Integrated platform of on-board computer and star sensor electronics system based on COTS

XiaoXiao Feng, Shengwei Meng, Xiuhai Cui
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Abstract

In recent years, with the deployment and application of LEO microsatellite constellations, microsatellite has entered the development stage of “blowout”. How to further improve the performance of the microsatellite electronic system, the utilization rate and reliability of computing resources, reduce its cost and volume and weight has become one of the key problems in the design of a microsatellite electronic system. Based on COTS (Commercial-Off-The-Shelf), an integrated platform of on-board computer and star sensor electronics system is designed in this paper. The platform adopts heterogeneous multiprocessor architecture, which makes up for the low reliability of commercial devices. Its comprehensive computing capacity can reach 14000MIPS, compared with the general space antiradiation processing platform, its performance is improved by 10~100 times. The reliability analysis shows that the reliability of the platform is not less than 0.9999 in three years.
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基于COTS的星载计算机与星敏感器电子系统集成平台
近年来,随着低轨道微卫星星座的部署和应用,微卫星进入了“井喷式”发展阶段。如何进一步提高微卫星电子系统的性能、计算资源的利用率和可靠性,降低微卫星电子系统的成本和体积重量,已成为微卫星电子系统设计中的关键问题之一。本文以商用现货为基础,设计了星载计算机与星敏感器电子系统集成平台。该平台采用异构多处理器架构,弥补了商用设备可靠性低的不足。其综合计算能力可达14000MIPS,与一般空间抗辐射处理平台相比,性能提升10~100倍。可靠性分析表明,三年内平台的可靠性不小于0.9999。
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