[HTML][HTML] Design and implementation of a real-time onboard system for a stratospheric balloon mission using commercial off-the-self components and a model-based …

ÁG Pérez-Muñoz, JC Gamazo-Real… - Computers and …, 2023 - Elsevier
Stratospheric balloons have emerged as an affordable and flexible alternative to traditional
spacecrafts as they are implemented using commercial off-the-shelf (COTS) equipment …

[PDF][PDF] Universidad Politécnica de Madrid

UBEH García - Aprendizaje Automático. Redes de Neuronas, 2009 - oa.upm.es
UNIVERSIDAD POLITÉCNICA DE MADRID Page 1 FACULTAD DE INFORMÁTICA
UNIVERSIDAD POLITÉCNICA DE MADRID UNIVERSIDAD POLITÉCNICA DE MADRID …

[HTML][HTML] On-orbit performance analysis of spinning spacecraft magnetic control laws. Application to the UPMSat-2 mission

A Porras-Hermoso, J Piqueras, J Cubas… - Measurement, 2024 - Elsevier
This paper studies the performance of a new magnetic attitude control law developed for the
UPMSat-2 satellite. The UPMSat-2 control law, which is a modification of the B-dot, allows …

Numerical results of modal coupling in the UPMSat-2 structure

A García Pérez, M Chimeno Manguan… - 2019 - oa.upm.es
This work presents a study of the effects of modal coupling on the microsatellite UPMSat-2,
where some design parameters are modified to achieve different levels of modal coupling …

On the UPMSat-2 attitude, control and determination subsystem's design

E Rodríguez-Rojo, J Cubas Cano, E Roibás Millán… - 2019 - oa.upm.es
In the present paper the work carried out in relation to the Attitude, Control and
Determination Subsystem (ACDS) of the UPMSat-2 is summarized. This engineering project …

UPMSat-2 Micro-satellite: In-orbit technological demonstration for education and science

E Roibás-Millán, J Pérez-Álvarez, S Pindado, J Cubas… - 2021 - digitalcommons.usu.edu
The UPMSat-2 micro-satellite was launched on September the 3rd 2020 at 01: 51: 10 UTC
from Kourou spaceport in French Guyana. The VV16 Vega Flight has been the first low Earth …

A generalized control law for uniform, global and exponential magnetic detumbling of rigid spacecraft

N Petit, I Sarras - IFAC-PapersOnLine, 2020 - Elsevier
The problem of magnetic detumbling, also known as magnetic momentum unloading, is
considered. The objective is to stabilize a rigid spacecraft angular velocity to zero only …

Timing Analysis of the UPMSat-2 Communications Subsystem

J Garrido, J Zamorano, A Alonso, JA de la Puente - IFAC-PapersOnLine, 2018 - Elsevier
Communication between satellites and ground stations is a critical element of all satellite
missions. Limitations in bandwidth and coverage may restrict the capability of ground …

The UPMQube: an academic/educational PocketQube proposal for the EU2Space Challenge

E Roibás Millán, JM Álvarez Romero… - Athens Journal of …, 2023 - oa.upm.es
In the present paper, the UPMQube PocketQube proposal for the EU2Space challenge is
described. This proposal has been developed by a group of master's degree students led by …

Optimization of Geomagnetic and Solar Reference Vector Algorithms for Micro-Nano Satellites

J Ye, G **a, X Yu, X Zhong, X Hu, L Pu… - Journal of Physics …, 2022 - iopscience.iop.org
To optimize the geomagnetic reference vector and the solar reference vector calculation
method, this paper proposes a geomagnetic fitting algorithm and simplifies the DE430 …