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一种应用SpaceWire总线的即插即用星载计算机体系结构设计

江耿丰 陈龙 吴军

航天器工程2026,Vol.35Issue(3):90-96,7.
航天器工程2026,Vol.35Issue(3):90-96,7.DOI:10.3969/j.issn.1673-8748.2026.03.012

一种应用SpaceWire总线的即插即用星载计算机体系结构设计

A Plug-and-play Computer Architecture Design Based on SpaceWire Bus

江耿丰 1陈龙 1吴军1

作者信息

  • 1. 北京控制工程研究所,北京 100190
  • 折叠

摘要

Abstract

To address the limitations of long system integration cycle and difficult expansion caused by the heterogeneity of interfaces and software are protocols in traditional on-board com-puter(OBC),the technical system represented by the Space Plug and Play Electronic System Ar-chitecture(SPA)in the United States is studied,and a on-board computer architecture design scheme based on the SpaceWire bus is proposed in this paper.Firstly,the fundamental principles and implementation methodologies of plug-and-play technology are elaborated to ensure that the designed system is compatible with the SPA standard.Secondly,with the satellite attitude and control system(AOCS)as the application background,a proof-of-concept prototype is devel-oped,encompassing both hardware implementation and software architecture.To resolve univer-sality issues,an additional sensor interface module is designed.Furthermore,the synchronization network mechanism of the electronic system is improved using a SpaceWire time-code based de-sign.Finally,ground experiments demonstrate that the proposed architecture effectively sup-ports the rapid integration of on-board computers and enables stable closed-loop operation of the satellite AOCS.

关键词

即插即用/同步/星载计算机

Key words

plug-and-play/synchronization/on-board computer

分类

航空航天

引用本文复制引用

江耿丰,陈龙,吴军..一种应用SpaceWire总线的即插即用星载计算机体系结构设计[J].航天器工程,2026,35(3):90-96,7.

航天器工程

1673-8748

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