DocumentCode
2257983
Title
Target allocation method based on intercept geometry
Author
Jingchuan, Wu ; Baoqing, Yang ; Kai-Ning, Wu
Author_Institution
Control and Simulation Center, Harbin Institute of Technology, Harbin 150001, China
fYear
2015
fDate
28-30 July 2015
Firstpage
5200
Lastpage
5205
Abstract
A target allocation method based on intercept geometry is presented. All the possible intercept points are derived which form the intercept geometry in one-on-one engagement by considering all possible velocity directions of the target. Based on the intercept geometry, the maximum change in velocity for the missile to intercept the target is studied. To obtain the optimal allocation plan, a performance index is proposed based on the maximum change in velocity in one-on-one engagement. In this method, the initial velocity direction of the target and the model of target manoeuvre are needless. Finally, the effectiveness of the proposed method is proved by the simulations under different initial conditions.
Keywords
Energy consumption; Geometry; Missiles; Performance analysis; Predictive models; Resource management; Trajectory; intercept geometry; intercept point; target allocation;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2015 34th Chinese
Conference_Location
Hangzhou, China
Type
conf
DOI
10.1109/ChiCC.2015.7260450
Filename
7260450
Link To Document