Unmanned aerial vehicle cluster booster rocket ignition control system and working method thereof

A technology of ignition control and unmanned aerial vehicle, which is applied in the direction of rocket engine device, mechanical equipment, jet propulsion device, etc., to avoid the risk of human error and realize the effect of wireless remote ignition control

Pending Publication Date: 2020-12-01
NO 60 RES INST OF GENERAL STAFF DEPT PLA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to solve the above-mentioned problems and risks existing in the prior art, the object of the present invention is to provide a UAV cluster booster roc

Method used

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  • Unmanned aerial vehicle cluster booster rocket ignition control system and working method thereof
  • Unmanned aerial vehicle cluster booster rocket ignition control system and working method thereof
  • Unmanned aerial vehicle cluster booster rocket ignition control system and working method thereof

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Example Embodiment

[0060] The present invention will be further described below with reference to the accompanying drawings and embodiments.

[0061] like figure 1 As shown, the present invention provides a UAV cluster booster rocket ignition control system, including a physical port identification module 1, a display module 2, an information processing module 3, an ignition control module 4, a computer (including host computer software) 5, Telemetry receiver 6 and remote control receiver 7.

[0062] The physical port identification module 1 includes a wiring port and a port inspection circuit board connected to the wiring port, and several booster rockets are connected to the wiring port of the physical port identification module 1 through wires;

[0063] The display module 2 includes a display screen and a circuit board connected to the display screen for displaying the current system working state;

[0064] The information processing module 3 includes a wiring port and a circuit board conne...

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Abstract

The invention discloses an unmanned aerial vehicle cluster booster rocket ignition control system and a working method thereof. The system comprises a display module, an information processing module,a physical port recognition module, a computer (including upper computer software), an ignition control module, a remote-control receiver and a telemetering receiver. Ignition triggering conditions are judged through the computer (including the upper computer software), remote control code recognition logic and telemetering code recognition logic, and manual or automatic triggering of multi-channel booster rocket ignition is achieved. According to the unmanned aerial vehicle cluster booster rocket ignition control system and the working method thereof, multi-aircraft ignition launching is supported in an unmanned aerial vehicle cluster scene, automatic or manual ignition launching of different types of unmanned aerial vehicle booster rockets can be adapted to, and the problem that a booster rocket ignition control device is numerous in type, tedious in operation and high in error risk during unmanned aerial vehicle cluster launching is solved.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicle booster rocket ignition control, and in particular relates to an unmanned aerial vehicle cluster booster rocket ignition control system and a working method thereof. Background technique [0002] UAVs have been widely used in civilian and military fields, especially UAVs launched by booster rockets are the most widely used in military projects. The use of rocket-assisted launch has the characteristics of rapid deployment, strong mobility, and low requirements for the site. Typically, a UAV is equipped with a booster rocket ignition control system. As the training of troops is close to actual combat, the execution of tasks by a single aircraft can no longer meet the needs of practical training, and there is an urgent need for drone clusters to take off for multiple sorties. Therefore, the future UAV launch and take-off will be a kind of intensive cluster launch and take-off in the...

Claims

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Application Information

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IPC IPC(8): F02K9/95F02K9/96B64F1/04
CPCF02K9/95F02K9/96B64F1/04Y02P90/02
Inventor 卜培和毛师彬王德明
Owner NO 60 RES INST OF GENERAL STAFF DEPT PLA
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