Özet
Magnetometers are widely used for attitude determination of the low Earth orbit satellites. In order to estimate the satellite attitude accurately, bias of magnetometer must be estimated. In this study a linear Kalman filter based algorithm for estimation of magnetometer biases is proposed. We present computer technology for onboard signal processing and in-flight calibration of a low-cost strap-down inertial navigation system (SINS) for small land-survey satellite. For the system with small financial expenditures on practical implementation, the requirements are not severe on accuracy of the attitude determination. In this situation, we have applied the SINS correction based on signals of a Sun optoelectronic sensor and magnetometer.
Orijinal dil | İngilizce |
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Ana bilgisayar yayını başlığı | Proceedings of the 2014 6th International Conference on Electronics, Computers and Artificial Intelligence, ECAI 2014 |
Yayınlayan | Institute of Electrical and Electronics Engineers Inc. |
Sayfalar | 1-7 |
Sayfa sayısı | 7 |
ISBN (Elektronik) | 9781479954780 |
DOI'lar | |
Yayın durumu | Yayınlandı - 2014 |
Etkinlik | 6th International Conference on Electronics, Computers and Artificial Intelligence, ECAI 2014 - Pitesti, Romania Süre: 23 Eki 2014 → 25 Eki 2014 |
Yayın serisi
Adı | Proceedings of the 2014 6th International Conference on Electronics, Computers and Artificial Intelligence, ECAI 2014 |
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???event.eventtypes.event.conference??? | 6th International Conference on Electronics, Computers and Artificial Intelligence, ECAI 2014 |
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Ülke/Bölge | Romania |
Şehir | Pitesti |
Periyot | 23/10/14 → 25/10/14 |
Bibliyografik not
Publisher Copyright:© 2014 IEEE.