Three-Dimensional Cooperative Guidance Law Design for Simultaneous Attack with Multiple Missiles Against a Maneuvering Target

2018 ◽  
Author(s):  
Jialing Zhou ◽  
Yuezu Lv ◽  
Guanghui Wen ◽  
Xiongjun Wu ◽  
Meng Cai
Keyword(s):  
Three Dimensional ◽  
Maneuvering Target ◽  
Guidance Law ◽  
Multiple Missiles ◽  
Cooperative Guidance ◽  
Simultaneous Attack

scholarly journals Fixed-Time Cooperative Guidance Law With Angle Constraint for Multiple Missiles Against Maneuvering Target

IEEE Access ◽  
2020 ◽  
Vol 8 ◽  
pp. 73268-73277
Author(s):  
Liang Jing ◽  
Liang Zhang ◽  
Jifeng Guo ◽  
Naigang Cui
Keyword(s):  
Fixed Time ◽  
Maneuvering Target ◽  
Guidance Law ◽  
Multiple Missiles ◽  
Cooperative Guidance

Simultaneous attack strategy against a maneuvering target with unknown acceleration

2017 ◽  
Vol 233 (1) ◽  
pp. 71-80
Author(s):  
Zilun Hu ◽  
Jianying Yang
Keyword(s):  
Maneuvering Target ◽  
Guidance Law ◽  
Multiple Missiles ◽  
Simultaneous Attack ◽  
Attack Strategy

This paper is concerning the simultaneous attack problem with multiple missiles against a maneuvering target with unknown acceleration. The new guidance protocol, which avoids using the time-to-go information, ensures the simultaneous attack based on the consensus of the range-to-go and the approaching rate of each missile. This strategy is a distributed guidance law where each missile can only get information from neighbors. The consensus of the missiles is shown mathematically as well as with extensive simulations.

scholarly journals On 3D simultaneous attack against manoeuvring target with communication delays

2020 ◽  
Vol 17 (1) ◽  
pp. 172988141989480
Author(s):  
Zhaohui Liu ◽  
Yuezu Lv ◽  
Jialing Zhou ◽  
Liang Hu
Keyword(s):  
Kinetic Model ◽  
Dimensional Space ◽  
Three Dimensional ◽  
Line Of Sight ◽  
Communication Delays ◽  
Delayed Information ◽  
Guidance Law ◽  
Multiple Missiles ◽  
Simultaneous Attack ◽  
Three Dimensional Space

This article investigates the simultaneous attack problem of multiple missiles against a manoeuvring target with delayed information transmission in three-dimensional space. Based on the kinetic model of the missiles, the problem is divided into three demands: the velocity components normal to line-of-sight converge to zero in finite time, the component of motion states along line-of-sight should achieve consensus and converge to zero. The guidance law is designed for each demand and by theoretical proof, the upper bound of delay which can tolerate is presented and the consensus error of the relative distances can converge to a small neighbourhood of zero. And simulation example presented also demonstrates the validity of the theoretical result.

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