Modeling the Angular Motion Dynamics of Small Spacecraft with a Magnetic Attitude Control System in a Three-Axis Stabilization Mode
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The problem of modeling the attitude control modes of small spacecraft using electromagnetic systems interacting with the Earth’s magnetic field is considered. A mathematical model for the angular motion dynamics of small spacecraft has been developed. The control law for linear magnetic attitude control systems of small spacecraft is formulated. The results of our numerical modeling of the motion of a satellite with a magnetic attitude control system are presented.
This work was financially supported by the Ministry of Education and Science of the Russian Federation (project RFMEFI57414X0103). The work was supported by a grant from the President of the Russian Federation for State support of young Russian scientists, candidates of science (MK-3869.2019.8).
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