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

Sebastián, Eduardo and Pérez, Joel and Bravo, Andrés and Ferrándiz, Ricardo and Fernández, Maite and Rodríguez Manfredi, J.A. and Peña, Antonio and González, David and Moreno, José and Pérez-Grande, Isabel and Chamarro, Adrián and Martínez, Germán and Lucas, Javier de and Hernández, Pedro and Ramos, Miguel (2017). Performance analysis of the MEDA's Thermal InfraRed Sensor (TIRS) on board the Mars 2020. In: "Proceding 2017 IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)", 21-23 jun 2017, Padua (Italia). pp. 85-92. https://doi.org/10.1109/MetroAeroSpace.2017.7999543.

Description

Title: Performance analysis of the MEDA's Thermal InfraRed Sensor (TIRS) on board the Mars 2020
Author/s:
  • Sebastián, Eduardo
  • Pérez, Joel
  • Bravo, Andrés
  • Ferrándiz, Ricardo
  • Fernández, Maite
  • Rodríguez Manfredi, J.A.
  • Peña, Antonio
  • González, David
  • Moreno, José
  • Pérez-Grande, Isabel
  • Chamarro, Adrián
  • Martínez, Germán
  • Lucas, Javier de
  • Hernández, Pedro
  • Ramos, Miguel
Item Type: Presentation at Congress or Conference (Article)
Event Title: Proceding 2017 IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)
Event Dates: 21-23 jun 2017
Event Location: Padua (Italia)
Title of Book: 2017 IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)
Date: June 2017
Subjects:
Faculty: Instituto de Microgravedad Ignacio Da Riva (UPM)
Department: Aeronaves y Vehículos Espaciales
Creative Commons Licenses: Recognition - No derivative works - Non commercial

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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 source-

More information

Item ID: 51007
DC Identifier: http://oa.upm.es/51007/
OAI Identifier: oai:oa.upm.es:51007
DOI: 10.1109/MetroAeroSpace.2017.7999543
Official URL: https://ieeexplore.ieee.org/document/7999543
Deposited by: Memoria Investigacion
Deposited on: 04 Apr 2019 12:14
Last Modified: 04 Apr 2019 12:40
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