@inproceedings{2ae4f8cc0cdf44948e9973a29e5c9c26,
title = "Fault diagnosis and reconfigurable control for flight control systems with actuator failures",
abstract = "In this paper we develop some fault diagnosis and reconfigurable control design techniques with possibly actuator failures for a special class of dynamic systems in which the full system states are reliably measurable and available for feedback and diagnosis. This class of dynamical systems is quite common in modern flight control systems. We have developed an analytic method for the detection and isolation of the actuator faults. We then further develop a robust reconfigurable state feedback controller design technique that guarantees stability and closed-loop performance under the actuator faults. A Boeing 747 model is used to demonstrate the design techniques.",
author = "Kemin Zhou and Rachinayani, \{Phalguna K.\} and Nike Liu and Zhang Ren and Jorge Aravena",
year = "2004",
doi = "10.1109/CDC.2004.1429644",
language = "英语",
isbn = "0780386825",
series = "Proceedings of the IEEE Conference on Decision and Control",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "5266--5271",
booktitle = "2004 43rd IEEE Conference on Decision and Control (CDC)",
address = "美国",
note = "43rd IEEE Conference on Decision and Control, CDC 2004 ; Conference date: 14-12-2004 Through 17-12-2004",
}