Synthesis of Guidance Law for Air-To-Air Missiles Intercepts Separating Targets at Long Distances

被引:3
作者
Nguyen Tat Tuan [1 ]
Vu Hoa Tien [1 ]
Doan Van Minh [1 ]
Nguyen Ngoc Hung [1 ]
机构
[1] Le Quy Don Tech Univ, Hanoi, Vietnam
来源
JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION | 2023年 / 55卷 / 04期
关键词
Optimal Proportional Preemptive Navigation law; Separating target; Super maneuverable target; Long-range air-to-air missile;
D O I
10.6125/JoAAA.202312_55(4).01
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents the results synthesis of an optimal guidance law for air-to-air missiles (AAM) to intercept separating targets at a long distance. Based on the optimal filtering theory, this proposed guidance law allows interceptor missiles to distinguish each target in a group according to the Doppler frequency of each target and guides the missile to a selected target in the group. The simulation results have proved that the proposed guidance law is highly effective when intercepting a separating target, one of the particularly dangerous types of targets.
引用
收藏
页码:507 / 515
页数:9
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