Multi-rotor unmanned aerial vehicle and multi-rotor unmanned aerial vehicle system

Abstract

The invention relates to a multi-rotor unmanned aerial vehicle, which comprises a vehicle body, a data acquisition assembly and a processing assembly, wherein the vehicle body comprises a rack, brushless motors, a propeller, a battery, an electronic speed controller and a flight control computer; the data acquisition assembly is used for acquiring environmental data of the operating environment ofthe multi-rotor unmanned aerial vehicle; and the processing assembly is used for processing the environmental data, determining the control logic of the multi-rotor unmanned aerial vehicle and sending the control logic to the flight control computer so as to control the multi-rotor unmanned aerial vehicle. According to the multi-rotor unmanned aerial vehicle, the environmental data of the operating environment of the multi-rotor unmanned aerial vehicle can be automatically acquired, the control logic of the multi-rotor unmanned aerial vehicle is determined according to the obtained operationenvironment data, the operation state of the multi-rotor unmanned aerial vehicle is controlled according to the control logic. The multi-rotor unmanned aerial vehicle can be automatically controlled according to the operation environment, and under the scene that long-time control is needed, the manpower cost does not need to be consumed, and risks caused by misoperation are avoided.

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 and a multi-rotor unmanned aerial vehicle system. Background technique [0002] Multi-rotor drones are a type of rotor drones. Multi-rotor drones are usually composed of multiple symmetrically distributed rotors and bodies. Multi-rotor drones are quite different from conventional helicopters. Conventional helicopters mainly provide lift through the main rotor, and realize forward, backward, climbing, landing and other movements by controlling the collective pitch and periodic pitch of the main rotor. The yaw control of conventional helicopters is generally realized by controlling the pitch of the tail rotor. Conventional helicopters usually require a complex transmission system to distribute the power of the whole machine between the main rotor and the tail rotor, and a steering gear to control the pitch of the ma...

AI Technical Summary

Problems solved by technology

[0004] The present invention provides a multi-rotor UAV and a multi-rotor UAV system, which are used to solve the problem that the current UAV is only manually controlled and made by the operator in the whole process, and some of the scenes need to be controlled for a long time, requiring more manpower. cost and there are technical problems with the risk of operational errors leading to work errors

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