This work deals with an ADCS model for a satellite orbiting around Earth. The object is to achieve a preliminary design and perform some analysis on it. To do so, a GNB was selected and main properties are exploited. Previous works of [9], [13], [14], [15] and [17] were analyzed and a synthesis was obtained; then a suitable control system was designed to satisfy technical requirements. Coding was performed using Matlab and Simulink. Keywords: Attitude Determination, Attitude Control, Nanosatellite, Orbital Perturbations, Quaternion, Two Body Problem, Euler's Equations, Lyapunov Function.
@article{arxiv.2103.02017,
title = {ADCS Preliminary Design For GNB},
author = {Alessio Bocci and Giovanni Mingari Scarpello},
journal= {arXiv preprint arXiv:2103.02017},
year = {2021}
}