Multi-Model Based Adaptive Reconfiguration Control for Flight Control Systems with Actuator Faults

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Guo, Yuying, Zhang, Youmin, Shi, Peng, Jiang, Bin and Zhu, Zhengwei (2011) Multi-Model Based Adaptive Reconfiguration Control for Flight Control Systems with Actuator Faults. In: 2011 Chinese Control and Decision Conference (CCDC). IEEE, [Piscataway, N.J.], pp. 1335-1340.


This paper concerns the application of multi-model based adaptive control approach to accommodate actuator fault for flight control systems. isolation. This approach does not require the 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.

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Proceedings of a meeting held 23-25 May 2011, Mianzhou Hotel, Mianyang, China

Item type Book Section
DOI 10.1109/CCDC.2011.5968397
Official URL
ISBN 9781424487370 (print) 9781424487363 (CD-ROM)
Subjects Historical > Faculty/School/Research Centre/Department > Institute for Logistics and Supply Chain Management (ILSCM)
Historical > FOR Classification > 0802 Computation Theory and Mathematics
Historical > SEO Classification > 970108 Expanding Knowledge in the Information and Computing Sciences
Keywords ResPubID25047, adaptive control, aerospace control, aircraft, stability, actuator fault, direct adaptive reconfiguration control, flight control systems, multiple model
Citations in Scopus 1 - View on Scopus
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