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Unmanned aerial vehicle countermeasure method and system, electronic equipment and storage medium

A technology of unmanned aerial vehicles and machine countermeasures, which is applied in the direction of control/adjustment system, non-electric variable control, three-dimensional position/channel control, etc., to achieve the effect of improving effectiveness

Pending Publication Date: 2020-01-21
泰州中益海洋装备有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0011] In order to overcome the deficiencies of the prior art, one of the objectives of the present invention is to provide a UAV countermeasure method, system, electronic equipment and storage medium, which can solve the problem of fast and effective countermeasures

Method used

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  • Unmanned aerial vehicle countermeasure method and system, electronic equipment and storage medium

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Embodiment Construction

[0034] Below, the present invention will be further described in conjunction with the accompanying drawings and specific implementation methods. It should be noted that, under the premise of not conflicting, the various embodiments described below or the technical features can be combined arbitrarily to form new embodiments. .

[0035]It should be noted that when a component is said to be "fixed" to another component, it can be directly on the other component or there can also be an intervening component. When a component is said to be "connected" to another component, it may be directly connected to the other component or there may be intervening components at the same time. When a component is said to be "set on" another component, it may be set directly on the other component or there may be an intervening component at the same time. The terms "vertical," "horizontal," "left," "right," and similar expressions are used herein for purposes of illustration only.

[0036] Unl...

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Abstract

The invention discloses an unmanned aerial vehicle countermeasure method. The unmanned aerial vehicle countermeasure method is applied to an unmanned aerial vehicle countermeasure system. The unmannedaerial vehicle countermeasure system includes area identifier units, unmanned aerial vehicle wing capture cameras, a countermeasure jet device, a targeting device, a microcomputer, unmanned aerial vehicle identifier units and an interaction unit, wherein the area identifier units communicate with the microprocessor separately. The area identifier units select a monitoring area and feed the monitoring area back to the microprocessor to generate a countermeasure area. The unmanned aerial vehicle wing capture cameras capture images of the countermeasure area in real time, whether an intruding unmanned aerial vehicle needs to be countered or not is identified by the unmanned aerial vehicle identifier units, and if the intruding unmanned aerial vehicle needs to be countered, the next step is performed; the unmanned aerial vehicle wing capture cameras identify wing positions and feed back identifiers of the wing positions to the targeting device; the targeting device generates a strike identifier and feeds the strike identifier back to the microprocessor; and the strike position is determined by the strike identifier, and the microprocessor drives the countermeasure jet device to strikequickly according to the strike position. Unmanned aerial vehicle wings can be quickly destroyed, and the problem of delay is solved.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicle countermeasures, in particular to a method, system, electronic equipment and storage medium for unmanned aerial vehicle countermeasures. Background technique [0002] At present, in the existing technology, the UAV countermeasure system is generally composed of four main subsystems and modules: the search system, the photoelectric tracking system, the radio frequency interference system and the display and control unit. Among them, the search system completes the monitoring and position indication functions of low-altitude targets in the mission area. It is composed of a search radar and a radio spectrum monitoring system. The search systems of the two systems can be used independently or in combination to improve detection performance according to the environment; the optical tracking system Complete the automatic tracking function of the target, so that the directional antenna of the radio...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 崔小飞王呈贵谢月强邱来贤
Owner 泰州中益海洋装备有限公司
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