Performance analysis of the MEDA's Thermal InfraRed Sensor (TIRS) on board the Mars 2020
dc.contributor.author | Sebastián, E. | es |
dc.contributor.author | Pérez, Joel | es |
dc.contributor.author | Bravo, Andrés | es |
dc.contributor.author | Ferrándiz, R. | es |
dc.contributor.author | Fernández, Maite | es |
dc.contributor.author | Rodríguez Manfredi, J. A. | es |
dc.contributor.author | Martínez, G. | es |
dc.contributor.author | Peña, A. | es |
dc.contributor.author | González, David | es |
dc.contributor.author | Moreno, José | es |
dc.contributor.author | De Lucas Veguillas, Javier | es |
dc.contributor.author | Hernández, Pedro | es |
dc.contributor.author | Pérez Grande, I. | es |
dc.contributor.author | Chamorro, Adrián | es |
dc.contributor.author | Ramos, M. | es |
dc.contributor.funder | Instituto Nacional de Técnica Aeroespacial (INTA) | es |
dc.date.accessioned | 2023-03-08T10:03:23Z | |
dc.date.available | 2023-03-08T10:03:23Z | |
dc.date.issued | 2017-06-23 | |
dc.description.abstract | The 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.peerreviewed | Preprint | es |
dc.description.sponsorship | This 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.citation | IEEE International Workshop on Metrology for Aerospace | es |
dc.identifier.doi | 10.1109/MetroAeroSpace.2017.7999543 | |
dc.identifier.e-issn | 9781509042340 | |
dc.identifier.isbn | 9781509042357 | |
dc.identifier.other | https://ieeexplore.ieee.org/document/7999543 | es |
dc.identifier.uri | http://hdl.handle.net/20.500.12666/860 | |
dc.language.iso | eng | es |
dc.publisher | Institute of Electrical and Electronics Engineers | es |
dc.rights.accessRights | info:eu-repo/semantics/restrictedAccess | es |
dc.rights.license | Copyright © 2017, IEEE | es |
dc.subject | IR radiometer | es |
dc.subject | Mars | es |
dc.subject | Performance | es |
dc.subject | Accuracy | es |
dc.subject | Resolution | es |
dc.subject | Requirements | es |
dc.subject | MEDA | es |
dc.subject | Mars 2020 | es |
dc.title | Performance analysis of the MEDA's Thermal InfraRed Sensor (TIRS) on board the Mars 2020 | es |
dc.type | info:eu-repo/semantics/conferenceObject | es |
dc.type.coar | http://purl.org/coar/resource_type/c_5794 | es |
dc.type.hasVersion | info:eu-repo/semantics/publishedVersion | es |
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