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Unmanned aerial vehicle counter system

A drone and machine countermeasure technology, applied in the field of drone analysis, can solve problems such as destruction failure and tracking failure, and achieve the effect of solving tracking failure or destruction failure

Active Publication Date: 2019-12-20
ARMY ENG UNIV OF PLA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of this, the embodiment of the present invention provides a drone countermeasure system to solve the problem in the prior art that may lead to tracking failure or destruction failure when the position of the drone changes

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Embodiment Construction

[0040] In the following description, for the purpose of illustration rather than limitation, specific details such as a specific system structure and technology are proposed for a thorough understanding of the embodiments of the present invention. However, it should be clear to those skilled in the art that the present invention can also be implemented in other embodiments without these specific details. In other cases, detailed descriptions of well-known systems, devices, circuits, and methods are omitted to avoid unnecessary details from obstructing the description of the present invention.

[0041] In order to illustrate the technical solution of the present invention, specific embodiments are used for description below.

[0042] figure 1 It is a schematic diagram of an unmanned aerial vehicle countermeasure system provided by an embodiment of the present invention, which is detailed as follows.

[0043] Such as figure 1 As shown, a UAV countermeasure system may include: a dete...

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Abstract

The present invention provides an unmanned aerial vehicle counter system, pertaining to the technical field of unmanned aerial vehicle analysis. The system comprises a ground measurement and control module. The ground measurement and control module plans the air route of an attack unmanned aerial vehicle according to the received location information of a target unmanned aerial vehicle, and a pre-planned air route is acquired. When the location of the target unmanned aerial vehicle is changed, the attack unmanned aerial vehicle re-plans the pre-planned air route according to the location change information of the target unmanned aerial vehicle, the information detected by the attack unmanned aerial vehicle in real time and the received real-time information monitored by the ground measurement and control module, and the attack unmanned aerial vehicle flies to an attackable area and attack the target unmanned aerial vehicle according to the re-planed air route, so that the attack unmanned aerial vehicle can still attack the target unmanned aerial vehicle when the location of the target unmanned aerial vehicle is changed, and thus the possible problem of tracking failure or destruction failure caused by the location change of the unmanned aerial vehicle in the prior art, is solved.

Description

Technical field [0001] The invention belongs to the technical field of drone analysis, and particularly relates to a drone countermeasure system. Background technique [0002] In recent years, with the rapid development of drones and other aircraft and the gradual opening of low-altitude airspace control, there has been an increasing number of incidents such as "low, slow, and small" drones illegally flying into the air and black flying. The “Slow and Small” drones are tracked and destroyed to resist the illegal launch of the “Low and Small” drones. [0003] The "low, slow, small" UAV has the characteristics of low flying height, slow movement speed, and small radar scattering area. Therefore, it is difficult to defend, strike and counter-control the "low, slow, small" UAV. In the prior art, when countering "low, slow, small" drones, the drone is directly tracked after the position of the drone is determined. When the position of the drone changes, the tracking or destruction may ...

Claims

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Application Information

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IPC IPC(8): G05D1/02
CPCG05D1/02
Inventor 李伟席雷平马彦恒杨森李建增左宪章史凤鸣郑翌洁赵东昊
Owner ARMY ENG UNIV OF PLA
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