Abstract The Kalman filter accuracy study method is proposed. Application of the method is demonstrated by a satellite attitude determination algorithm which uses sun-sensor and magnetometer measurements. The algorithm was implemented on board of a microsatellite Chibis-M. The attitude determination algorithm study method validated using in-flight measurements.

    Highlights Approach to the study of Kalman filter features is proposed. The approach is applied to study Chibis-M attitude determination algorithm. Calculated accuracy of Kalman filter is compared with in-flight results.


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    Title :

    Approach to study satellite attitude determination algorithms


    Contributors:

    Published in:

    Acta Astronautica ; 98 ; 133-137


    Publication date :

    2014-01-27


    Size :

    5 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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