Análisis de los modos de fallo del sistema de gestión de energía de un Cubesat
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Date
Subject
CubeSat
Energía
Paneles fotovoltaicos
nanosatélites
potencia eléctrica
Matlab
Gestión Energética
CubeSat
energy
photovoltaic panels
nanosatellites
electrical power
electrical energy
MATLAB
energy management
Energía
Paneles fotovoltaicos
nanosatélites
potencia eléctrica
Matlab
Gestión Energética
CubeSat
energy
photovoltaic panels
nanosatellites
electrical power
electrical energy
MATLAB
energy management
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Journal Title
Journal ISSN
Volume Title
Publisher
Instituto Tecnológico de Santo Domingo (INTEC)
Un satélite es un dispositivo que se sitúa en órbita alrededor de la Tierra con fines científicos, militares, educacionales o de comunicaciones. Se pueden clasificar según su peso como: satélites grandes, que pesan más de 1,000 kilogramos (kg), satélites medianos, que pesan entre 500-1,000 kg, y satélites pequeños, que pesan menos de 500 kg. Dentro de los satélites pequeños se encuentran los nanosatélites, los cuales pesan entre 1-10 kg. La principal ventaja que poseen los nanosatélites es que son capaces de realizar misiones complejas a un menor costo. Dentro de las limitaciones que estos presentan es que tienen poca capacidad para captar y almacenar energía debido a su tamaño. Considerando la importancia del sistema de energía durante el funcionamiento de los satélites, este artículo analiza los modos de fallos que se presentan en el sistema y cómo estos afectan a los sistemas de generación y almacenamiento de energía. Para la simulación de estos sistemas se determinaron la cantidad mínima de paneles solares y baterías necesarios para su correcto funcionamiento. Los resultados obtenidos muestran que con este análisis se logra dimensionar correctamente el sistema de gestión de energía, reduciendo el tamaño de estos y a su vez el peso dentro del satélite.
A satellite is a device that is placed in orbit around the earth for scientific, military, educational, or communications purposes. They can be classified according to their weight as: large satellites weighing more than 1,000 kilograms (kg), medium satellites weighing between 500-1000 kg, and small satellites, weighing less than 500 kg. Within the small satellites are the nanosatellites, which weigh between 1-10 kg. The main advantage of nanosatellites is that they are capable of performing complex missions at a lower cost. Among the limitations that this present is that they have little capacity to capture and store energy due to their size. Considering the importance of the power system during the operation of satellites, this article analyzes the failure modes that occur in the system and how these affect energy generation and storage systems. For the simulation of these systems the minimum number of solar panels and batteries necessary for their correct operation was determined. The results obtained show that with this analysis it is possible to correctly size the energy management system, reducing the size of these and in turn the weight within the satellite.
A satellite is a device that is placed in orbit around the earth for scientific, military, educational, or communications purposes. They can be classified according to their weight as: large satellites weighing more than 1,000 kilograms (kg), medium satellites weighing between 500-1000 kg, and small satellites, weighing less than 500 kg. Within the small satellites are the nanosatellites, which weigh between 1-10 kg. The main advantage of nanosatellites is that they are capable of performing complex missions at a lower cost. Among the limitations that this present is that they have little capacity to capture and store energy due to their size. Considering the importance of the power system during the operation of satellites, this article analyzes the failure modes that occur in the system and how these affect energy generation and storage systems. For the simulation of these systems the minimum number of solar panels and batteries necessary for their correct operation was determined. The results obtained show that with this analysis it is possible to correctly size the energy management system, reducing the size of these and in turn the weight within the satellite.
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info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
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info:eu-repo/semantics/publishedVersion
Art.
Source
Science, Engineering and Applications; Vol. 4 No. 2 (2021): Science, Engineering and Applications; 5-20
Ciencia, Ingenierías y Aplicaciones; Vol. 4 Núm. 2 (2021): Ciencia, Ingenierías y Aplicaciones; 5-20
2636-2171
2636-218X
10.22206/cyap.2021.v4i2
Ciencia, Ingenierías y Aplicaciones; Vol. 4 Núm. 2 (2021): Ciencia, Ingenierías y Aplicaciones; 5-20
2636-2171
2636-218X
10.22206/cyap.2021.v4i2