Please use this identifier to cite or link to this item:
https://hdl.handle.net/2440/87981
Citations | ||
Scopus | Web of Science® | Altmetric |
---|---|---|
?
|
?
|
Type: | Conference paper |
Title: | Multi-model based adaptive reconfiguration control for flight control systems with actuator faults |
Author: | Guo, Y. Zhang, Y. Shi, P. Jiang, B. Zhu, Z. |
Citation: | Proceedings of the 2011 Chinese Control and Decision Conference, CCDC 2011, 2011, pp.1335-1340 |
Publisher: | IEEE |
Publisher Place: | USA |
Issue Date: | 2011 |
Series/Report no.: | Chinese Control and Decision Conference |
ISBN: | 9781424487370 |
ISSN: | 1948-9439 |
Conference Name: | Chinese Control and Decision Conference (CCDC) (23 May 2011 - 25 May 2011 : Mianyang, China) |
Statement of Responsibility: | Yuying Guo, Youmin Zhang, Peng Shi, Bin Jiang and Zhengwei Zhu |
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. |
Rights: | © 2011 IEEE |
DOI: | 10.1109/CCDC.2011.5968397 |
Published version: | http://dx.doi.org/10.1109/ccdc.2011.5968397 |
Appears in Collections: | Aurora harvest 7 Electrical and Electronic Engineering publications |
Files in This Item:
There are no files associated with this item.
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.