{"title":"On-Board Partial Run-Time Reconfiguration for Pico-Satellite Constellations","authors":"T. Vladimirova, Xiaofeng Wu","doi":"10.1109/AHS.2006.54","DOIUrl":null,"url":null,"abstract":"Distributed satellite systems are considered a promising new direction in spacecraft architecture design. Pico-satellite constellations flying in low Earth orbit (LEO) could become an efficient and low-cost solution to Earth observation and remote sensing in the future. There is a pressing need for condition-based maintenance, self-repair and upgrade capabilities on-board satellites in order to enable future space applications. In this paper we present a methodology for onboard partial run-time reconfiguration to enable onboard system-level functional changes ensuring correct operation, longer life and higher quality of service. The technique of partial run-time reconfiguration is introduced and a remote reconfiguration methodology is described. The architecture of an FPGA-based reconfigurable SoC design for on-board computing is outlined. A case study, which demonstrates the feasibility of the approach, is presented","PeriodicalId":232693,"journal":{"name":"First NASA/ESA Conference on Adaptive Hardware and Systems (AHS'06)","volume":"4 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2006-06-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"18","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"First NASA/ESA Conference on Adaptive Hardware and Systems (AHS'06)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AHS.2006.54","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 18
Abstract
Distributed satellite systems are considered a promising new direction in spacecraft architecture design. Pico-satellite constellations flying in low Earth orbit (LEO) could become an efficient and low-cost solution to Earth observation and remote sensing in the future. There is a pressing need for condition-based maintenance, self-repair and upgrade capabilities on-board satellites in order to enable future space applications. In this paper we present a methodology for onboard partial run-time reconfiguration to enable onboard system-level functional changes ensuring correct operation, longer life and higher quality of service. The technique of partial run-time reconfiguration is introduced and a remote reconfiguration methodology is described. The architecture of an FPGA-based reconfigurable SoC design for on-board computing is outlined. A case study, which demonstrates the feasibility of the approach, is presented