Recommended Citation
Published in Proceedings of the 2003 IEEE Conference on Control Applications, Volume 2, June 23, 2003, pages 1372-1374.
Copyright © 2003 IEEE. Personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution to servers or lists, or to reuse any copyrighted component of this work in other works must be obtained from the IEEE. The definitive version is available online at: http://dx.doi.org/10.1109/CCA.2003.1223212.
Abstract
A fault-tolerant system is the one that can continue its operation without significant impact on performance in the presence of hardware and/or software errors. In this paper, the design of a fault-tolerant flight controller to control UH-60 helicopter is investigated. A 9th-order state space representation of the helicopter model operating at the forward mode with 80 knots is presented; then a fault-tolerant optimal feedback controller is designed and tested.
Disciplines
Electrical and Computer Engineering
URL: http://digitalcommons.calpoly.edu/eeng_fac/112