DocumentCode
233757
Title
A fuzzy guidance law design with terminal-angle constraint
Author
Chuanjiang Li ; Yanchao Sun ; Teng Lv ; Guangfu Ma ; Junzi Xiao
Author_Institution
Harbin Inst. of Technol., Harbin, China
fYear
2014
fDate
28-30 July 2014
Firstpage
749
Lastpage
753
Abstract
In this paper, a kind of reference trajectory of line-of-sight angle based on the optimal control theory is given, which can make the missile hit the ground fixed target accurately and satisfy the demand for terminal-angle constraint. Then, the corresponding fuzzy control law is designed to achieve the tracking of the reference trajectory of line-of-sight angle. Simulation results show that the proposed fuzzy guidance law has high control precision and can meet the demand for terminal-angle constraint.
Keywords
control system synthesis; fuzzy control; missile guidance; optimal control; trajectory control; fuzzy control law; fuzzy guidance law design; ground fixed target; line-of-sight angle; optimal control theory; reference trajectory; terminal-angle constraint; Fuzzy control; Missiles; Navigation; Niobium; Optimal control; Target tracking; Trajectory; Terminal-angle constraint; fuzzy control; line-of-sight angle tracking; optimal control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2014 33rd Chinese
Conference_Location
Nanjing
Type
conf
DOI
10.1109/ChiCC.2014.6896720
Filename
6896720
Link To Document