针对样例主从式双余度飞控计算机体系架构,提出一种容错管理策略,设计了系统故障检测与诊断、系统资源管理、故障恢复等算法。在无人机半物理仿真平台下进行了容错策略算法测试,结果表明,该容错策略正确,算法功能和性能满足工程应用需求。 Aimed at the master-slave dual redundant flight control computer architecture, a fault-tolerant management strategy was proposed and the algorithms of system fault detection and diagnosis, system resource management and fault recovery were designed. Fault-tolerant strategy algorithm is tested under the semi-physical simulation platform of UAV. The results show that the fault-tolerant strategy is correct, and the algorithm function and performance meet the requirements of engineering application.