Results of the Nanosatellite Munin Attitude Determination using solar arrays output
A problem of attitude determination of the passive magnetic stabilized nanosatellite Munin using solar array output is considered. The attitude control system consists of a strong permanent magnet and a set of hysteresis rods fabricated from the soft magnetic material treated using a specific technology. Developed software for the nanosatellite attitude determination is given. Results of its verification and attitude motion determination are described.
attitude determination, solar array output, Earth’s Albedo, passive magnetic attitude control system, nanosatellite Munin