MultiChipSat Fault-Tolerant Architecture

Matthew McCormack, A. Saenz-Otero
{"title":"MultiChipSat Fault-Tolerant Architecture","authors":"Matthew McCormack, A. Saenz-Otero","doi":"10.1109/ISORCW.2011.17","DOIUrl":null,"url":null,"abstract":"With the process size of microelectronics shrinking well below 90 nm, the characteristics of upsets experienced by spacecraft avionics are drastically changing; traditional hardware mitigation techniques are reaching performance limitations. A method for achieving reliability, along with the performance capabilities of new technologies, is through the use of an innovative avionics architecture which utilizes both software and hardware redundancy techniques to achieve reliability. Instead of ensuring consistent reliability levels to every operation, the fault mitigation levels are user defined for each operation. Thus the architecture allows the system to be optimized about the needed fault tolerance and performance characteristics of each operation through its use of tightly coupled hardware and software design.","PeriodicalId":126022,"journal":{"name":"2011 14th IEEE International Symposium on Object/Component/Service-Oriented Real-Time Distributed Computing Workshops","volume":"13 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2011-03-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2011 14th IEEE International Symposium on Object/Component/Service-Oriented Real-Time Distributed Computing Workshops","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ISORCW.2011.17","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2

Abstract

With the process size of microelectronics shrinking well below 90 nm, the characteristics of upsets experienced by spacecraft avionics are drastically changing; traditional hardware mitigation techniques are reaching performance limitations. A method for achieving reliability, along with the performance capabilities of new technologies, is through the use of an innovative avionics architecture which utilizes both software and hardware redundancy techniques to achieve reliability. Instead of ensuring consistent reliability levels to every operation, the fault mitigation levels are user defined for each operation. Thus the architecture allows the system to be optimized about the needed fault tolerance and performance characteristics of each operation through its use of tightly coupled hardware and software design.
MultiChipSat容错架构
随着微电子工艺尺寸缩小到90 nm以下,航天器航空电子设备所经历的扰动特性正在发生巨大变化;传统的硬件缓解技术正在达到性能极限。实现可靠性的一种方法,以及新技术的性能能力,是通过使用创新的航空电子架构,利用软件和硬件冗余技术来实现可靠性。用户为每个操作定义了故障缓解级别,而不是确保每个操作的可靠性级别一致。因此,该体系结构允许系统通过使用紧密耦合的硬件和软件设计来优化每个操作所需的容错性和性能特征。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信