Design of a Nanosatellite Ground Monitoring and Control Software – a Case Study

The growing countries that have carried out the development of CubeSat missions for academic purposes do not offer aerospace engineering programs at their universities. This causes difficulties for traditional engineers upon the formal use of different standards and frameworks for aerospace developm...

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Main Authors: Freddy Alexander Díaz González, Pablo Roberto Pinzón Cabrera, Claudio Marcel Hernández Calderón
Format: Article
Language:English
Published: Departamento de Ciência e Tecnologia Aeroespacial 2016-04-01
Series:Journal of Aerospace Technology and Management
Subjects:
3D
Online Access:http://www.jatm.com.br/ojs/index.php/jatm/article/view/553
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spelling doaj-d6e84b8cb2364f75bf88db4178c5efba2020-11-25T01:55:59ZengDepartamento de Ciência e Tecnologia AeroespacialJournal of Aerospace Technology and Management1984-96482175-91462016-04-018221123110.5028/jatm.v8i2.553Design of a Nanosatellite Ground Monitoring and Control Software – a Case StudyFreddy Alexander Díaz González0Pablo Roberto Pinzón Cabrera1Claudio Marcel Hernández Calderón2Universidad Sergio Arboleda – Escuela de Ciencias Exactas e IngenieríaUniversidad Sergio Arboleda – Escuela de Ciencias Exactas e IngenieríaUniversidad Sergio Arboleda – Escuela de Ciencias Exactas e IngenieríaThe growing countries that have carried out the development of CubeSat missions for academic purposes do not offer aerospace engineering programs at their universities. This causes difficulties for traditional engineers upon the formal use of different standards and frameworks for aerospace development, such as the European Cooperation for Space Standardization and Space Mission Analysis and Design . One way in which traditional software engineers can easily understand the structure of an aerospace framework, in order to apply it on the development of CubeSat mission software parts, is comparing its most important elements in relation to the elements suggested by a more familiar method. In this paper, we present a hybrid framework between the ECSS-E-ST-40C standard and the Rational Unified Process, which can be used by traditional software engineers as a guide model for the development of software elements in academic nanosatellite missions. The model integrates the processes and documentation suggested by the ECSS-E-ST-40C with the disciplines, workflows and artifacts suggested in Rational Unified Process. This simplifies the structure of ECSS-E-ST-40C and allows traditional software engineers to easily understand its work elements. The paper describes as study case the implementation of the hybrid model in the analysis and design of ground monitoring and control software for the Libertad-2 satellite mission, which is currently being developed by the Universidad Sergio Arboleda in Colombia.http://www.jatm.com.br/ojs/index.php/jatm/article/view/553CubeSatEuropean Cooperation for Space StandardizationRational Unified ProcessMonitoringGraphical User Interface3D
collection DOAJ
language English
format Article
sources DOAJ
author Freddy Alexander Díaz González
Pablo Roberto Pinzón Cabrera
Claudio Marcel Hernández Calderón
spellingShingle Freddy Alexander Díaz González
Pablo Roberto Pinzón Cabrera
Claudio Marcel Hernández Calderón
Design of a Nanosatellite Ground Monitoring and Control Software – a Case Study
Journal of Aerospace Technology and Management
CubeSat
European Cooperation for Space Standardization
Rational Unified Process
Monitoring
Graphical User Interface
3D
author_facet Freddy Alexander Díaz González
Pablo Roberto Pinzón Cabrera
Claudio Marcel Hernández Calderón
author_sort Freddy Alexander Díaz González
title Design of a Nanosatellite Ground Monitoring and Control Software – a Case Study
title_short Design of a Nanosatellite Ground Monitoring and Control Software – a Case Study
title_full Design of a Nanosatellite Ground Monitoring and Control Software – a Case Study
title_fullStr Design of a Nanosatellite Ground Monitoring and Control Software – a Case Study
title_full_unstemmed Design of a Nanosatellite Ground Monitoring and Control Software – a Case Study
title_sort design of a nanosatellite ground monitoring and control software – a case study
publisher Departamento de Ciência e Tecnologia Aeroespacial
series Journal of Aerospace Technology and Management
issn 1984-9648
2175-9146
publishDate 2016-04-01
description The growing countries that have carried out the development of CubeSat missions for academic purposes do not offer aerospace engineering programs at their universities. This causes difficulties for traditional engineers upon the formal use of different standards and frameworks for aerospace development, such as the European Cooperation for Space Standardization and Space Mission Analysis and Design . One way in which traditional software engineers can easily understand the structure of an aerospace framework, in order to apply it on the development of CubeSat mission software parts, is comparing its most important elements in relation to the elements suggested by a more familiar method. In this paper, we present a hybrid framework between the ECSS-E-ST-40C standard and the Rational Unified Process, which can be used by traditional software engineers as a guide model for the development of software elements in academic nanosatellite missions. The model integrates the processes and documentation suggested by the ECSS-E-ST-40C with the disciplines, workflows and artifacts suggested in Rational Unified Process. This simplifies the structure of ECSS-E-ST-40C and allows traditional software engineers to easily understand its work elements. The paper describes as study case the implementation of the hybrid model in the analysis and design of ground monitoring and control software for the Libertad-2 satellite mission, which is currently being developed by the Universidad Sergio Arboleda in Colombia.
topic CubeSat
European Cooperation for Space Standardization
Rational Unified Process
Monitoring
Graphical User Interface
3D
url http://www.jatm.com.br/ojs/index.php/jatm/article/view/553
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