This paper presents a fault-tolerant software design method and its application to the micro-controller system (MCS-51) of a type of Pilotless aircraft.
本文介绍了某型无人驾驶飞机系列MCS - 51单片机控制系统的软件容错设计方法与实现。
When actuator is in trouble, we give a design method of fault tolerant controller for pipeline's normally running.
保证管道运行工况平稳,给出了执行器故障时容错控制器的设计方法。
The test structure and test method in an air-born real-time fault-tolerant distributed computer system are dealt. The design of test controller and test buses are also discussed briefly.
阐述了机载实时容错分布式计算机系统测试体系结构及测试方法,并简要介绍了测试总线和测试控制器的设计。
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