Implementation Features of Attitude Determination Algorithm for the SamSat-ION Nanosatellite

Implementation features of attitude determination algorithm of the SamSat-ION nanosatellite are considered. Nanosatellite attitude is estimated via deterministic approach and Kalman filter. The set of magnetometers and light sensors is used as a source of measurement information. The performance of algorithms on the onboard computer of the SamSat-ION nanosatellite is presented.