NASA LogoNTRSNTRS - NASA Technical Reports ServerSearchmore_vertCollectionsAboutNewsHelpLogin Back to ResultsOptical Communication Link Atmospheric Attenuation ModelThe Space Communications and Navigation (SCaN) Center for Networking, Integration, and Communications (SCENIC) user interface, which provides web accessible space mission simulation and communication system analysis capabilities using verified and validated analysis algorithms, can execute analyses including, but not limited to, line-of-sight, orbit propagation, and dynamic link budget calculations between sets of missions and/or assets. SCENIC's purpose is to provide NASA civil servants and contractors a user-friendly tool, integrated with model data, that can simulate and analyze a range of space mission architectures without the need for repeated and redundant modeling. Given the abundance and further future development of free space optical (FSO) communication channels within modern space infrastructure, the availability of a reliable optical link analysis capability is crucial for SCENIC users. The efforts outlined in this paper aim to provide a model for atmospheric attenuation of FSO communication links, both due to absorption/scattering and turbulence, to increase the accuracy of SCENIC's optical link assessment capabilities. A previous model existed for optical absorption/scattering within the SCaN Link Budget Tool, but it was not location specific for the Earth ground-based nodes, nor was the model optimized for run-time. The new model utilizes years of National Oceanic and Atmospheric Administration (NOAA) visibility data from ground station locations around the world. Visibility, along with the wavelength of the optical signal, are input parameters to calculate the optical specific attenuation, which is a parameter in the calculation of the slant-path attenuation. A final FSO atmospheric attenuation value is comprised of the absorption/scattering attenuation and the turbulence attenuation. A run-time efficient algorithm for the model was then developed and programmed in MATLAB®. Due to the simple model and vectorization possible in MATLAB, the algorithm has an average run-time of less than one fourth of the run-time of the previous implementation.Document ID20190001012Acquisition SourceGlenn Research CenterDocument TypeTechnical Memorandum (TM)AuthorsGreen, Jack L.*(Tulane Univ. New Orleans, LA, United States)*Welch, Bryan W.*(NASA Glenn Research Center Cleveland, OH, United States)*Manning, Robert M.*(NASA Glenn Research Center Cleveland, OH, United States)*Date AcquiredFebruary 27, 2019Publication DateFebruary 1, 2019Subject CategoryCommunications And RadarReport/Patent NumberE-19597NASA/TM-2019-219991GRC-E-DAA-TN60479Funding Number(s)WBS: WBS 439432.07.01.03.02Distribution LimitsPublicCopyrightPublic Use Permitted.Available DownloadsNameType20190001012.pdfSTIcloud_downloadcontent_copyvisibilityRelated RecordsThere are no records associated with this record.visibility_offNo Preview Available
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