General miniature unmanned aerial vehicle

Abstract

The invention relates to a general miniature unmanned aerial vehicle. The general miniature unmanned aerial vehicle structurally comprises a server (I) and a server (II) which are positioned on left and right wings of the aerial vehicle, wherein wingtips and ailerons are connected with the tail ends of the left and right wings; a brushless electronic speed-regulating module and a flight control module are respectively embedded into a body of an aircraft, and keep sealed; a propeller is arranged on a brushless motor; the flight control module is connected with an air speed sensor which is positioned at the right upper end of the aircraft; a lithium polymer battery is arranged on a nose; a battery compartment cover covers the lithium polymer battery; a camera is adjacent to the lithium polymer battery; a camera compartment cover covers the camera. The general miniature unmanned aerial vehicle is high in self-detectivity on a barrier, small in size, light in weight, waterproof, high in integration degree and easy to take off, and can completely get rid of the intervention control from ground staff.

Description

technical field [0001] The invention relates to a miniature universal unmanned aircraft, in particular to an autonomous and practical miniature universal aircraft. Background technique [0002] Small and micro UAVs in active service cannot completely get rid of human intervention and control. During the take-off or landing process, ground personnel need to control the remote control to some extent. They cannot automatically avoid flight routes and cannot autonomously detect obstacles on the take-off and landing routes. There are great security risks. [0003] Traditional small and micro UAVs mostly have a tail layout, low thrust-to-weight ratio, and the length is mostly about 2m, and there are many other peripheral accessories. Therefore, take-off and landing places are greatly restricted. [0004] The integration of traditional UAVs is low, and the coordination between the airborne equipment is poor. Before taking off, the user must check whether each device is in working...

AI Technical Summary

Problems solved by technology

[0002] Small and micro UAVs in active service cannot completely get rid of human intervention and control. During the take-off or landing process, ground personnel need to control the remote control to some extent. They cannot automatically avoid flight routes and cannot autonomously detect obstacles on the take-off and landing routes. There are great security risks in

[0003] Traditional small and micro UAVs mostly have a tail layout, low thrust-to-weight ratio, and the length is mostly about 2m, and there are many other peripheral accessories. Therefore, take-off and landing places are greatly restricted

[0004] The integration of traditional UAVs is low, and the coordination between the airborne equipment is poor. Before taking off, the user must check whether each device is in working condition, whether each switch is in the correct position, etc. A slight negligence will lead to this take-off and landing. have an accident

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