在面向航天应用的FPGA设计中，必须采用容错设计技术来弥补器件本身抗辐射能力的不足。
Hence, FPGA fault tolerant design technology must be developed to make up for the insufficiency in radiation resistance of its components.
在设计控制系统中，采用了硬件冗余和软件容错技术，使得整个系统的可靠性大大增强。
In designing the control system, the hardware redundance and the software tolerance technology are adopted. It greatly enhances the reliability of the control system.
详细阐述了该系统设计与开发的目标、系统结构、业务流程、关键技术和容错处理。
The object of design and development of this system, system's structure, system's procedure, key technologies, mechanism in mistake are emphasized.
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