{"title":"System architecture for Byzantine resilient computation in launch vehicle applications","authors":"M. Iacoponi, R. Grisell","doi":"10.1109/DASC.1990.111307","DOIUrl":null,"url":null,"abstract":"A system architecture for fault-tolerant computation is presented that meets or exceeds projected unmanned and manned launch vehicle requirements. The system architecture discussed is under development at Harris Corporation on the Advanced Fault-Tolerant Data Processor (AFTDP) project. The AFTDP addresses both long-life missions where resource preservation is critical and shorter-life ultra-reliable missions relevant to launch vehicle applications. A distributed computation model is used to achieve robust fault tolerance based on a Byzantine fault model. The AFTDP employs a high-performance shared-memory multiprocessing model of computation for application programs, which is based on a 20 million instruction per second RISC (reduced-instruction-set computer) processor.<<ETX>>","PeriodicalId":141205,"journal":{"name":"9th IEEE/AIAA/NASA Conference on Digital Avionics Systems","volume":"8 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1990-10-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"9th IEEE/AIAA/NASA Conference on Digital Avionics Systems","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/DASC.1990.111307","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
A system architecture for fault-tolerant computation is presented that meets or exceeds projected unmanned and manned launch vehicle requirements. The system architecture discussed is under development at Harris Corporation on the Advanced Fault-Tolerant Data Processor (AFTDP) project. The AFTDP addresses both long-life missions where resource preservation is critical and shorter-life ultra-reliable missions relevant to launch vehicle applications. A distributed computation model is used to achieve robust fault tolerance based on a Byzantine fault model. The AFTDP employs a high-performance shared-memory multiprocessing model of computation for application programs, which is based on a 20 million instruction per second RISC (reduced-instruction-set computer) processor.<>