Decentralized Control of Nanosatellite Tetrahedral Formation Flying Using Aerodynamic Forces

نویسندگان

چکیده

A decentralized control algorithm for the construction of a tetrahedral configuration using differential lift and drag forces is proposed in this paper. Four 3U CubeSats launched LEO are considered. Satellite attitude-controlled motion relative to incoming airflow provides required order change translational motion. The developed allows one track reference trajectories satellites at vertices tetrahedron shape size. influence initial launch conditions on controlled studied

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ژورنال

عنوان ژورنال: Aerospace

سال: 2021

ISSN: ['2226-4310']

DOI: https://doi.org/10.3390/aerospace8080199