{"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.