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
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;
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
DOI :
10.1109/ChiCC.2014.6896318