Cooperative interception of multiple missiles outside the atmosphere based on predicted hit points

Author(s):  
Gaocan Zhu ◽  
Songyan Wang ◽  
Tao Chao
Keyword(s):  
Author(s):  
Daekyu Sang ◽  
Chang-Kyung Ryoo ◽  
Hyoun Jin Kim ◽  
Min-Jae Tahk

Author(s):  
Qilun Zhao ◽  
Xiwang Dong ◽  
Jian Chen ◽  
Zihao Xiong ◽  
Qingdong Li ◽  
...  

2010 ◽  
Vol 33 (1) ◽  
pp. 275-280 ◽  
Author(s):  
In-Soo Jeon ◽  
Jin-Ik Lee ◽  
Min-Jea Tahk

2019 ◽  
Vol 69 (4) ◽  
pp. 369-377
Author(s):  
Yan Shi ◽  
Lihua Zhang ◽  
Shouquan Dong

The path planning of anti-ship missile should be considered both cruising in safety and striking in quick, which is an intractable problem. In particular, it is difficult to consider the safety of each missile path in the path planning of multiple missiles. To solve this problem, the “AREA Algorithm” is presented to divide the relative relations of areas:relative security area of the threat areas and fast-attack area of target approaching. Specifically,it is a way to achieve area division through the relationship between the target and the center of the operational area. The Voronoi diagram topology network, Dijkstra algorithm and binary tree algorithm have been used in the above process as well. Finally, Simulations have verified the feasibility and obvious advantages of “AREA Algorithm” compared with the single algorithm, and the tactical meaning in path planning of multiple missiles.


2019 ◽  
Vol 123 (1262) ◽  
pp. 464-483
Author(s):  
X.L. Ai ◽  
L.L. Wang ◽  
Y.C. Shen

ABSTRACTThis study focuses on the co-operative salvo attack problem of multiple missiles against a stationary target under jointly connected switching topologies subject to time-varying communication delays. By carefully exploring certain features of the typical pure proportional navigation guidance law, a two-stage distributed guidance scheme is proposed without any information on time-to-go in this study to realise the simultaneous attack of multiple missiles. In the first guidance stage, a co-operative guidance law is proposed using local neighbouring communications only to achieve consensus on range-to-go and heading error to provide favourable initial conditions for the latter phase, in which switching topologies and time-varying communication delays are taken into account when obtaining sufficient conditions of consensus in terms of linear matrix inequalities. Then, missiles disconnect from each other and are guided individually by the typical pure proportional navigation guidance law with the same navigation gain to realise salvo attack in the second guidance phase. Finally, numerical simulations are carried out to clearly validate the theoretical results.


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