Selen Gecgel Cetin, Angeles Vazquez-Castro, Gunes Karabulut Kurt
{"title":"Cislunar Communication Performance and System Analysis with Uncharted Phenomena","authors":"Selen Gecgel Cetin, Angeles Vazquez-Castro, Gunes Karabulut Kurt","doi":"arxiv-2409.09426","DOIUrl":null,"url":null,"abstract":"The Moon and its surrounding cislunar space have numerous unknowns,\nuncertainties, or partially charted phenomena that need to be investigated to\ndetermine the extent to which they affect cislunar communication. These include\ntemperature fluctuations, spacecraft distance and velocity dynamics, surface\nroughness, and the diversity of propagation mechanisms. To develop robust and\ndynamically operative Cislunar space networks (CSNs), we need to analyze the\ncommunication system by incorporating inclusive models that account for the\nwide range of possible propagation environments and noise characteristics. In\nthis paper, we consider that the communication signal can be subjected to both\nGaussian and non-Gaussian noise, but also to different fading conditions.\nFirst, we analyze the communication link by showing the relationship between\nthe brightness temperatures of the Moon and the equivalent noise temperature at\nthe receiver of the Lunar Gateway. We propose to analyze the ergodic capacity\nand the outage probability, as they are essential metrics for the development\nof reliable communication. In particular, we model the noise with the additive\nsymmetric alpha-stable distribution, which allows a generic analysis for\nGaussian and non-Gaussian signal characteristics. Then, we present the\nclosed-form bounds for the ergodic capacity and the outage probability.\nFinally, the results show the theoretically and operationally achievable\nperformance bounds for the cislunar communication. To give insight into further\ndesigns, we also provide our results with comprehensive system settings that\ninclude mission objectives as well as orbital and system dynamics.","PeriodicalId":501034,"journal":{"name":"arXiv - EE - Signal Processing","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2024-09-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"arXiv - EE - Signal Processing","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/arxiv-2409.09426","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
The Moon and its surrounding cislunar space have numerous unknowns,
uncertainties, or partially charted phenomena that need to be investigated to
determine the extent to which they affect cislunar communication. These include
temperature fluctuations, spacecraft distance and velocity dynamics, surface
roughness, and the diversity of propagation mechanisms. To develop robust and
dynamically operative Cislunar space networks (CSNs), we need to analyze the
communication system by incorporating inclusive models that account for the
wide range of possible propagation environments and noise characteristics. In
this paper, we consider that the communication signal can be subjected to both
Gaussian and non-Gaussian noise, but also to different fading conditions.
First, we analyze the communication link by showing the relationship between
the brightness temperatures of the Moon and the equivalent noise temperature at
the receiver of the Lunar Gateway. We propose to analyze the ergodic capacity
and the outage probability, as they are essential metrics for the development
of reliable communication. In particular, we model the noise with the additive
symmetric alpha-stable distribution, which allows a generic analysis for
Gaussian and non-Gaussian signal characteristics. Then, we present the
closed-form bounds for the ergodic capacity and the outage probability.
Finally, the results show the theoretically and operationally achievable
performance bounds for the cislunar communication. To give insight into further
designs, we also provide our results with comprehensive system settings that
include mission objectives as well as orbital and system dynamics.