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小卫星设计中软件重注入的关键技术研究 被引量:2

RESEARCH ON THE PROGRAM RELOADING IN THE MICRO-SATELLITE DESIGN
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摘要 针对小卫星的一体化设计思想,采用CCSDS测控体制,星上采用CAN总线的分布网络,对小卫星软件重注入的课题做了深入的研究. The difference of the development of modern micro-satellite from traditional large satellites is the introduction of the integration conception. The integrated design conception of the micro-satellite make the program reloading on-board form the trend in the development of small satellite. Based on the conception of modularization and standardization, a method for program reloading in the micro-satellite is proposed and discussed in detail to meet the requirement of the micro-satellite design principle in this paper. The discussion is based on the CCSDS telemetry and telecommand scheme and distributed system on board connected with CAN bus. Some extension of the CAN protocol is involved to distinguish the normal data and program data when the node is receiving bytes from the bus. And some additional processes ensure the program data's security and precision. This method can be developed for system bootloading or just for error handling and system re-construction on-board. It will have wide application in the future.
出处 《空间科学学报》 CAS CSCD 北大核心 2002年第3期275-281,共7页 Chinese Journal of Space Science
关键词 卫星设计 软件重注 分布式系统 分包遥测 遥控 CAN总线 Program reloading, Distributed system, Packet telemetry, Packet telecommand, CAN field bus
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  • 22,左莉华.我国载人航天测控与通信系统实施AOS的技术途径研究.见:与CCSDS标准接轨专题研究文集,1996:54-65
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