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dc.rights.licenseCopyright © 2017, IEEEes
dc.contributor.authorSebastián, E.es
dc.contributor.authorPérez, Joeles
dc.contributor.authorBravo, Andréses
dc.contributor.authorFerrándiz, R.es
dc.contributor.authorFernández, Maitees
dc.contributor.authorRodríguez Manfredi, J. A.es
dc.contributor.authorMartínez, G.es
dc.contributor.authorPeña, A.es
dc.contributor.authorGonzález, Davides
dc.contributor.authorMoreno, Josées
dc.contributor.authorDe Lucas Veguillas, Javieres
dc.contributor.authorHernández, Pedroes
dc.contributor.authorPérez Grande, I.es
dc.contributor.authorChamorro, Adriánes
dc.contributor.authorRamos, M.es
dc.date.accessioned2023-03-08T10:03:23Z-
dc.date.available2023-03-08T10:03:23Z-
dc.date.issued2017-06-23-
dc.identifier.citationIEEE International Workshop on Metrology for Aerospacees
dc.identifier.isbn9781509042357-
dc.identifier.otherhttps://ieeexplore.ieee.org/document/7999543es
dc.identifier.urihttp://hdl.handle.net/20.500.12666/860-
dc.description.abstractThe Thermal InfraRed Sensor (TIRS), an infrared (IR) radiometer developed at Centro de Astrobiología, is one the sensors that compose the Mars Environmental Dynamics Analyzer (MEDA) onboard NASA's Mars 2020 mission. It will measure the net thermal infrared radiation, reflected solar radiation at the surface, atmosphere temperature and surface skin brightness temperature using five different channels. The present paper provides a brief description on TIRS design and channels requirements. Then, a detailed presentation of sensor model equations and a sensitivity analysis to model uncertainties are included. Finally, accuracy and resolution calculus for each channel versus operational temperature is presented. The calculus is performed based on sensitivity equations and the estimated values for different uncertainties sources.es
dc.description.sponsorshipThis work forms part of the research project regarding the design and scientific issues of the NASA/MARS2020 MEDA. The authors would like to express special thanks to all MEDA Co-Is and personnel who participate in a variety of ways to the development of MEDA TIRS.es
dc.language.isoenges
dc.publisherInstitute of Electrical and Electronics Engineerses
dc.subjectIR radiometeres
dc.subjectMarses
dc.subjectPerformancees
dc.subjectAccuracyes
dc.subjectResolutiones
dc.subjectRequirementses
dc.subjectMEDAes
dc.subjectMars 2020es
dc.titlePerformance analysis of the MEDA's Thermal InfraRed Sensor (TIRS) on board the Mars 2020es
dc.typeinfo:eu-repo/semantics/conferenceObjectes
dc.identifier.doi10.1109/MetroAeroSpace.2017.7999543-
dc.identifier.e-issn9781509042340-
dc.contributor.funderInstituto Nacional de Técnica Aeroespacial (INTA)es
dc.description.peerreviewedPreprintes
dc.type.hasVersioninfo:eu-repo/semantics/publishedVersiones
dc.rights.accessRightsinfo:eu-repo/semantics/restrictedAccesses
dc.type.coarhttp://purl.org/coar/resource_type/c_5794es
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(Calib.) Comunicaciones de Congresos

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