DocumentCode
2254835
Title
A fighter aircraft pitch rate control based on neural network parallel controller
Author
Kamalasadan, Sukumar ; Ghandakly, Adel A.
fYear
2005
fDate
20-22 July 2005
Firstpage
135
Lastpage
140
Keywords
Adaptive control; Aerospace control; Artificial neural networks; Military aircraft; Neural networks; Nonlinear dynamical systems; Nonlinear systems; Programmable control; Radial basis function networks; Robust control;
fLanguage
English
Publisher
ieee
Conference_Titel
Computational Intelligence for Measurement Systems and Applications, 2005. CIMSA. 2005 IEEE International Conference on
Print_ISBN
0-7803-9026-1
Type
conf
DOI
10.1109/CIMSA.2005.1522846
Filename
1522846
Link To Document