The Design and Implementation of the UPMSAT-2 Attitude Control System * *This work has been partially funded by the Spanish National R&D&I plan (projects M2C2, TIN2014-56158-C4-3-P).-Reference-Cited by-同舟云学术

The Design and Implementation of the UPMSAT-2 Attitude Control System * *This work has been partially funded by the Spanish National R&D&I plan (projects M2C2, TIN2014-56158-C4-3-P).

Published:2017-07 Issue:1 Volume:50 Page:11245-11250
ISSN:2405-8963
Container-title:IFAC-PapersOnLine
language:en
Short-container-title:IFAC-PapersOnLine

Author:

Zamorano Juan,Garrido Jorge,Cubas Javier,Alonso Alejandro,de la Puente Juan A.

Publisher

Elsevier BV

Subject

Control and Systems Engineering

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2. ARM05 (2007). ISO/IEC 8652:1995(E)/TC1 (2000)/AMD1 (2007): Information Technology — Programming Languages — Ada.

3. Cubas, J. (2015). Analytical models for the power subsystem and the attitude control subsystem of a microsatel-lite. Ph.D. thesis, Universidad Politécnica de Madrid.

4. Magnetic attitude control for satellites in polar or sun-synchronous orbits;Cubas;Journal of Guidance, Control, and Dynamics,2015

5. Model-driven design of real-time software for an experimental satellite;de la Puente;IFAC Proceedings,2014

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2. Optimization of Geomagnetic and Solar Reference Vector Algorithms for Micro-Nano Satellites;Journal of Physics: Conference Series;2022-03-01

3. An Embedded Systems Laboratory for Aerospace Students;IFAC-PapersOnLine;2020

4. A generalized control law for uniform, global and exponential magnetic detumbling of rigid spacecraft;IFAC-PapersOnLine;2020

5. Timing Analysis of the UPMSat-2 Communications Subsystem ⁎ ⁎This work has been partially funded by the Spanish National R&D&I plan (project M2C2, TIN2014-56158-C4-3-P).;IFAC-PapersOnLine;2018