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.
Approach to study satellite attitude determination algorithms
Acta Astronautica ; 98 ; 133-137
2014-01-27
5 pages
Article (Journal)
Electronic Resource
English
Approach to study satellite attitude determination algorithms
Online Contents | 2014
|PLANCK ATTITUDE DETERMINATION ALGORITHMS
British Library Conference Proceedings | 2006
|GPS-based attitude determination of gyrostat satellite by quaternion estimation algorithms
Online Contents | 2002
|Analytical study of microsatellite attitude determination algorithms
Online Contents | 2015
|Analytical study of microsatellite attitude determination algorithms
Elsevier | 2015
|