Özet
Magnetometers are vital for satellite attitude determination, providing measurements of the Earth's magnetic field to infer orientation. However, accurate attitude estimation requires thorough calibration to correct errors such as bias, scaling factors, and nonorthogonality of the magnetometer axes. This study investigates four magnetometer calibration methods, categorized into batch and real-time techniques, analyzing their performance under two distinct spacecraft states: tumbling and detumbling. Simulated data was used to evaluate the calibration algorithms under varying orbital elements, highlighting their effectiveness in each state. The findings offer valuable insights for selecting robust calibration techniques for precise attitude determination in satellite operations.
| Orijinal dil | İngilizce |
|---|---|
| Ana bilgisayar yayını başlığı | 2025 IEEE International Workshop on Metrology for AeroSpace, MetroAeroSpace 2025 - Proceedings |
| Yayınlayan | Institute of Electrical and Electronics Engineers Inc. |
| Sayfalar | 204-209 |
| Sayfa sayısı | 6 |
| ISBN (Elektronik) | 9798331501525 |
| DOI'lar | |
| Yayın durumu | Yayınlandı - 2025 |
| Etkinlik | 12th IEEE International Workshop on Metrology for AeroSpace, MetroAeroSpace 2025 - Naples, Italy Süre: 18 Haz 2025 → 20 Haz 2025 |
Yayın serisi
| Adı | 2025 IEEE International Workshop on Metrology for AeroSpace, MetroAeroSpace 2025 - Proceedings |
|---|
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| ???event.eventtypes.event.conference??? | 12th IEEE International Workshop on Metrology for AeroSpace, MetroAeroSpace 2025 |
|---|---|
| Ülke/Bölge | Italy |
| Şehir | Naples |
| Periyot | 18/06/25 → 20/06/25 |
Bibliyografik not
Publisher Copyright:© 2025 IEEE.
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