Özet
An adaptive integrated navigation system, consisting of barometric altimeter (Baro) and GPS, is presented. The integration is achieved by using an adaptive data fusion algorithm with the filter gain correction. Proposed adaptive data fusion algorithm utilizes the measurement noise scale factor in order to reduce the effects of the incorrect barometric altimeter measurements on the estimation procedure. By using the algorithm, incorrect baro measurements are corrected by the system without any impact on the good estimation behavior. Performance of the proposed Baro/GPS integrated system is examined by simulations for altitude estimation of an aircraft.
| Orijinal dil | İngilizce |
|---|---|
| Sayfa (başlangıç-bitiş) | 2-14 |
| Sayfa sayısı | 13 |
| Dergi | International Journal of Adaptive Control and Signal Processing |
| Hacim | 35 |
| Basın numarası | 1 |
| DOI'lar | |
| Yayın durumu | Yayınlandı - Oca 2021 |
Bibliyografik not
Publisher Copyright:© 2020 John Wiley & Sons Ltd.
Finansman
This research is part of the project numbered with TM3061 which is fully financed by Turkish Aerospace Inc. In order to learn for more details about the project, please apply/refer to Turkish Aerospace Inc. information Turkish Aerospace Inc, TM3061This research is part of the project numbered with TM3061 which is fully financed by Turkish Aerospace Inc. In order to learn for more details about the project, please apply/refer to Turkish Aerospace Inc.
| Finansörler | Finansör numarası |
|---|---|
| Turkish Aerospace Inc | TM3061 |
| Turkish Aerospace Inc. |
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