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|Title:||Fault-Tolerant Flight Tracking Control with Stuck Faults||Authors:||Yang, G.-H.
H∞ robust design
Linear matrix inequality
|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||URI:||http://scholarbank.nus.edu.sg/handle/10635/111571||ISSN:||07431619|
|Appears in Collections:||Staff Publications|
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