Analysis and Implementation of an Orbital Orientation Controlsystem for a Pico-Satellite

This project presents the development of a stabilization and orientation system for the space vehicle in orbit that allows obtaining the adequate orientation to establish communication with the ground station. This requirement is achieved through the implementation of a joint actuator and sensor system for the acquisition, reacquisition and reorientation of the satellite. Taking into account that the proposal establishes the use of a triaxial gyroscope as an actuator, as well as the implementation of solar sensors located in each of the faces of the pico-satellite. Allowing fast actions and the use of little memory in the main program.