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Beijing Adv Innovat Ctr Big Data Based Precis Med, Beijing 100191, Peoples R China
[3] Zhejiang Univ, State Key Lab Fluid Power & Mechatron Syst, Hangzhou 310027, Peoples R China
来源：
2018 IEEE CSAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2018年
基金：
中国国家自然科学基金;
关键词：
actuator faults; fault-tolerant control system; response performance; reliability analysis; TRACKING CONTROL; DESIGN;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The fault-tolerant control system of the large civil aircraft can response to several fault conditions by using specific fault-tolerant control strategies, which can further to improve the reliability of the aircraft. This paper presents a response performance based reliability analysis method. A comprehensive reliability concept is given considering both the functional reliability and the performance reliability. The simulation work also gives an example of the reliability analysis method. According to the simulation and reliability analysis work, the key hardware is very important for the aircraft fault-tolerant control system to be reconfigured successfully.
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页数：5
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