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An adaptive fault-tolerant flight controller combining linear matrix inequality (LMI) and adaptive methods can optimize tracking performance and mitigate actuator faults without requiring a separate fault detection and isolation (FDI) mechanism. Novelty: ClaimNovelty.METHODOLOGICAL. Consensus alignment: ConsensusAlignment.NEUTRAL.

October 18, 2006

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

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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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Cite This Study

Ye et al. (Wed,) studied this question.

synapsesocial.com/papers/6a1cf2ac80c583248385e54d https://doi.org/https://doi.org/10.1109/tcst.2006.883191

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