UKF for the identification of the pico satellite attitude dynamics parameters and the external torques on IMU and magnetometer measurements

Halil Ersin Söken, Chingiz Hajiyev

Araştırma sonucu: ???type-name???Konferans katkısıbilirkişi

11 Atıf (Scopus)

Özet

In this study, an Unscented Kalman Filter (UKF) algorithm, which integrates mathematical model of the attitude dynamics with the measurements of Inertial Measurement Unit (IMU) and the magnetometers, is designed. The identified vector is arranged from the Euler angles, angular rates, and the unknown constant components of the external torques (the gravity-gradient, magnetic field pressure and the sun radiation) acting on the pico satellite. Because of the inherent nonlinear dynamics and the nonlinear measurement model caused by the magnetometer measurements, UKF is selected as a filter algorithm. Performance of the proposed algorithm is demonstrated via simulations for a cube pico satellite.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıRAST 2009 - Proceedings of 4th International Conference on Recent Advances Space Technologies
Sayfalar547-552
Sayfa sayısı6
DOI'lar
Yayın durumuYayınlandı - 2009
Etkinlik4th International Conference on Recent Advances in Space Technologies 2009, RAST '09 - Istanbul, Turkey
Süre: 11 Haz 200913 Haz 2009

Yayın serisi

AdıRAST 2009 - Proceedings of 4th International Conference on Recent Advances Space Technologies

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???event.eventtypes.event.conference???4th International Conference on Recent Advances in Space Technologies 2009, RAST '09
Ülke/BölgeTurkey
ŞehirIstanbul
Periyot11/06/0913/06/09

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