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Reconnaissance and strike integrated unmanned plane image guided missile target capture method

A technology of unmanned aerial vehicles and missiles, applied in image enhancement, image analysis, image data processing, etc., to achieve the effect of small amount of calculation on board, simple operation, and lighten the burden

Inactive Publication Date: 2017-09-29
XIAN AISHENG TECH GRP +2
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] In order to avoid the deficiencies of the prior art, the present invention proposes a target acquisition method for reconnaissance and attack of unmanned aerial vehicle image-guided missiles, which solves the problem of unmanned aerial vehicle-borne image-guided missile target search and capture, thereby overcoming the problems of airborne movable base and Operational difficulty caused by link delay, improve target acquisition efficiency, and enhance the combat effectiveness of fixed-point clearing

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  • Reconnaissance and strike integrated unmanned plane image guided missile target capture method
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  • Reconnaissance and strike integrated unmanned plane image guided missile target capture method

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Embodiment Construction

[0023] Now in conjunction with embodiment, accompanying drawing, the present invention will be further described:

[0024] A method for capturing a UAV image-guided missile target proposed by the present invention, first uses the UAV airborne photoelectric load within a large field of view, and uses the traditional method to search and track the target; then uses the optical axis automatic guidance method Point the optical axis of the missile seeker to the target, and the fire control operator at the ground control station is on the seeker image, and uses image matching and pixel correction to track and capture the target, so as to constitute the launch condition, within the effective operation time.

[0025] The steps of the method involved in the present invention are as follows:

[0026] 1. Automatic guidance and calculation of the optical axis of the photoelectric load seeker

[0027] 1) The shafting relationship between the missile and the aircraft;

[0028] The present...

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Abstract

The invention relates to a reconnaissance and strike integrated unmanned plane image guided missile target capture method. The method comprises steps that firstly, an unmanned airborne photoelectric load is in a large view field scope, and target searching and tracking are carried out in a traditional mode; and secondly, an optical axis automatic guiding method is utilized to make a missile seeker optical axis point to a target, a ground control station fire control manipulator is on a seeker image, an image matching and pixel correction mode is employed to realize target tracking and capture, and emission conditions are constructed with the operational use time. The method is advantaged in that airborne calculation is small, high timeliness and simple operation are realized, autonomous attack capability of the unmanned plane is effectively improved, and a reconnaissance and strike integrated unmanned plane image guided missile is simple and convenient to use.

Description

technical field [0001] The invention belongs to the control technology of unmanned aerial vehicle mission equipment, and in particular relates to a method for capturing an image-guided missile target of an unmanned aerial vehicle. Background technique [0002] The weapon configuration of integrated drones for reconnaissance and attack is generally based on laser-guided missiles or bombs. The guidance method is mostly laser semi-active. The location puts it at risk. [0003] Image-guided missiles have the characteristics of "locking before launch and leaving after launch". In recent years, their miniaturization technology has become more mature, but they are mainly used for "ground-to-ground" or "ground-to-air" attacks on individual vehicles. There are fewer applications for "air-to-ground" attacks carried on UAVs. [0004] Image-guided missiles mounted on UAVs, on the one hand, due to the small market scope of missile seekers, it is very difficult to directly search for ta...

Claims

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Application Information

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IPC IPC(8): G06T7/73G06T7/246
CPCG06T7/251G06T7/73G06T2207/20092G06T2207/30212
Inventor 贾伟李大健马夏莹马远超
Owner XIAN AISHENG TECH GRP
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