DocumentCode :
2977973
Title :
MEMS solar sensor testing for satellite applications
Author :
Ortega, J. Garcia ; Tarrida, C.L. ; Quero, J.M. ; Delgado, F.J. ; Ortega, P. ; Castaner, L. ; Reina, M. ; Angulo, M. ; Morilla, Y. ; Lopez, J. Garcia
Author_Institution :
Dept. de Ing. Electron., Univ. de Sevilla (US), Sevilla
fYear :
2009
fDate :
11-13 Feb. 2009
Firstpage :
345
Lastpage :
348
Abstract :
Solar sensors are very common devices used for attitude control of satellites. MEMS technology is very useful to reach the target of reducing the sensor size and cost. We have designed and manufactured a 2 axis analog sun sensor in order to be testing and validated in a real application. The sensor is boarding in the NANOSAT 1B Spanish satellite to be launched in 2009. For several years the satellite and the load devices will be exposed to very hard working conditions. Very accurate calibrating and testing processes have been developed in land to ensure a right performance in orbit. Mechanical, electrical and thermal tests have been applied to the sensor. These tests and its results are discussed In this paper.
Keywords :
aerospace instrumentation; artificial satellites; attitude control; calibration; mechanical testing; micromechanical devices; microsensors; thermal analysis; MEMS solar sensor; NANOSAT 1B Spanish satellite; analog sun sensor; calibration process; mechanical test; satellite attitude control; thermal test; Aluminum; Manufacturing; Mechanical sensors; Micromechanical devices; Photodiodes; Protection; Satellites; Space technology; Sun; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electron Devices, 2009. CDE 2009. Spanish Conference on
Conference_Location :
Santiago de Compostela
Print_ISBN :
978-1-4244-2838-0
Electronic_ISBN :
978-1-4244-2839-7
Type :
conf
DOI :
10.1109/SCED.2009.4800503
Filename :
4800503
Link To Document :
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