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Assessment of magnetic storm effects under various magnetometer noise levels for satellite attitude estimation

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde BölümKonferans katkısıbilirkişi

6 Atıf (Scopus)

Özet

In this study, external magnetic fields measured by the magnetometer sensors are considered. For low-Earth orbiting (LEO) satellites, there are variety of magnetometers available off-the-shelf commercially. Their noise levels differ based on the mission goals of the satellites and technological advances. Earth's geomagnetic field predicted by the geomagnetic field models is used for satellite attitude control. Any deviations from the model fields, caused by the external sources such as magnetic storms, are treated as magnetometer noise or bias. This may prevent the determination of the magnitude of the effects from the external sources correctly. This study aims to reveal the magnitude of the geomagnetic field variations due to the magnetospheric storms obscured by the magnetometer noise level used in the attitude control systems by implementing a range of magnetometer sensor noise levels on the simulation of the satellite's rotational motion for the selected geomagnetic storm events.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıProceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019
EditörlerS. Menekay, O. Cetin, O. Alparslan
YayınlayanInstitute of Electrical and Electronics Engineers Inc.
Sayfalar769-773
Sayfa sayısı5
ISBN (Elektronik)9781538694480
DOI'lar
Yayın durumuYayınlandı - Haz 2019
Etkinlik9th International Conference on Recent Advances in Space Technologies, RAST 2019 - Istanbul, Türkiye
Süre: 11 Haz 201914 Haz 2019

Yayın serisi

AdıProceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019

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???event.eventtypes.event.conference???9th International Conference on Recent Advances in Space Technologies, RAST 2019
Ülke/BölgeTürkiye
ŞehirIstanbul
Periyot11/06/1914/06/19

Bibliyografik not

Publisher Copyright:
© 2019 IEEE.

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