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EKF based spacecraft localization with single station antenna tracking data

  • Istanbul Technical University
  • Samara State Technical University

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde BölümKonferans katkısıbilirkişi

Özet

In this study, an extended Kalman filter (EKF) for estimation of spacecraft's position and velocity by single station antenna tracking data in the presence of singularities is proposed. The designed EKF estimates the position and velocity of the spacecraft on direct nonlinear range-azimuth- elevation measurements. The proposed EKF is examined through the geostationary satellite orbital motion simulations. The corruption in the results by EKF emerges from singularities caused by the highly complex elements of the Jacobian measurement matrix. The recommendations to prevent the mentioned problem are given.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıRAST 2013 - Proceedings of 6th International Conference on Recent Advances in Space Technologies
Sayfalar1115-1120
Sayfa sayısı6
DOI'lar
Yayın durumuYayınlandı - 2013
Etkinlik6th International Conference on Recent Advances in Space Technologies, RAST 2013 - Istanbul, Türkiye
Süre: 12 Haz 201314 Haz 2013

Yayın serisi

AdıRAST 2013 - Proceedings of 6th International Conference on Recent Advances in Space Technologies

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???event.eventtypes.event.conference???6th International Conference on Recent Advances in Space Technologies, RAST 2013
Ülke/BölgeTürkiye
ŞehirIstanbul
Periyot12/06/1314/06/13

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