摘要
提出了一种航空机载容错计算机系统的设计与实现方法。该系统采用二模冗余的热跟随体系结构。重点分析了基于硬件冗余的冗余管理技术。通过冗余主要实现故障检测、故障隔离、通道切换与故障报警等。
This paper introduces an aviation fault tolerant computer system which is based on hardware redundancy architecture with two identical channels and hot follow. The redundancy management technique is emphatically described.
出处
《空军雷达学院学报》
2001年第3期42-45,共4页
Journal of Air Force Radar Academy