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Authordc.contributor.authorGutiérrez, Samuel T.
Authordc.contributor.authorFuentes, César I.
Authordc.contributor.authorDíaz, Marcos A.
Admission datedc.date.accessioned2023-03-09T19:43:21Z
Available datedc.date.available2023-03-09T19:43:21Z
Publication datedc.date.issued2020
Cita de ítemdc.identifier.citationIEEE Access Volume 8, 2020es_ES
Identifierdc.identifier.other10.1109/ACCESS.2020.3020048
Identifierdc.identifier.urihttps://repositorio.uchile.cl/handle/2250/192025
Abstractdc.description.abstractAbsolute attitude estimation sensors provide high accuracy pointing capabilities to spacecraft, but as developed thus far, they constitute a large fraction of CubeSat mission’s budget. We introduce SPE Lab Open Star Tracker (SOST), an ultra-low-cost solution that currently provides sub-arcminute precision at a frequency of 1 to 3 estimations per minute in the Lost-In-Space scenario. Our Star Tracker development rests on open source astronomy software, the Raspberry Pi 3 B+, and its camera. We developed a new algorithm to solve the Lost-In-Space problem that works by acquiring an image and comparing it with different stellar catalog segments. We tested our algorithm using images from working satellites. The functioning of our platform was evaluated by using night-sky pictures taken from ground. We also conducted environmental tests of our platform by using a thermal-vacuum chamber. We optimized the catalog segment separation by analyzing the execution time, success rate, precision, and power consumption of the full platform. SOST delivers a mean precision below 1-arcminute for the boresight direction. With a segment separation of 10◦ , the attitude estimation is found in the 97.3% of the cases with processing time under 20s. The success rate improves to 99.8% by using 5 ◦ as segments separation but processing time doubles. This platform is open and freely available to CubeSat researchers interested in further development or deployment.es_ES
Patrocinadordc.description.sponsorshipUnited States Department of Defense Air Force Office of Scientific Research (AFOSR) FA9550-18-1-0249 Comision Nacional de Investigacion Cientifica y Tecnologica (CONICYT) 190004 Comision Nacional de Investigacion Cientifica y Tecnologica (CONICYT) CONICYT FONDECYT 1211331 1151476 CONICYT Fondo de Equipamiento Cientifico y Tecnologico (FONDEQUIP) EQM150138es_ES
Lenguagedc.language.isoenes_ES
Publisherdc.publisherIEEE-Inst Electrical Electronics Engineerses_ES
Type of licensedc.rightsAttribution-NonCommercial-NoDerivs 3.0 United States*
Link to Licensedc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/us/*
Sourcedc.sourceIEEE Accesses_ES
Keywordsdc.subjectAttitude determinationes_ES
Keywordsdc.subjectCubeSates_ES
Keywordsdc.subjectLow-cost hardwarees_ES
Keywordsdc.subjectNanosatelliteses_ES
Keywordsdc.subjectOpen-sourcees_ES
Keywordsdc.subjectRaspberry Pies_ES
Keywordsdc.subjectStar trackeres_ES
Títulodc.titleIntroducing SOST: An Ultra-Low-Cost Star Tracker Concept Based on a Raspberry Pi and Open-Source Astronomy Softwarees_ES
Document typedc.typeArtículo de revistaes_ES
dc.description.versiondc.description.versionVersión publicada - versión final del editores_ES
dcterms.accessRightsdcterms.accessRightsAcceso abiertoes_ES
Catalogueruchile.catalogadorlajes_ES
Indexationuchile.indexArtículo de publícación WoSes_ES


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Attribution-NonCommercial-NoDerivs 3.0 United States
Except where otherwise noted, this item's license is described as Attribution-NonCommercial-NoDerivs 3.0 United States