Sliced-LLDN: Hardware-Governed Deterministic Wireless Communication for Intra-Spacecraft and Intra-Launcher Applications

IF 3.7 Q2 ENGINEERING, ELECTRICAL & ELECTRONIC
Mohamed Khalil;Kai Müller;Karsten Peter
{"title":"Sliced-LLDN: Hardware-Governed Deterministic Wireless Communication for Intra-Spacecraft and Intra-Launcher Applications","authors":"Mohamed Khalil;Kai Müller;Karsten Peter","doi":"10.1109/JRFID.2026.3735816","DOIUrl":null,"url":null,"abstract":"Wireless sensor networks can reduce the mass and integration complexity of spacecraft and launch vehicle harnesses, yet existing flight-heritage implementations do not meet the determinism required by attitude control loops and launcher functional chains. This article presents Sliced-LLDN, a wireless sensor network protocol that binds MAC processing, radio access, upper-layer data handling, and sensor sampling to a single hardware-governed timeline. The protocol modifies the IEEE 802.15.4e LLDN MAC, operates over an impulse radio ultra-wideband physical layer, and is implemented bare-metal on a ZYNQ System-on-Chip platform. Each 1.0 ms timeslot is subdivided into hardware-timed slices to which all in-slot processes are pinned, yielding data latency that is constant rather than merely bounded and supporting up to five sensor nodes within a 10 ms superframe. Two data acquisition modes are formalized: synchronous sampling for network-wide time-aligned measurements and uniform-latency sampling for slot-position-independent sub-millisecond delivery. Experimental evaluation on a four-node network demonstrates timestamping accuracy within <inline-formula> <tex-math>$\\pm 4~\\mu $ </tex-math></inline-formula>s, synchronous sampling accuracy within <inline-formula> <tex-math>$\\pm 2~\\mu $ </tex-math></inline-formula>s, per-node latency of approximately <inline-formula> <tex-math>$930~\\mu $ </tex-math></inline-formula>s in uniform-latency mode, RMS jitter below <inline-formula> <tex-math>$1.1~\\mu $ </tex-math></inline-formula>s, and zero packet loss over one million superframes per node. These results satisfy the timing requirements of spacecraft attitude and orbit control systems and a subset of launch vehicle requirements.","PeriodicalId":73291,"journal":{"name":"IEEE journal of radio frequency identification","volume":"10 ","pages":"886-903"},"PeriodicalIF":3.7000,"publicationDate":"2026-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE journal of radio frequency identification","FirstCategoryId":"1085","ListUrlMain":"https://ieeexplore.ieee.org/document/11701502/","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"2026/9/22 0:00:00","PubModel":"Epub","JCR":"Q2","JCRName":"ENGINEERING, ELECTRICAL & ELECTRONIC","Score":null,"Total":0}
引用次数: 0

Abstract

Wireless sensor networks can reduce the mass and integration complexity of spacecraft and launch vehicle harnesses, yet existing flight-heritage implementations do not meet the determinism required by attitude control loops and launcher functional chains. This article presents Sliced-LLDN, a wireless sensor network protocol that binds MAC processing, radio access, upper-layer data handling, and sensor sampling to a single hardware-governed timeline. The protocol modifies the IEEE 802.15.4e LLDN MAC, operates over an impulse radio ultra-wideband physical layer, and is implemented bare-metal on a ZYNQ System-on-Chip platform. Each 1.0 ms timeslot is subdivided into hardware-timed slices to which all in-slot processes are pinned, yielding data latency that is constant rather than merely bounded and supporting up to five sensor nodes within a 10 ms superframe. Two data acquisition modes are formalized: synchronous sampling for network-wide time-aligned measurements and uniform-latency sampling for slot-position-independent sub-millisecond delivery. Experimental evaluation on a four-node network demonstrates timestamping accuracy within $\pm 4~\mu $ s, synchronous sampling accuracy within $\pm 2~\mu $ s, per-node latency of approximately $930~\mu $ s in uniform-latency mode, RMS jitter below $1.1~\mu $ s, and zero packet loss over one million superframes per node. These results satisfy the timing requirements of spacecraft attitude and orbit control systems and a subset of launch vehicle requirements.
切片- lldn:用于航天器内和发射器内应用的硬件控制的确定性无线通信
无线传感器网络可以降低航天器和运载火箭线束的质量和集成复杂性,但现有的飞行遗产实现不能满足姿态控制回路和发射功能链所要求的确定性。本文介绍了slice - lldn,这是一种无线传感器网络协议,它将MAC处理、无线电访问、上层数据处理和传感器采样绑定到单个硬件控制的时间轴上。该协议修改了IEEE 802.15.4e LLDN MAC,在脉冲无线电超宽带物理层上运行,并在ZYNQ片上系统平台上实现裸机。每个1.0 ms时隙被细分为硬件定时片,所有槽内进程都被固定在其中,产生恒定的数据延迟,而不仅仅是有限的,并且在10ms超帧内支持多达五个传感器节点。确定了两种数据采集模式:用于网络范围内时间对齐测量的同步采样和用于与插槽位置无关的亚毫秒交付的均匀延迟采样。在四节点网络上的实验评估表明,时间戳精度在$\pm 4~\mu $ s之间,同步采样精度在$\pm 2~\mu $ s之间,均匀延迟模式下每个节点的延迟约为$930~\mu $ s, RMS抖动低于$1.1~\mu $ s,并且每个节点超过100万超级帧时零数据包丢失。这些结果满足航天器姿态和轨道控制系统的定时要求以及运载火箭的子集要求。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
CiteScore
5.70
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信
小红书