一种航空机载容错计算机的冗余管理技术

Redundancy Management Technique on an Aviation Fault Tolerant Computer

文章介绍了作者自行研制的一种航空机载容错计算机系统的设计与实现,系统采用双通道热跟随体系结构。重点分析了基于硬件冗余的冗余管理技术。其冗余主要包括:故障检测、故障隔离、通道切换与故障报警等。

This paper introduces an aviation fault tolerant computer system which based hardware redundancy architec-ture with two same channels and hot follow,its redundancy management technique will be described specially.