Please use this identifier to cite or link to this item:
https://scholarbank.nus.edu.sg/handle/10635/111571
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 | URI: | http://scholarbank.nus.edu.sg/handle/10635/111571 | ISSN: | 07431619 |
Appears in Collections: | Staff Publications |
Show full item record
Files in This Item:
There are no files associated with this item.
Google ScholarTM
Check
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.