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(3)CAT-2: attitude determination and control system for a GNSS-R earth observation 6U CubeSat mission

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3CAT 2 Attitude Determination and Control System for a GNSS R Earth Observation 6U CubeSat Mission.pdf (2,592Mb)
 
10.5721/EuJRS20164940
 
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Cita com:
hdl:2117/102946

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Cortiella, Alexandre
Vidal Mateu, David
Jané Abad, Jaume
Juan, Enric
Olivé, Roger
Amézaga Sarries, Adrià
Francesc Muñoz, Joan
Carreño Luengo, Hugo
Camps Carmona, Adriano JoséMés informacióMés informacióMés informació
Document typeArticle
Defense date2016
Rights accessOpen Access
Attribution 3.0 Spain
This work is protected by the corresponding intellectual and industrial property rights. Except where otherwise noted, its contents are licensed under a Creative Commons license : Attribution 3.0 Spain
Abstract
This work describes the attitude determination and control system ( ADCS) of 3 CAT-2, a six-unit CubeSat scheduled for launch this 2016. The ADCS of 3CAT-2 aims at controlling the satellite in orbit and fulfilling the pointing requirements imposed by the mission. The attitude control system implemented in 3CAT-2 will be used to point the antennas towards the Earth to perform altimetry tests, orient the solar panels towards the Sun to maximize power input when battery levels are critical, and reduce the tumbling motion of the satellite after the deployment phase. In order to guarantee pointing requirements for remote sensing purposes, an active three-axis attitude determination and control system is considered.
CitationCortiella, A., Vidal, D., Jane, J., Juan, E., Olivé, R., Amezaga, A., Francesc, J., Carreño-Luengo, H., Camps, A. (3)CAT-2: attitude determination and control system for a GNSS-R earth observation 6U CubeSat mission. "European Journal of Remote Sensing", 2016, vol. 49, núm. 1, p. 759-776. 
URIhttp://hdl.handle.net/2117/102946
DOI10.5721/EuJRS20164940
ISSN2279-7254
Publisher versionhttp://www.tandfonline.com/doi/abs/10.5721/EuJRS20164940
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  • Departament de Teoria del Senyal i Comunicacions - Articles de revista [2.644]
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