| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1714657 | Acta Astronautica | 2014 | 5 Pages |
Abstract
•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.
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.
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Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Michael Ovchinnikov, Danil Ivanov,