The laboratory platform for achieving the positioning of the satellite in the orbital magnetic field

Abstract

The research/testing of nano-microsatellite attitudes with simulation satellite attitude in orbital conditions is a current issue, especially for nanosatellites, the attitude control of which is done with reaction wheels and magnetorquers. The proposed installation includes 2 simulators: - for experimental research in laboratory the kinematic and dynamic of nano-microsatellites with spherical space movement with a fixed point; - for experimental research of the dynamic attitude of the satellite in the simulated geomagnetic field.