Özet
-A new fault-tolerant estimating approach for unmanned aerial vehicle (UAV) dynamics in the presence of sensor/actuator faults is proposed, which is both adaptive and robust. This study discusses how to choose between adaptive and robust approaches when a sensor or actuator fails. We provide an adaptive method with Q-adaptation as well as a robust method with R-adaptation. The Kalman filter detects faults using the chi-square distribution of the normalized quadratic innovation function (NQI). After detecting a fault, it is recommended to run both R-adaptive and Q-adaptive Kalman filters concurrently and compare their estimation capabilities to distinguish between sensor and actuator faults. As a performance criterion, the mean-squared residuals between estimation and extrapolation values of robust and adaptive filters are proposed.
| Orijinal dil | İngilizce |
|---|---|
| Sayfa (başlangıç-bitiş) | 157-169 |
| Sayfa sayısı | 13 |
| Dergi | WSEAS Transactions on Systems and Control |
| Hacim | 21 |
| DOI'lar | |
| Yayın durumu | Yayınlandı - 2026 |
| Harici olarak yayınlandı | Evet |
Bibliyografik not
Publisher Copyright:© 2026, World Scientific and Engineering Academy and Society. All rights reserved.
Parmak izi
Robust Adaptive Kalman Filter against Sensor/Actuator Faults' araştırma başlıklarına git. Birlikte benzersiz bir parmak izi oluştururlar.Alıntı Yap
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver