DocumentCode :
597798
Title :
Fuzzy guidance law for surface-to-air missile in the command control systems
Author :
Trung-Dung Pham ; Qui Tran ; Duc-Vuong Vu
Author_Institution :
Dept. of Control Eng., Mil. Tech. Acad., Hanoi, Vietnam
fYear :
2012
fDate :
26-29 Nov. 2012
Firstpage :
317
Lastpage :
322
Abstract :
A fuzzy guidance law for surface-to-air missile in the command control system is proposed. The performance of the designed guidance law is compared with the famous and widely used guidance law, known as proportional navigation guidance law. The simulation results are proved the effectiveness of the novel guidance law.
Keywords :
command and control systems; fuzzy control; missile control; motion control; navigation; command control system; fuzzy guidance law; proportional navigation guidance law; surface-to-air missile; Acceleration; Missiles; Navigation; Pragmatics; Target tracking; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control, Automation and Information Sciences (ICCAIS), 2012 International Conference on
Conference_Location :
Ho Chi Minh City
Print_ISBN :
978-1-4673-0812-0
Type :
conf
DOI :
10.1109/ICCAIS.2012.6466610
Filename :
6466610
Link To Document :
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