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Adaptive Fault-Tolerant Tracking Control Against Actuator Faults With Application to Flight Control
Abstract
This paper deals with the problem of flight tracking control against actuator faults using the linear matrix inequality (LMI) method and adaptive method. An adaptive fault-tolerant flight controller design method is developed based on the online estimation of an eventual fault and the addition of a new control law to the normal control law in order to reduce the fault effect on the system without the need for a fault detection and isolation (FDI) mechanism. In the framework of LMI approach, the normal tracking performance of the resultant closed-loop system is optimized without any conservativeness and the states of fault modes asymptotically track those of the normal mode. A numerical example of an F-16 aircraft model and its simulation results are given
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Cited by
Tong, S., Huo, B., & Li, Y. (2014) · IEEE Transactions on Fuzzy Systems · doi:10.1109/tfuzz.2013.2241770 · Cited by 560
Adaptive Neural Fault-Tolerant Control of a 3-DOF Model Helicopter System
Chen, M., Shi, P., & Lim, C.-C. (2016) · IEEE Transactions on Systems, Man, and Cybernetics: Systems · doi:10.1109/tsmc.2015.2426140 · Cited by 414
Adaptive Fuzzy Finite-Time Control of Nonlinear Systems With Actuator Faults
Wang, H., Liu, P. X., Zhao, X., & Liu, X. (2020) · IEEE Transactions on Cybernetics · doi:10.1109/tcyb.2019.2902868 · Cited by 345
Metadata
- Authors
- Ye, D., & Yang, G.-H.
- Venue
- IEEE Transactions on Control Systems Technology
- Published
- 2006-11
- Volume
- 14
- Issue
- 6
- Pages
- 1088-1096
- ISSN
- 1063-6536 (ISSN-L)
- OpenAlex
- W2119493620
- Cited by
- 506
- References
- 0
- FWCI
- 41.92
- Type
- journal article
- Language
- en
- Open access
- closed
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- Ye, D., & Yang, G.-H. (2006). Adaptive Fault-Tolerant Tracking Control Against Actuator Faults With Application to Flight Control. IEEE Transactions on Control Systems Technology. https://doi.org/10.1109/tcst.2006.883191
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