Please use this identifier to cite or link to this item: https://hdl.handle.net/2440/83469
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Type: Journal article
Title: Adaptive reconfiguration scheme for flight control systems
Author: Jiang, B.
Guo, Y.
Shi, P.
Citation: Proceedings of the Institution of Mechanical Engineers Part I: Journal of Systems and Control Engineering, 2010; 224(6):713-723
Publisher: Professional Engineering Publishing Ltd
Issue Date: 2010
ISSN: 0959-6518
2041-3041
Statement of
Responsibility: 
B Jiang, Y Guo, and P Shi
Abstract: This paper presents a framework for actuator fault accommodation using a multiple-model-based direct adaptive control approach that does not include explicit fault detection and isolation. This approach does not require exact information about the controlled system and persistent input excitations. The method can increase robustness and provides stable adaptation of unknown faults. Asymptotic model following conditions and adaptive rules are derived and system stability is guaranteed, while appropriate switching of the multiple models ensures asymptotic tracking for system outputs. An aircraft model is given to illustrate the efficiency of the proposed method.
Keywords: actuator fault
direct adaptive reconfiguration control
multiple model
flight control systems
Rights: © Authors 2010
DOI: 10.1243/09596518JSCE894
Appears in Collections:Aurora harvest 4
Electrical and Electronic Engineering publications

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