@misc{10481/53798,
year = {2018},
month = {9},
url = {http://hdl.handle.net/10481/53798},
abstract = {This Bachelor Thesis introduces a Theoretical Description and Simulink
implementation of di erent ADCS (Attitude Determination and Control
System), a fundamental feature of spacecrafts. As it makes possible to
control the orientation and stabilize the satellite within its orbit. Which is
as complex as fascinating. Mathematical Formalism and Physical Model
are presented in order to fully understand this phenomenon and build it
to make it work in Simulink, creating a simulation of a Digital Dynamical
System that would be present at the on board computer of the satellite
GranaSAT-I. In this context, the Aerospace GranaSAT Group at UGR is
building the GranaSAT-I.},
publisher = {Prof. Andrés Roldán Aranda},
keywords = {GranaSAT},
keywords = {ADCS},
keywords = {simulink},
title = {GranaSAT-I: Kinematic and Dynamic Model for Attitude Determination and Control System},
author = {Marchante Arjona, Luis},
}