Adaptive fault-tolerant tracking controller design against actuator stuck faults
This paper studies the problem of adaptive fault-tolerant tracking control for linear continuous-time systems with actuator stuck faults. A design method of an adaptive fault-tolerant tracking controller is developed based on the online estimation of the functioning of the actuators that is used to...
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sg-ntu-dr.10356-847622020-03-07T13:24:45Z Adaptive fault-tolerant tracking controller design against actuator stuck faults Wang, Jianliang Zhang, Xiao-Ni. Yang, Guang-Hong. School of Electrical and Electronic Engineering Chinese Control and Decision Conference (24th : 2012 : Taiyuan, China) This paper studies the problem of adaptive fault-tolerant tracking control for linear continuous-time systems with actuator stuck faults. A design method of an adaptive fault-tolerant tracking controller is developed based on the online estimation of the functioning of the actuators that is used to monitor the health of the system. In the event of actuator stuck faults, a compensation controller is incorporated into the initial controller to improve control effect and reject the zero-frequency disturbance produced by the stuck-actuators. Finally, the design procedure and the advantage of the proposed method are illustrated via a numerical example of flight control of an F-16 aircraft. 2013-08-01T04:36:06Z 2019-12-06T15:50:52Z 2013-08-01T04:36:06Z 2019-12-06T15:50:52Z 2012 2012 Conference Paper Zhang, X.-N., Wang, J., & Yang, G.-H. (2012). Adaptive fault-tolerant tracking controller design against actuator stuck faults. 2012 24th Chinese Control and Decision Conference (CCDC), 4098-4103. https://hdl.handle.net/10356/84762 http://hdl.handle.net/10220/12792 10.1109/CCDC.2012.6244655 en |
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This paper studies the problem of adaptive fault-tolerant tracking control for linear continuous-time systems with actuator stuck faults. A design method of an adaptive fault-tolerant tracking controller is developed based on the online estimation of the functioning of the actuators that is used to monitor the health of the system. In the event of actuator stuck faults, a compensation controller is incorporated into the initial controller to improve control effect and reject the zero-frequency disturbance produced by the stuck-actuators. Finally, the design procedure and the advantage of the proposed method are illustrated via a numerical example of flight control of an F-16 aircraft. |
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School of Electrical and Electronic Engineering |
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School of Electrical and Electronic Engineering Wang, Jianliang Zhang, Xiao-Ni. Yang, Guang-Hong. |
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Conference or Workshop Item |
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Wang, Jianliang Zhang, Xiao-Ni. Yang, Guang-Hong. |
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Wang, Jianliang Zhang, Xiao-Ni. Yang, Guang-Hong. Adaptive fault-tolerant tracking controller design against actuator stuck faults |
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Wang, Jianliang |
title |
Adaptive fault-tolerant tracking controller design against actuator stuck faults |
title_short |
Adaptive fault-tolerant tracking controller design against actuator stuck faults |
title_full |
Adaptive fault-tolerant tracking controller design against actuator stuck faults |
title_fullStr |
Adaptive fault-tolerant tracking controller design against actuator stuck faults |
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Adaptive fault-tolerant tracking controller design against actuator stuck faults |
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adaptive fault-tolerant tracking controller design against actuator stuck faults |
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2013 |
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https://hdl.handle.net/10356/84762 http://hdl.handle.net/10220/12792 |
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1681047338336911360 |