同时对系统的结构特点、软件和硬件的配置、容错功能的实现等进行了分析和讨论。

Regarding subsonic wind tunnel as a monitored object, we discussed and analysed the structure and feature of system, allocation of software and hardware and implementation of tolerant function.

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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。

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.

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结果表明，在非容错商用计算机系统中加入简单的软件实现的错误检测机制，也可以达到很高的错误检测覆盖率。

The result show that a commercial non fault tolerant computer can achieve higher error detection coverage by adding simple software based EDMs in it.

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