This Thesis presents the design of a ground segment for the GranaSAT-I cubesat, a microsatellite
in development process which will require of a system capable of receiving its
telemetry and sending telecommands when it is launched. The project includes an analysis
of all the physical phenomena and components involved in the transmission of the signal
from an spacecraft in Low Earth Orbit to the station located in the Faculty of Sciences of
the University of Granada. The deployment and testing processes were also carried out and
are described in detail.Proyecto Fin de Carrera de la Univ. de Granada. Departamento de Electrónica y Tecnología de Computadores. Curso 2014-201
