Özet
A reconfigurable unscented Kalman filter (UKF)-based estimation algorithm for magnetometer biases and scale factors is proposed as a part of the attitude estimation scheme of a pico satellite. Unlike existing algorithms, in this paper, scale factors are not treated, together with other parameters, as part of the state vector; they are estimated separately. After satisfying the conditions of the proposed stopping rule for bias estimation, UKF reconfigures itself for estimation of attitude parameters alone.
| Orijinal dil | İngilizce |
|---|---|
| Makale numarası | 6237612 |
| Sayfa (başlangıç-bitiş) | 2614-2627 |
| Sayfa sayısı | 14 |
| Dergi | IEEE Transactions on Aerospace and Electronic Systems |
| Hacim | 48 |
| Basın numarası | 3 |
| DOI'lar | |
| Yayın durumu | Yayınlandı - 2012 |
Finansman
We thank Sir Christopher White, Bt., for his helps during the grammatical review process of the paper. This work was supported in part by The Scientific and Technological Research Council of Turkey under Grant No. 108M523.
| Finansörler | Finansör numarası |
|---|---|
| Türkiye Bilimsel ve Teknolojik Araştirma Kurumu | 108M523 |
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