Geomagnetic models at low earth orbit and their use in attitude determination

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5 Atıf (Scopus)

Özet

In this study, three geomagnetic field models, T89, CHAOS-6 and IGRF-12 models are compared at LEO orbit altitudes with the satellite observations. Comparisons between the models and with the observations are made using the total magnetic field and the components during the geomagnetically disturbed and quiet times. Main interest is to see how the angle between the modelled and observed magnetic field vectors changes. The differences are important since satellite's attitude determination system strongly depends on the angle. Effects of geomagnetic activity on the angle is investigated using geomagnetic activity index and the position of the satellite which are inputs to the models. Comparisons are made between the models using root mean square error analysis. Differences between the model magnetic fields and those of observed are seen to increase when the geomagnetic activity occurs. We discuss the implications of these differences on the satellite attitude determination system.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıProceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017
EditörlerM.F. Unal, A. Hacioglu, M.S. Yildiz, O. Altan, M. Yorukoglu
YayınlayanInstitute of Electrical and Electronics Engineers Inc.
Sayfalar301-305
Sayfa sayısı5
ISBN (Elektronik)9781538616031
DOI'lar
Yayın durumuYayınlandı - 4 Ağu 2017
Etkinlik8th International Conference on Recent Advances in Space Technologies, RAST 2017 - Istanbul, Turkey
Süre: 19 Haz 201722 Haz 2017

Yayın serisi

AdıProceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017

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???event.eventtypes.event.conference???8th International Conference on Recent Advances in Space Technologies, RAST 2017
Ülke/BölgeTurkey
ŞehirIstanbul
Periyot19/06/1722/06/17

Bibliyografik not

Publisher Copyright:
© 2017 IEEE.

Finansman

ACKNOWLEDGMENTS This work is supported in part by TUBITAK Project, 113E595. The authors communicated with Chris Finlay about the CHAOS model, we thank him for clarifying all of the issues. We also thank Nikolai Tsyganenko for his kind advice and sharing the most updated version of his model. The spacecraft data have been obtained from NASA’s public website CDAWeb (cdaweb.nasa.gov). We thank for the data providers.

FinansörlerFinansör numarası
TUBITAK Project113E595

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