基于异构箭控平台的动态重构设计与实现

Ran Tao, Gang Xiang, Y. Luo, Kun Tian, Hui Li, Zhaolei Wang
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引用次数: 0

摘要

传统的火箭控制计算平台多采用硬件冗余的方式来提升可靠性,同样存在硬件冗余常见故障、无法应对复杂环境的缺点,提出了基于异构架构的火箭控制平台,通过采用SOPC、FPGA和DSP三大核心组件构建新一代控制计算平台,具有可靠性高、对环境适应性强等特点。异构平台以SOPC为核心,通过高速串行传输完成数据传输,支持动态逻辑重构,利用动态重构技术实现异常状态下的自恢复。本文详细介绍了平台的体系结构、数据传输与同步方法、动态重构策略和控制方法。最后,通过实验和仿真验证了平台设计的正确性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design and Implementation of Dynamic Reconfiguration Based on Heterogeneous Arrow Control Platform
Traditional rocket control computing platform use hardware redundancy more ways to promote the reliability, the same hardware redundancy of common cause failure, unable to cope with complex environment against the shortcomings, is proposed based on heterogeneous architecture arrows control platform, by using SOPC, FPGA and DSP three core components to build a new generation of control computing platform, has high reliability, strong adaptability to environment, etc. With SOPC as the core, the heterogeneous platform completes data transmission through high-speed serial transmission, supports dynamic logical reconstruction, and utilizes dynamic reconstruction technology to realize self-recovery under abnormal state. In this paper, the platform architecture, data transmission and synchronization methods, dynamic reconstruction strategy and control methods are described in detail. Finally, the correctness of the platform design is verified by experiments and simulations.
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