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Method for simulating infrared characteristic and target drone

A simulation method and infrared technology, applied in the aviation field, can solve the problems of non-reuse, large size of the target body, damage to the target aircraft, etc., and achieve the effects of avoiding waste, low cost and high flexibility.

Pending Publication Date: 2020-04-10
北京安达维尔航空设备有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Target drones damaged by real strikes cannot be reused, and reusable target drones are mostly larger in size and more expensive

Method used

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  • Method for simulating infrared characteristic and target drone
  • Method for simulating infrared characteristic and target drone
  • Method for simulating infrared characteristic and target drone

Examples

Experimental program
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Embodiment

[0032]In this embodiment, the engine room includes three cabins, the fuel system cabin, the infrared source placement cabin and the avionics system cabin, and each cabin is equipped with a portable dismountable cabin cover, and the inside of the cabin is equipped with Reinforcing ribs; the airfoil of the side wing 5 is a flat convex wing, including a main beam, ribs and skin, the main beam is a carbon tube structure, the ribs are balsa wood, and the skin is aviation glass fiber and Compatible material of honeycomb core material, ailerons are installed on the rear edge, and the distribution method of the full span is adopted; the empennage 7 is an integrated gradual airfoil, the front edge adopts a U-shaped installation card slot and a pin shaft docking method, and the back-up adopts A fixing method in which a firmware penetrates up and down; the landing gear adopts the design method of hydraulic pressure and shock absorbing spring, and is connected with the nacelle through a hi...

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Abstract

According to a simulation method for infrared characteristics of an actual aircraft, a designed infrared source can adjust the luminous intensity and the radiation intensity according to the infraredcharacteristics of the actual aircraft so as to be closer to the actual aircraft, and it can be guaranteed that the striking effect is real and effective. The infrared source is applied to the targetdrone, and the target drone simulating the infrared characteristics is designed and comprises a drone body unit, a navigation control unit, a power unit and an infrared source unit. The infrared source unit is provided with a device capable of releasing an infrared source, so that the infrared source is combusted and hit outside a cabin of the drone aircraft, and the drone aircraft can be repeatedly used. The target drone is further provided with a recycling device, the combustion condition of the infrared source combustion agent can be detected in real time, and therefore the infrared sourceobtained after combustion and the infrared source with abnormal combustion are recycled, pollution is reduced, waste is avoided, and cost is saved.

Description

technical field [0001] The invention relates to the field of aviation, in particular to a method for simulating infrared features and a target drone. Background technique [0002] At present, the target drones used for military shooting training are mostly used for one-time use, as objects attacked by air and ground weapons. The target drone flies through a pre-set flight trajectory, providing hypothetical attack targets for various weapons to improve the actual combat level of weapon operators, or used to test the attack capabilities of newly developed weapons. The damage to the target drone caused by real strikes cannot be reused, and most of the reusable target drones are larger in size and more expensive. Contents of the invention [0003] The object of the present invention is to provide a method and target drone for simulating infrared features, so as to solve the aforementioned problems in the prior art. [0004] In order to achieve the above object, the technical...

Claims

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Application Information

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IPC IPC(8): G05D27/02G09B9/00F41J9/08G01M99/00
CPCF41J9/08G01M99/005G05D27/02G09B9/003
Inventor 刘小猛穆俊光王震荣涛
Owner 北京安达维尔航空设备有限公司
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