Unmanned aerial vehicle

Abstract

The invention discloses an unmanned aerial vehicle. The unmanned aerial vehicle comprises a vehicle head area, a vehicle tail area, a battery bin, a pan-tilt camera module, a sensor module, a battery and two vehicle arms. The battery compartment is formed between the machine head area and the machine tail area, the pan-tilt camera module is arranged in the machine head area, the sensor module is arranged in the machine tail area, a battery is detachably installed in the battery compartment, and the two machine arms are movably connected to the two sides of the machine head area or the two sides of the battery compartment. The unmanned aerial vehicle is a miniaturized double-wing unmanned aerial vehicle, the two vehicle arms are arranged in a foldable mode, and the unmanned aerial vehicle is small and exquisite in structure, multiple in function module and capable of executing shooting tasks. The pan-tilt camera module and the sensor module of the unmanned aerial vehicle are separated through the battery compartment, so that signal interference of the pan-tilt camera module on the sensor module is avoided, and the flight control end of the unmanned aerial vehicle can timely and accurately obtain own state parameters.

Description

technical field [0001] The present application relates to the technical field of aircraft, in particular to an unmanned aerial vehicle. Background technique [0002] At present, UAV technology is developing faster and faster, and its application in aerial photography, monitoring and reconnaissance is becoming more and more common and urgent. [0003] The UAVs currently on the market, when they are large in size, have large blade spans and are not suitable for short-distance flying, so they do not have indoor flight capabilities and their use is limited. The miniature quadrotor UAVs sold on the market are small in size, and the folded size is roughly below 500cm^2. It is difficult to install GPS and other sensors, and it is not possible to install gimbal and camera modules, and its battery capacity is small. , and the flight time is less than 10 minutes. [0004] When the size of the drone is small, if the gimbal camera module and the sensor module are loaded on the drone, ...

AI Technical Summary

Problems solved by technology

[0003] The UAVs currently on the market, when they are large in size, have large blade spans and are not suitable for short-distance flying, so they do not have indoor flight capabilities and their use is limited.

The miniature quadrotor UAVs sold on the market are small in size, and the folded size is roughly below 500cm^2. It is difficult to install GPS and other sensors, and it is not possible to install gimbal and camera modules, and its battery capacity is small. , the flight time is less than 10 minutes

[0004] When the size of the drone is small, if the gimbal camera module and the sensor module are loaded on the drone, and the two are located close to each other, the lines in the gimbal camera module will interfere with each sensor module in the sensor module The induction signal of the UAV makes it impossible for the flight control terminal of the UAV to obtain the status information of the UAV in a timely and accurate manner, which is not conducive to the automatic control of the UAV itself, and also cannot give the user timely feedback on the status information of the UAV itself. Or feed back wrong information to the user, which seriously affects the user experience

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