Multi-Model Based Adaptive Reconfiguration Control for Flight Control Systems with Actuator Faults
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.
Abstract
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.
Dimensions Badge
Altmetric Badge
Additional Information | Proceedings of a meeting held 23-25 May 2011, Mianzhou Hotel, Mianyang, China |
Item type | Book Section |
URI | https://vuir.vu.edu.au/id/eprint/10546 |
DOI | 10.1109/CCDC.2011.5968397 |
Official URL | http://ieeexplore.ieee.org/xpl/articleDetails.jsp?... |
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 |
Download/View statistics | View download statistics for this item |