International Journal of Control, Automation and Systems 2017; 15(3): 1077-1088
Published online May 22, 2017
https://doi.org/10.1007/s12555-015-0383-6
© The International Journal of Control, Automation, and Systems
This paper addresses an adjustable parameter (AP)-based multi-objective fault estimation design for continuous-time/discrete-time dynamic systems. First, a fault estimation observer with AP is constructed to on-line identify the size of occurred faults. The fault estimation design not only possesses a wider application compared with adaptive observers, but also uses the current output information to enhance fault estimation performance. Then a multi-objective approach is proposed to determine the gain matrices of fault estimation observer. Moreover, fault estimation results with the slack-variable technique are obtained to further reduce the conservatism. Finally, simulation results of an aircraft application are presented to illustrate the effectiveness of our contribution."
Keywords Fault diagnosis, fault estimation, multi-objective design.
International Journal of Control, Automation and Systems 2017; 15(3): 1077-1088
Published online June 1, 2017 https://doi.org/10.1007/s12555-015-0383-6
Copyright © The International Journal of Control, Automation, and Systems.
Ke Zhang, Vincent Cocquempot, and Bin Jiang*
Nanjing University of Aeronautics and Astronautics
This paper addresses an adjustable parameter (AP)-based multi-objective fault estimation design for continuous-time/discrete-time dynamic systems. First, a fault estimation observer with AP is constructed to on-line identify the size of occurred faults. The fault estimation design not only possesses a wider application compared with adaptive observers, but also uses the current output information to enhance fault estimation performance. Then a multi-objective approach is proposed to determine the gain matrices of fault estimation observer. Moreover, fault estimation results with the slack-variable technique are obtained to further reduce the conservatism. Finally, simulation results of an aircraft application are presented to illustrate the effectiveness of our contribution."
Keywords: Fault diagnosis, fault estimation, multi-objective design.
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