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UKF-based reconfigurable attitude parameters estimation and magnetometer calibration

  • Halil Ersin Soken*
  • , Chingiz Hajiyev
  • *Bu çalışma için yazışmadan sorumlu yazar
  • The Graduate University for Advanced Studies

Araştırma sonucu: Dergiye katkıMakalebilirkişi

53 Atıf (Scopus)

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 dilİngilizce
Makale numarası6237612
Sayfa (başlangıç-bitiş)2614-2627
Sayfa sayısı14
DergiIEEE Transactions on Aerospace and Electronic Systems
Hacim48
Basın numarası3
DOI'lar
Yayın durumuYayınlandı - 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.

FinansörlerFinansör numarası
Türkiye Bilimsel ve Teknolojik Araştirma Kurumu108M523

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