Design and first simulations of the TASEC-Lab power subsystem

Marín Coca, Sergio and González Barcena, D. and Roibás-Millán, Elena and Pindado Carrion, Santiago (2021). Design and first simulations of the TASEC-Lab power subsystem. "Journal of Physics: Conference Series", v. 2090 ; ISSN 1742-6596. https://doi.org/10.1088/1742-6596/2090/1/012111.

Description

Title: Design and first simulations of the TASEC-Lab power subsystem
Author/s:
  • Marín Coca, Sergio
  • González Barcena, D.
  • Roibás-Millán, Elena
  • Pindado Carrion, Santiago
Item Type: Article
Título de Revista/Publicación: Journal of Physics: Conference Series
Date: 2021
ISSN: 1742-6596
Volume: 2090
Subjects:
Faculty: Instituto de Microgravedad Ignacio Da Riva (UPM)
Department: Aeronaves y Vehículos Espaciales
UPM's Research Group: Desarrollo y Ensayos Aeroespaciales DEA
Creative Commons Licenses: Recognition - No derivative works - Non commercial

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Abstract

This paper describes the modelling and simulation of the Electrical Power Subsystem (EPS) of the Thermal Analysis Support and Environment Characterization Laboratory (TASEC-Lab). TASEC-Lab is a university experiment on board a sub-orbital platform. It is designed to measure the convection heat transfer in high-altitude balloon missions. The EPS provides, regulates, and distributes electric power to the different systems, parts, and sensors that compose the TASEC-Lab (e.g., On Board Computer (OBC), temperature and pressure sensors, cup anemometer, GPS, heaters...). It mainly consists of a Li-ion battery and two DC-DC converters, and they have been characterized by conducting laboratory tests and fitting to experimental data. A real power consumption profile of the first TASEC-Lab’s mission (designed by Universidad Politécnica de Madrid) is used as input to simulate the EPS. The mathematical model is validated by comparison with experimental results.

More information

Item ID: 69269
DC Identifier: https://oa.upm.es/69269/
OAI Identifier: oai:oa.upm.es:69269
DOI: 10.1088/1742-6596/2090/1/012111
Official URL: https://iopscience.iop.org/article/10.1088/1742-6596/2090/1/012111
Deposited by: Biblioteca ETSI Aeronauticos
Deposited on: 14 Dec 2021 15:17
Last Modified: 26 Apr 2022 15:54
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