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Multi rotor unmanned aerial vehicle with high brightness air illumination

A multi-rotor unmanned aerial vehicle, high-brightness technology, applied in the field of unmanned aerial vehicles, can solve the problem of not having high-brightness aerial lighting function, etc., and achieve the effects of wide power supply range, high flexibility, and improved efficiency

Pending Publication Date: 2017-05-17
合肥佳讯科技有限公司
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AI Technical Summary

Problems solved by technology

However, at present, multi-rotor UAVs do not have the above-mentioned high-brightness aerial lighting functions, and there are deficiencies in the application of multi-rotor UAVs in on-site command and control, which urgently need to be solved

Method used

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  • Multi rotor unmanned aerial vehicle with high brightness air illumination

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Embodiment Construction

[0031] Now describe in detail the structural features of the present invention in conjunction with the accompanying drawings.

[0032] A multi-rotor drone with high-brightness aerial lighting, see figure 1 , including a mobile terminal 10 and a terminal 20, the mobile terminal 10 is installed on the multi-rotor UAV, and the terminal 20 is installed in the ground receiving station;

[0033] Wherein, the mobile terminal 10 includes a mobile terminal central processing unit 11, a mobile terminal data transmission module 12, a mobile terminal remote control receiver module 13, a mobile terminal LED lamp power control module 14, a mobile terminal LED lamp 15, and a mobile terminal steering gear 16; specifically , the mobile terminal central processing unit 11 is respectively connected with the mobile terminal data transmission module 12, the mobile terminal remote control receiver module 13, and the mobile terminal LED light power control module 14; 20, the mobile terminal central...

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Abstract

The invention discloses a multi rotor unmanned aerial vehicle with high brightness air illumination, comprising a mobile terminal and a terminal, wherein the mobile terminal installed on the unmanned aerial vehicle, and the terminal mounted in the ground receiving station; the mobile terminal comprises a central processing unit of mobile terminal, a data transmission module for mobile terminal, a remote control receiver module for mobile terminal, a LED lamp power supply control module and a mobile terminal LED lamp; the central processing unit of mobile terminal is respectively connected with the mobile terminal data transmission module, the remote control receiver module and the LED lamp power supply control module; the terminal comprises a terminal data transmission module and a terminal aircraft remote controller which are respectively connected and communicated in two directions with the terminal central processing unit; the remote control receiver module receives the signal from the terminal aircraft remote controller, and the switch control is achieved by the mobile LED power control module. The invention solves the shortcomings of the existing multi rotor UAV in the field of command and control application through the airborne high brightness air illumination.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a multi-rotor unmanned aerial vehicle with a high-brightness aerial lighting function. Background technique [0002] The rotor unmanned aerial vehicle is an advanced vertical take-off and landing micro-autopilot unmanned aerial vehicle system. It is suitable for departments such as firefighting, transportation, public security and police technical investigation. Various aerial missions such as tracking and real-time intelligence gathering. [0003] Unmanned aerial vehicles have many advantages such as small size, flexible maneuverability, simple operation, convenient maintenance, convenient portability, reliability and high cost performance. In addition, they also have all-terrain take-off and landing capabilities and are highly intelligent. They can fly in various attitudes, such as hovering , forward flight, side flight and inverted flight, etc., h...

Claims

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Application Information

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IPC IPC(8): G05D1/12
CPCG05D1/12Y02B20/40
Inventor 王秀俊陈梅玲张淑萍
Owner 合肥佳讯科技有限公司
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