基于Zynq芯片的星载系统在轨运行优化方法及系统

By adopting a hierarchical reconfiguration mode and ARM+FPGA co-design, the problem of low on-orbit reliability of Zynq chips was solved, enabling active loading and refreshing, and improving the on-orbit operational stability and data accuracy of the spaceborne system.

CN121957725BActive Publication Date: 2026-07-17HUNAN SIBEITU TECH CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
HUNAN SIBEITU TECH CO LTD
Filing Date
2026-04-02
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Zynq chips have low on-orbit reliability, complex loading methods, and difficulty in implementing refresh functions, resulting in limited on-orbit use.

Method used

The system adopts a hierarchical reconstruction mode, which actively determines the loading requirements through the ground station. It utilizes the collaborative design of ARM processing system and FPGA programmable logic to achieve active loading and refreshing. It combines hardware-level and software-level verification to form a dual verification mechanism. The independent storage area isolates data, simplifies the process, and records telemetry data.

Benefits of technology

It significantly improves the reliability of on-orbit operation of satellite programs, reduces data transmission and storage error rates, solves the problem of missing records in traditional Zynq refresh functions, and enhances the stability of on-orbit operation of the system.

✦ Generated by Eureka AI based on patent content.

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Abstract

本发明涉及一种基于Zynq芯片的星载系统在轨运行优化方法及系统。所述方法包括:当地面站判定需更新星载系统的加载程序时,发送第一重构指令与加载文件至星载系统,ARM处理系统响应第一重构指令后,切换至加载存储区,通过FPGA可编程逻辑解析加载文件并执行一级校验通过后,从DDR中提取加载文件执行二级校验,完成第一次重构。当地面站判定需更新星载系统的运行程序时,发送第二重构指令与刷新文件至星载系统,ARM处理系统响应第二重构指令后,切换至刷新存储区,通过FPGA可编程逻辑解析刷新文件并执行一级校验通过后,从DDR中提取刷新文件执行二级校验,完成第二次重构。采用本方法能够提高星载程序在轨运行可靠性。
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