ADCS Preliminary Design For GNB

Alessio Bocci; Giovanni Mingari Scarpello

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arXiv · 2103.02017

ADCS Preliminary Design For GNB

Alessio Bocci·Giovanni Mingari Scarpello

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Abstract

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.

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Alessio Bocci, Giovanni Mingari Scarpello. 2021-03-02. ADCS Preliminary Design For GNB. https://arxiv.org/abs/2103.02017

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