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Continuous automatic ejection device and control method for fixed-wing UAV

A technology of ejection device and UAV, which is applied in the direction of launch/drag transmission device, etc. It can solve the problems of long time, inability to complete short-term UAV deployment, and continuous automatic ejection, etc., to achieve the effect of reducing labor costs

Active Publication Date: 2022-05-24
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

One of the effective methods to achieve the above effects is catapult take-off. Therefore, this method of take-off has been paid more and more attention by many countries at home and abroad. The period of time for the drone to leave the ejection device after connecting to the device is very long, and it is impossible to achieve continuous purposes, and it is also impossible to complete the deployment of short-term drones.
Existing devices cannot perform continuous automatic ejection

Method used

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  • Continuous automatic ejection device and control method for fixed-wing UAV
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  • Continuous automatic ejection device and control method for fixed-wing UAV

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Embodiment Construction

[0062] Below in conjunction with accompanying drawing, the technical scheme of the present invention is described in further detail:

[0063] The invention discloses a continuous automatic ejection device for a fixed-wing unmanned aerial vehicle, which comprises a continuous transmission device, a rack assembly, an ejection reset device, a racking device and a control module;

[0064] The rack assembly is used to adjust the ejection angle and to load the racking device and the ejection reset device;

[0065] The continuous transmission device transmits the drone to between the racking device and the ejection reset device;

[0066] The racking device is used to push the UAV transmission from the continuous transmission device to the ejection reset device;

[0067] The ejection reset device is used to eject the UAV on it;

[0068] The control module is used to control the coordinated work of the continuous conveying device, the rack assembly, the ejection reset device and the ...

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Abstract

The invention discloses a continuous automatic ejection device for a fixed-wing unmanned aerial vehicle and a control method thereof. The device includes a continuous transmission device, a frame assembly, an ejection reset device, a racking device and a control module; Telescopic rod and N hangers; rack assembly includes base, frame body, fixed rod and hydraulic telescopic rod; ejection reset device includes pulley, first to fourth reversing pulleys, rail car, pull rope, winch, winch rope , the first motor, the clutch, the first driving gear, the first to the fourth transmission gears and the elastic rope; fifth to seventh driven gears. The invention realizes automatic ejection of UAVs and re-ejection after reset, and solves the problems of long preparation time before ejection of fixed-wing UAVs, the need for personnel to cooperate to complete the ejection, manual reset after ejection, and long interval between two ejections. .

Description

technical field [0001] The invention relates to the field of control of the ejection of unmanned aerial vehicles, in particular to a continuous automatic ejection device of a fixed-wing unmanned aerial vehicle and a control method thereof. Background technique [0002] With the continuous advancement of technology in the field of drone swarm control, the application field of drones continues to expand, and the prospect of use becomes broader. As part of the drone system, drone launch technology determines whether the drone can be successfully launched into the air. , is a crucial part of the value, but so far there is no product that continuously launches the UAV group into the air in a short period of time. [0003] In order to realize the deployment of the UAV from the designated position in a short period of time, it is necessary to realize the compactness of the UAV group from the preparation state to obtaining the required speed for take-off, that is, continuity, that i...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F1/06
CPCB64F1/06
Inventor 魏小辉郝嘉煜彭一明张钊罗江雪
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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