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Adaptive Fault-Tolerant Tracking Control Against Actuator Faults With Application to Flight Control

Ye, D., Yang, G.-H.·2006·IEEE Transactions on Control Systems Technology

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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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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CoChat. (2026). Citation check: Adaptive Fault-Tolerant Tracking Control Against Actuator Faults With Application to Flight Control. https://app.cochat.ai/papers/10.1109/tcst.2006.883191
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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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Contains information from the Semantic Scholar Academic Graph Datasets, made available under the ODC Attribution License (ODC-BY 1.0).

Semantic Scholar’s data is described in: Kinney, R., et al. (2023). The Semantic Scholar Open Data Platform. arXiv:2301.10140.