Adaptive Neural Network Dynamic Inversion with Prescribed Performance for Aircraft Flight Control
Joint Authors
Zhang, Jing
Li, Yuxia
Wang, Honglun
Gai, Wendong
Source
Journal of Applied Mathematics
Issue
Vol. 2013, Issue 2013 (31 Dec. 2013), pp.1-12, 12 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2013-11-21
Country of Publication
Egypt
No. of Pages
12
Main Subjects
Abstract EN
An adaptive neural network dynamic inversion with prescribed performance method is proposed for aircraft flight control.
The aircraft nonlinear attitude angle model is analyzed.
And we propose a new attitude angle controller design method based on prescribed performance which describes the convergence rate and overshoot of the tracking error.
Then the model error is compensated by the adaptive neural network.
Subsequently, the system stability is analyzed in detail.
Finally, the proposed method is applied to the aircraft attitude tracking control system.
The nonlinear simulation demonstrates that this method can guarantee the stability and tracking performance in the transient and steady behavior.
American Psychological Association (APA)
Gai, Wendong& Wang, Honglun& Zhang, Jing& Li, Yuxia. 2013. Adaptive Neural Network Dynamic Inversion with Prescribed Performance for Aircraft Flight Control. Journal of Applied Mathematics،Vol. 2013, no. 2013, pp.1-12.
https://search.emarefa.net/detail/BIM-472731
Modern Language Association (MLA)
Gai, Wendong…[et al.]. Adaptive Neural Network Dynamic Inversion with Prescribed Performance for Aircraft Flight Control. Journal of Applied Mathematics No. 2013 (2013), pp.1-12.
https://search.emarefa.net/detail/BIM-472731
American Medical Association (AMA)
Gai, Wendong& Wang, Honglun& Zhang, Jing& Li, Yuxia. Adaptive Neural Network Dynamic Inversion with Prescribed Performance for Aircraft Flight Control. Journal of Applied Mathematics. 2013. Vol. 2013, no. 2013, pp.1-12.
https://search.emarefa.net/detail/BIM-472731
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-472731