一种基于数字双子星的卫星网络sdc引起的天坑和灰洞节点检测与保护框架

IF 0.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Gongzhe Qiao, Zhuang Yi, Tong Ye, Yuan Qiao
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引用次数: 0

摘要

在空间环境中,宇宙射线和高能粒子可能在程序执行过程中引起单事件扰动(SEU),进而在程序输出中引起静默数据损坏(SDC)错误。通过对SEU和SDC误差的广泛研究,发现卫星网络路由程序中的SDC误差可能导致网络中出现Sinkhole (SH)和Grayhole (GH)节点,从而对卫星网络造成破坏。为了及时发现和解决问题,提出了一种基于数字孪生的卫星网络sdc诱导SH和GH节点检测与保护框架。首先,描述了SEU条件下的卫星网络故障模型以及SDC误差引起的SH和GH节点的产生机制;然后,设计了所提出的检测与保护框架所需的基于数字孪生的数据结构,并提出了由SDC错误引起的SH和GH节点的检测方法。利用SKT和LLFI仿真工具建立了模拟的铱星网络,并进行了断层注入实验。实验结果表明,所提检测方法的准确率为98-100%,所提框架导致的路由收敛的额外时间成本为3.1-28.2%。与现有的SH和GH检测方法相比,该方法能够及时、准确地检测路由更新阶段的故障。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Digital-Twin-Based Detection and Protection Framework for SDC-Induced Sinkhole and Grayhole Nodes in Satellite Networks
In the space environment, cosmic rays and high-energy particles may cause a single-event upset (SEU) during program execution, and further cause silent data corruption (SDC) errors in program outputs. After extensive research on SEU and SDC errors, it has been found that SDC errors in the routing program in satellite networks may lead to the emergence of Sinkhole (SH) and Grayhole (GH) nodes in the network, which may cause damage to satellite networks. To find and solve the problems in time, a digital-twin-based detection and protection framework for SDC-induced SH and GH nodes in satellite networks is proposed. First, the satellite network fault model under SEU and the generation mechanism of SH and GH nodes induced by SDC errors are described. Then, the data structure based on digital twins required by the proposed detection and protection framework is designed, and the detection methods of SH and GH nodes induced by SDC errors are proposed. SKT and LLFI simulation tools are used to build a simulated Iridium satellite network and carry out fault injection experiments. Experiment results show that the accuracy of the proposed detection method is 98–100%, and the additional time cost of routing convergence caused by the proposed framework is 3.1–28.2%. Compared with existing SH and GH detection methods, the proposed methods can timely and accurately detect faults during the routing update stage.
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来源期刊
Aerospace America
Aerospace America 工程技术-工程:宇航
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发文量
9
审稿时长
4-8 weeks
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