| 卫星控制系统的三机容错计算机系统 |
| |
| 引用本文： | 王桂英,杨孟飞,常隆兴.卫星控制系统的三机容错计算机系统[J].航天控制,1990(4). |
| |
| 作者姓名： | 王桂英 杨孟飞 常隆兴 |
| |
| 作者单位： | 北京控制工程研究所
(王桂英，杨孟飞)，北京控制工程研究所(常隆兴) |
| |
| 摘 要： | 本文讨论了容错计算机的三种容错结构,即D/S(双机变单机)、TMR/J(三模冗余变单机)、以及TMR/D/S(三模冗余变双机再变单机)结构。给出了三种容错结构的可靠性数学模型,对影响可靠性的诸多因素进行了讨论、比较,确定采用TMR/S方案。文中对TMR/S的硬件设置及容错管理程序做了简要介绍。对从事容错设计的工程技术人员有一定参考价值。
|
| 关 键 词： | ~+三重模块冗余 容错计算机 自动控制系统 |
TMR BASED FAULT-TOLERANT ONBOARD COMPUTER FOR SATELLITE CONTROL SYSTEM |
| |
| Wang Guiying,Yang Mengfei,Chang Longxing Beijing Institute of Control Engineering.TMR BASED FAULT-TOLERANT ONBOARD COMPUTER FOR SATELLITE CONTROL SYSTEM[J].Aerospace Control,1990(4). |
| |
| Authors: | Wang Guiying Yang Mengfei Chang Longxing Beijing Institute of Control Engineering |
| |
| Institution: | Wang Guiying;Yang Mengfei;Chang Longxing Beijing Institute of Control Engineering |
| |
| Abstract: | In this paper, three fanlt-tolerant structures of a fanlt-tolerantcomputer, or D/S,TMR/S and TMR/D /S, are discussed. Their reliabitlity models are given, such factorseffecting on the releability are analyzed and compared, Finally the TMR/S structure is de-termined, In addition, The hardware configuration and fanlt-tolerant management routines ofthe TMR/S system are described in brief. |
| |
| Keywords: | ~+Triple modular redundancy Fault tolerant computer Automatic control system |
| 本文献已被 CNKI 等数据库收录！ |
