Published in Proceedings of the 2003 IEEE Conference on Control Applications, Volume 2, June 23, 2003, pages 1372-1374.
The definitive version is available at https://doi.org/10.1109/CCA.2003.1223212.
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.
Electrical and Computer Engineering
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