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Title: Fault-Tolerant Flight Tracking Control with Stuck Faults
Authors: Yang, G.-H. 
Lum, K.-Y. 
Keywords: Fault-tolerant control
Flight control
H∞ robust design
Linear matrix inequality
Peak-to-peak gain
Stuck faults
Issue Date: 2003
Citation: Yang, G.-H.,Lum, K.-Y. (2003). Fault-Tolerant Flight Tracking Control with Stuck Faults. Proceedings of the American Control Conference 1 : 521-526. ScholarBank@NUS Repository.
Abstract: This paper is concerned with the problem of flight tracking control in the presence of stuck-actuator faults. A stuck fault is modeled as a bounded input, and its effect on the closed-loop system is described by a peak-to-peak gain. A fault-tolerant flight controller design method is developed based on the H ∞ and peak-to-peak gain performance indexes in a multiobjective optimization setting, and the proposed iterative LMI-based algorithm is shown to have some convergence properties. The design is such that the nominal performance of the resultant closed-loop system is optimized subject to the requirement that all the closed-loop systems corresponding to different fault modes have acceptable performances.
Source Title: Proceedings of the American Control Conference
ISSN: 07431619
Appears in Collections:Staff Publications

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