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Rapid integration method for realizing plug and play of task loads

A plug-and-play, integrated method of technology, applied in the direction of aircraft parts, aircraft, motor vehicles, etc., can solve the problems of lagging development cycle, rising cost, huge workload of load integration, etc., and achieve the effect of expanding the application field

Active Publication Date: 2021-01-08
CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When there are dozens or hundreds of types of task loads, the workload of load integration will be huge, the development cycle will be seriously delayed, and the cost will continue to rise

Method used

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  • Rapid integration method for realizing plug and play of task loads
  • Rapid integration method for realizing plug and play of task loads

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Experimental program
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Embodiment Construction

[0017] This part is the embodiment of the present invention, which is used to explain and illustrate the technical solution of the present invention.

[0018] A fast integration method for realizing task load plug-and-play. First, the task load is analyzed to determine the classification of each functional channel; then a standard plug-and-play interface is designed according to the classification of each functional channel of the task load; finally, the task load is The payload is integrated into the aircraft, and each of its functional channels matches that of the aircraft.

[0019] The functional channels of the mission load include installation channels, power supply channels, command channels, information transmission channels and display control channels. Among them, the installation channel of the task load is classified according to the size of the task load, and is divided into three categories: large, medium and small. The power supply channels of the task load are ...

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Abstract

The invention belongs to the technical field of unmanned aerial vehicle design, and discloses a rapid integration method for realizing plug and play of task loads, which comprises the following stepsof: firstly, analyzing a task load, and determining the classification of each functional channel thereof, including an installation channel, a power supply channel, an instruction channel, an information transmission channel and a display control channel; designing a standard plug-and-play interface according to the classification of each functional channel of the task load; and finally, integrating the task load on an aircraft, wherein each functional channel is matched with a functional channel of the aircraft. Through a rapid integration method of load classification and function channel design, plug and play of task loads is realized, the task load integration period is greatly shortened, the development cost is reduced, the requirements of users can be rapidly met, various task loadsare integrated, and the application field of unmanned aerial vehicles is expanded.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicle design, relates to an integration method of unmanned aerial vehicle task loads, and in particular relates to a fast integration method for realizing plug-and-play task loads. Background technique [0002] With the continuous development of UAV application technology, UAVs are widely used in military fields such as intelligence reconnaissance, border patrol, ground attack, electronic countermeasures, and civilian fields such as artificial rain enhancement, forest fire prevention, disaster prevention, emergency rescue, and communication relay. The application is more and more extensive. More and more domestic and foreign users put forward demands to quickly integrate various mission loads specified by users on the basis of the existing UAV mission system to adapt to different mission requirements of users. When the traditional mission load is integrated into the UAV, it is necessary...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D43/00B64C39/02
CPCB64D43/00B64C39/02
Inventor 石继召潘静张阳卓强刘宽陈龙建
Owner CHENGDU AIRCRAFT DESIGN INST OF AVIATION IND CORP OF CHINA