Research Of Redundancy Management on Fight Control Computer For Unmanned Aerial Vehicle

被引:0
|
作者
Liu Lu [1 ]
Chen Xin [1 ]
Cao Dong [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut NUAA, Nanjing, Jiangsu, Peoples R China
来源
关键词
electric flight control computer; redundancy management; distributed system; CAN bus;
D O I
10.4028/www.scientific.net/AMR.383-390.1573
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
Redundancy technology is very important to improve the reliability and fault tolerant of redundant flight control computer for unmanned aerial vehicle. The key technology is redundancy management strategies and methods. The redundancy management strategies and methods are researched based on hardware redundancy and software management for the sample redundant flight control computer The redundancy management strategies make full use of the advantages of distributed systems and the CAN bus transmission characteristics, and solve the problem of fault diagnosis and fault treatment and system reconfiguration. Results show that the strategies meet the design specifications of application requirements.
引用
收藏
页码:1573 / 1577
页数:5
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