Study of the Microsatellites Attitude Determination Method of and Its Verification
Kalman filter study method is proposed. Application of the method is demonstrated on the satellite attitude determination algorithm based on the Sun-sensor and magnetometer measurements. The method was used to study the microsatellite Chibis-M attitude determination algorithm. The Chibis-M microsatellite attitude determination results are shown using in-flight measurements.
attitude determination, Kalman filter, method of accuracy study