Abstract
-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.
| Original language | English |
|---|---|
| Pages (from-to) | 157-169 |
| Number of pages | 13 |
| Journal | WSEAS Transactions on Systems and Control |
| Volume | 21 |
| DOIs | |
| Publication status | Published - 2026 |
| Externally published | Yes |
Bibliographical note
Publisher Copyright:© 2026, World Scientific and Engineering Academy and Society. All rights reserved.
Keywords
- actuator fault
- normalized innovation
- Q-adaptation
- R-adaptation
- Robust Adaptive Kalman Filter
- sensor fault
- Unmanned Aerial Vehicle
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