{"title":"Dependable MPSoC-Based Mixed-Criticality Systems for Space Applications","authors":"Stefano Esposito, M. Violante","doi":"10.1109/METROAEROSPACE.2018.8453618","DOIUrl":null,"url":null,"abstract":"Space applications' requirements, especially when scientific payload is considered, are rapidly increasing. A way to satisfy such requirements without increasing too much space, weight, and power consumption of the on-board equipment, is to exploit capabilities of new multi-processor system-on-chips (MPSoCs). A MPSoC-based computer would allow integration on a single equipment of several applications. However, there is not any space-qualified MPSoC, yet. This paper describes a mixed-criticality system (MCS) implementing a prototypical scientific payload computer for a space mission. The main focus is on the issue of using commercial-off-the-shelf (COTS) MPSoC in radioactive environment to deploy MCS implementing a payload computer. The paper states the beforementioned issue and a set of countermeasures to detect issues. The system is evaluated for dependability against single event effects (SEEs) through fault-injection simulation experiments. Results of such experiments are used to compute availability figures of a payload computer implementing described countermeasures, considering the radiation environment of the geostationary orbit.","PeriodicalId":142603,"journal":{"name":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"23 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 5th IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/METROAEROSPACE.2018.8453618","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
Space applications' requirements, especially when scientific payload is considered, are rapidly increasing. A way to satisfy such requirements without increasing too much space, weight, and power consumption of the on-board equipment, is to exploit capabilities of new multi-processor system-on-chips (MPSoCs). A MPSoC-based computer would allow integration on a single equipment of several applications. However, there is not any space-qualified MPSoC, yet. This paper describes a mixed-criticality system (MCS) implementing a prototypical scientific payload computer for a space mission. The main focus is on the issue of using commercial-off-the-shelf (COTS) MPSoC in radioactive environment to deploy MCS implementing a payload computer. The paper states the beforementioned issue and a set of countermeasures to detect issues. The system is evaluated for dependability against single event effects (SEEs) through fault-injection simulation experiments. Results of such experiments are used to compute availability figures of a payload computer implementing described countermeasures, considering the radiation environment of the geostationary orbit.