Performance analysis of the MEDA's Thermal InfraRed Sensor (TIRS) on board the Mars 2020

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.contributor.funderInstituto Nacional de Técnica Aeroespacial (INTA)es
dc.date.accessioned2023-03-08T10:03:23Z
dc.date.available2023-03-08T10:03:23Z
dc.date.issued2017-06-23
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.peerreviewedPreprintes
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.identifier.citationIEEE International Workshop on Metrology for Aerospacees
dc.identifier.doi10.1109/MetroAeroSpace.2017.7999543
dc.identifier.e-issn9781509042340
dc.identifier.isbn9781509042357
dc.identifier.otherhttps://ieeexplore.ieee.org/document/7999543es
dc.identifier.urihttp://hdl.handle.net/20.500.12666/860
dc.language.isoenges
dc.publisherInstitute of Electrical and Electronics Engineerses
dc.rights.accessRightsinfo:eu-repo/semantics/restrictedAccesses
dc.rights.licenseCopyright © 2017, IEEEes
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.type.coarhttp://purl.org/coar/resource_type/c_5794es
dc.type.hasVersioninfo:eu-repo/semantics/publishedVersiones

Archivos

Bloque original

Mostrando 1 - 1 de 1
Cargando...
Miniatura
Nombre:
acceso-restringido.pdf
Tamaño:
221.73 KB
Formato:
Adobe Portable Document Format
Descripción:

Bloque de licencias

Mostrando 1 - 1 de 1
No hay miniatura disponible
Nombre:
license.txt
Tamaño:
4.82 KB
Formato:
Item-specific license agreed upon to submission
Descripción: