Anti-falling unmanned aerial vehicle

Abstract

The invention relates to the technical field of unmanned aerial vehicles, and discloses an anti-falling unmanned aerial vehicle. The anti-falling unmanned aerial vehicle comprises an unmanned aerial vehicle body, a plurality of unmanned aerial vehicle arms circumferentially distributed on the unmanned aerial vehicle body, a first driving motor used for providing driving power for flight of the unmanned aerial vehicle, a second driving motor used for providing driving power for flight of the unmanned aerial vehicle, a first unmanned aerial vehicle blade arranged at one end of the first drivingmotor and used for driving the unmanned aerial vehicle to fly, a second unmanned aerial vehicle blade arranged at one end of the second driving motor and used for driving the unmanned aerial vehicle to fly, and a control panel arranged in the unmanned aerial vehicle body and used for independently controlling the start and stop of the first driving motor and the second driving motor. The unmannedaerial vehicle is provided with a dual-drive system, rotation of the first driving motor is independently controlled through the control panel, rotation of the second driving motor is independently controlled through the control panel, and the unmanned aerial vehicle is driven to fly, so that the flight reliability and safety of the unmanned aerial vehicle are improved, and falling accidents of the unmanned aerial vehicle are effectively prevented.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an anti-falling unmanned aerial vehicle. Background technique [0002] UAV is an unmanned aircraft operated by radio remote control equipment and self-contained program control device. There is no cockpit on board, but equipment such as autopilot and program control device are installed. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Under the radio control, it can take off like an ordinary aircraft or be launched into the air with a booster rocket, and it can also be taken into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the landing process of ordinary aircraft, and can also be recovered by remote control with a parachute or block, and can be used ...

AI Technical Summary

Problems solved by technology

[0003] In the existing technology, in most cases, there are many reasons for drone accidents. Due to problems such as long flight time and short equipment life, it is easy to cause the motor and ESC of the drone to stop (the ESC controls the motor) , and then the UAV crash accident occurred, resulting in property damage

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