Özet
In the paper an algorithm on aiding the Inertial Navigation System with GPS is presented. Federated Kalman filter, which includes two different Kalman filters and processes INS and GPS data in real time, is designed for this reason. Simulation is made and presented on flight dynamics, and it is determined that the algorithm for aiding the INS with GPS, evaluates the motion parameters with high accuracy.
| Orijinal dil | İngilizce |
|---|---|
| Ana bilgisayar yayını başlığı | RAST 2003 - Proceedings of International Conference on Recent Advances in Space Technologies |
| Editörler | S. Kurnaz, Fuat Ince, S. Onbasioglu |
| Yayınlayan | Institute of Electrical and Electronics Engineers Inc. |
| Sayfalar | 569-574 |
| Sayfa sayısı | 6 |
| ISBN (Elektronik) | 0780381424, 9780780381421 |
| DOI'lar | |
| Yayın durumu | Yayınlandı - 2003 |
| Etkinlik | International Conference on Recent Advances in Space Technologies, RAST 2003 - Istanbul, Türkiye Süre: 20 Kas 2003 → 22 Kas 2003 |
Yayın serisi
| Adı | RAST 2003 - Proceedings of International Conference on Recent Advances in Space Technologies |
|---|
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| ???event.eventtypes.event.conference??? | International Conference on Recent Advances in Space Technologies, RAST 2003 |
|---|---|
| Ülke/Bölge | Türkiye |
| Şehir | Istanbul |
| Periyot | 20/11/03 → 22/11/03 |
Bibliyografik not
Publisher Copyright:© 2003 IEEE.
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