DocumentCode
233027
Title
The application of proportional navigation in the process of UAV air combat guidance and optimization of proportional parameter
Author
Wang Hui ; Guan Zuoyu ; Yu Lijun
Author_Institution
Coll. of Autom., Harbin Eng. Univ., Harbin, China
fYear
2014
fDate
28-30 July 2014
Firstpage
7892
Lastpage
7896
Abstract
The authors propose a concept of effective attack range to follow the active attacking of Unmanned Aerial Vehicle. An improved proportional navigation model is suggested for being used in the air combat Unmanned Aerial Vehicle guidance model. In addition, the value of proportional parameter is calculated in nonlinear guidance model, and the optimal proportional parameter is confirmed. The simulation results show that the proposed model is effective and quickly.
Keywords
aircraft landing guidance; aircraft navigation; autonomous aerial vehicles; optimisation; proportional control; air combat UAV guidance model; nonlinear guidance model; optimal proportional parameter optimisation; proportional navigation model; unmanned aerial vehicle; Decision support systems; Trajectory; Attack range; Unmanned Aerial Vehicle; optimal parameter; proportional guidance law;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2014 33rd Chinese
Conference_Location
Nanjing
Type
conf
DOI
10.1109/ChiCC.2014.6896318
Filename
6896318
Link To Document