Congresos y publicaciones

En esta sección se incluyen las publicaciones y congresos relativos al MUSE. Además, por su carácter eminentemente docente y su importancia para este programa de Máster, se han incluido publicaciones relacionadas con trabajos de investigación ligados a distintos proyectos de desarrollo espacial (como los satélites UPMSat-2 y Unión/Lian-He), en los que participan profesores y colaboradores del MUSE.


Simple mathematical approach to solar cell/panel behavior based on datasheet information. Renewable Energy; Vol.: 103; pp. 729-738. ISSN 0960-1481.

The UPMSat-2 Satellite: an academic project within aerospace engineering education. 2nd Annual International Conference on Engineering Education & Teaching.  5-8 Jun 2017, Athens, Greece.



MUSE (Master in Space Systems), an advanced master’s degree in space engineering. 1st Annual International Conference on Engineering Education & Teaching. 9-12 May 2016, Athens, Greece.



Using Internet-based technologies in a university satellite project. IFAC Workshop on Internet Based Control Education (IBCE15), 4-6 November 2015, Brescia, Italy.

Ada, the programming language of choice for the UPMSAT-2 satellite. Data Systems In Aerospace (DASIA 2015), 19-21 May 2015. Proceedings of DASIA 2015 : DAta Systems In Aerospace. Vol.: 732.

Schedulability analysis of PWM tasks for the UPMSat-2 ADCS. Reliable Software Technologies — Ada-Europe 2015, LNCS 9111, pp. 85--99. Springer-Verlag, 2013. ISBN ISBN 978-3-319-19584-1.

Magnetic Attitude Control for Satellites in Polar or Sun-Synchronous Orbits. Journal of Guidance, Control And Dynamics; Vol: 38 (10); pp. 1-12. ISSN 0731-5090.

Analytical models for the power subsystem and the attitude control subsystem of a microsatellite. Tesis (Doctoral).

Magnetic Attitude Control System for a Small Satellite. Impact on the Thermal Performance. Tesis (Doctoral).



Experience in spacecraft on-board software development. Ada User Journal, v. 35 (n. 1); pp. 1-6. ISSN 1381-6551.

Explicit Expressions for Solar Panel Equivalent Circuit Parameters Based on Analytical Formulation and the Lambert W-Function. Energies; Vol.: 7; pp. 4098-4115. ISSN 1996-1073.

On the analytical approach for modeling photovoltaic systems behavior. Journal of Power Sources; Vol.: 247; pp. 467-474. ISSN 0378-7753.

Multidisciplinary Design Optimization Application to Conceptual Design of University-class Microsatellite Projects. Tesis (Doctoral).



Static analysis of WCET in a satellite software subsystem. 3th International Workshop on Worst-Case Execution Time Analysis, 9-12 July 2013, Paris, France.

Arquitectura de tiempo real para el control de actitud en un satélite experimental. XXIV Jornadas de Automática, 4-6 Septiembre 2013, Terrasa, Barcelona, España.

New method for analytical photovoltaic parameters identification: meeting manufacturer’s datasheet for different ambient conditions. International Congress on Energy Effciency and Energy Related Materials, 9-12 Oct 2013, Anatlya, Turkey. ISBN 978-3-319-05520.

New method for analytical photovoltaic parameter extraction. International Conference on Renewable Energy Research and Applications (ICRERA), 20-23 Oct 2013, Madrid.

Efficiency of hysteresis rods in small spacecraft attitude stabilization. The Scientific World Journal; Vol.: 2013; ISSN 2356-6140.

System Engineering Approach to Initial Design of LEO Remote Sensing Missions. 6th International Conference on Recent Advances in Space Technologies (RAST 2013), 12-14 Jun 2013, Istambul, Turkey. ISBN 978-1-4673-6395-2.

Vibrations loads in the process of designing scientific spacecraft payloads. 11th International Conference on Vibration Problems, 09/09/2013 - 12/09/2013, Lisboa (Portugal)



Multiobjective optimization applied to structural sizing of low cost university-class microsatellite projects. Acta Astronautica; Vol.: 79; pp. 212-220. ISSN 0094-5765.

Diseño preliminar térmico y estructural del instrumento NOMAD de ExoMars. XIX CONGRESO NACIONAL DE INGENIERÍA MECÁNICA, 14/11/2012 - 16/11/2012, Castellón, España

Linear Approach to the Orbiting Spacecraft Thermal Problem. Journal of Thermophysics and Heat Transfer, v. 26 (n. 3); pp. 511-522. ISSN 0887-8722



Diseño térmico preliminar del Instrumento PHI de Solar Orbiter. VII Congreso Nacional de Ingeniería Termodinámica - CNIT7, 15/06/2011 - 17/06/2011, Bilbao, España. ISBN 84-95416-79-4

Thermal behaviour of Sunrise, a balloon-borne solar Telescope. 20th Symposium on European Rocket and Balloon Programmes and Related Research, 22/05/2011 - 26/05/2011, Noordwijk, The Netherlands



Nonlinear analysis of a simple model of temperature evolution in a satellite. Nonlynear Dynamics, v. 58 ; pp. 405-419. ISSN 0924-090X