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|Title:||Adaptive fault-tolerant tracking control against actuator faults with application to flight control||Authors:||Ye, D.
Linear matrix inequality (LMI)
|Issue Date:||Nov-2006||Citation:||Ye, D., Yang, G.-H. (2006-11). Adaptive fault-tolerant tracking control against actuator faults with application to flight control. IEEE Transactions on Control Systems Technology 14 (6) : 1088-1096. ScholarBank@NUS Repository. https://doi.org/10.1109/TCST.2006.883191||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. © 2006 IEEE.||Source Title:||IEEE Transactions on Control Systems Technology||URI:||http://scholarbank.nus.edu.sg/handle/10635/115573||ISSN:||10636536||DOI:||10.1109/TCST.2006.883191|
|Appears in Collections:||Staff Publications|
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