Ting Wang, Yu'e Gao, Ce Li, Jinzhun Wang, Chong Wang
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引用次数: 0
Abstract
Targeted at the requirements of high reliability and extensibility of space station payload system, an On-orbit Reconfigurable Technology and implementation method based on SmartFusion2 is proposed. Adopting the theory of In Application Programming (IAP), the technical principles and key techniques of reconfigurable SmartFusion2 space station payload system is studied profoundly while the framework of “boot+3 Apps” is employed to update the application by means of ground data injection and to realize code area switch through the cooperation of the application and boot. With comprehensive consideration of the needs of the space-ground communication link, on-orbit operation control and space experiment, the reliability design is conducted from the perspectives of redundancy, verification and enabling protection, forming a common upload function module that can be easily ported to other processor platforms.
针对空间站有效载荷系统高可靠性和可扩展性的要求,提出了一种基于SmartFusion2的在轨可重构技术与实现方法。采用IAP (In Application Programming)理论,深入研究了可重构SmartFusion2空间站有效载荷系统的技术原理和关键技术,采用“boot+3 Apps”的框架,通过地面数据注入对应用进行更新,并通过应用与引导的协同实现代码区切换。综合考虑地空通信链路、在轨运行控制、空间实验等需求,从冗余、验证、使能保护等角度进行可靠性设计,形成通用上传功能模块,便于移植到其他处理器平台。