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