GranaSAT-I: Kinematic and Dynamic Model for Attitude Determination and Control System

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.