Title
Adaptive neural network internal model control for tilt rotor aircraft platform
Abstract
An adaptive neural networks internal model controller is designed for a tilt rotor aircraft platform. The behavior of the research platform, in certain aspects, resembles that of a tilt rotor aircraft. The proposed control architecture can compensate external disturbances and dynamic inversion error. The controller includes an on-line learning neural network of inverse model and an off-line trained neural network of forward model. Lyapunov stability analysis guarantees tracking errors and network parameters are bounded. The performance of the controller is demonstrated using the tilt rotor aircraft platform, including nacelle tilting flight.
Year
DOI
Venue
2005
10.1007/11539117_38
ICNC (2)
Keywords
Field
DocType
tilt rotor aircraft platform,adaptive neural network,internal model controller,network parameter,inverse model,neural network,tilt rotor aircraft,research platform,off-line trained neural network,forward model,inverse modeling
Control theory,Control theory,Computer science,Model predictive control,Lyapunov stability,Rotor (electric),Artificial neural network,Nacelle,Internal model,Tracking error
Conference
Volume
ISSN
ISBN
3611
0302-9743
3-540-28325-0
Citations 
PageRank 
References 
0
0.34
0
Authors
3
Name
Order
Citations
PageRank
Changjie Yu101.01
Jihong Zhu2105.89
Zengqi Sun374692.44