摘要： 以作者自行研制的一种航空机载容错计算机系统为背景,论述了系统的设计原理及实现技术。系统采用基于硬件冗余的双通道热跟随体系结构。其冗余管理主要包括:故障检测、故障隔离、通道切换、故障报警等功能。

关键词: 容错, 冗余, 体系结构, 热跟随

Abstract: The paper described the design principles and implementation technologies of an aviation fault tolerant computer system, the computer system is based on dual channel and hot-following architecture of hardware redundancy

中图分类号: 

• TP302.8