Adaptive NN Control for Multisteering Plane Aircraft with Dead Zone or Backlash Input Nonlinearity
Joint Authors
Lv, Mao-long
Meng, Xiang-fei
Wang, Ying
Source
Mathematical Problems in Engineering
Issue
Vol. 2017, Issue 2017 (31 Dec. 2017), pp.1-8, 8 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2017-06-22
Country of Publication
Egypt
No. of Pages
8
Main Subjects
Abstract EN
Considering that many factors such as actuator input dead zone, backlash, and external disturbance could affect the exactness of trajectory tracking, therewith a robust adaptive neural network control scheme on the basis of control allocation is proposed for the sake of tracking control of multisteering plane aircraft with actuator input dead zone or backlash nonlinearity.
First of all, an actuator input dead zone or backlash nonlinearity control assignment model is established and the control allocation equation is derived.
Secondly, the system nonlinear uncertainty is compensated by means of radial basis function neural network, and a robust term is introduced to achieve robustness against external disturbance and system errors.
Finally, by utilizing Lyapunov stability theorem, it has been proved that all the signals in the closed-loop system are bounded, and the tracking error converges to a small residual set asymptotically.
Simulation results on ICE101 multisteering plane aircraft demonstrate the outstanding tracking performance and strong robustness as well as effectiveness of the proposed approach, which can effectively overcome the adverse influence of dead zone, backlash nonlinearity, and external disturbance on the system.
American Psychological Association (APA)
Meng, Xiang-fei& Wang, Ying& Lv, Mao-long. 2017. Adaptive NN Control for Multisteering Plane Aircraft with Dead Zone or Backlash Input Nonlinearity. Mathematical Problems in Engineering،Vol. 2017, no. 2017, pp.1-8.
https://search.emarefa.net/detail/BIM-1190474
Modern Language Association (MLA)
Meng, Xiang-fei…[et al.]. Adaptive NN Control for Multisteering Plane Aircraft with Dead Zone or Backlash Input Nonlinearity. Mathematical Problems in Engineering No. 2017 (2017), pp.1-8.
https://search.emarefa.net/detail/BIM-1190474
American Medical Association (AMA)
Meng, Xiang-fei& Wang, Ying& Lv, Mao-long. Adaptive NN Control for Multisteering Plane Aircraft with Dead Zone or Backlash Input Nonlinearity. Mathematical Problems in Engineering. 2017. Vol. 2017, no. 2017, pp.1-8.
https://search.emarefa.net/detail/BIM-1190474
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1190474