DocumentCode
2769191
Title
Nonlinear control of missile dynamics
Author
Kwan, Chiman ; Xu, Roger ; Liu, Wei ; Tan, Richard ; Haynes, Len
Author_Institution
Intelligent Autom. Inc., Rockville, MD, USA
Volume
4
fYear
1998
fDate
16-18 Dec 1998
Firstpage
4685
Abstract
We propose an approach that combines the merits of both feedback linearization (FL) and an online tuning fuzzy CMAC neural network, and eliminates their weaknesses. In particular, the combined method eliminates the robustness weakness of FL and poor high acceleration tracking performance of fuzzy CMAC controller. The resulting method is robust to both system uncertainties and can track high acceleration manoeuvring targets
Keywords
acceleration control; cerebellar model arithmetic computers; dynamics; feedback; fuzzy control; fuzzy neural nets; linearisation techniques; missile control; neurocontrollers; nonlinear control systems; tuning; CMAC neural network; acceleration tracking; dynamics; feedback linearization; fuzzy CMAC neural network; fuzzy control; missile control; neurocontrol; nonlinear control systems; online tuning; robustness; Acceleration; Fuzzy control; Fuzzy logic; Fuzzy neural networks; Missiles; Neural networks; Neurofeedback; Robust control; Robustness; Target tracking;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1998. Proceedings of the 37th IEEE Conference on
Conference_Location
Tampa, FL
ISSN
0191-2216
Print_ISBN
0-7803-4394-8
Type
conf
DOI
10.1109/CDC.1998.762073
Filename
762073
Link To Document