An unmanned aerial vehicle and a flight control assembly thereof

Abstract

The invention relates to the technical field of unmanned aerial vehicles (UAVs), and discloses an UAV and a flight control assembly thereof, wherein, the flight control assembly comprises a flight control assembly, wherein, the flight control assembly comprises a flight control module and a mounting plate arranged on the UAV, and the flight control module is mounted on the mounting plate through asnap structure. Through the method, the flight control module and the mounting plate of the flight control module can be conveniently disassembled and assembled, and the efficiency is high.

Description

【Technical field】 [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle and its flight control components. 【Background technique】 [0002] UAV is a complex system covering multidisciplinary fields such as flight control, visual algorithm, and PTZ control. The modularization and standardization of each functional subsystem is conducive to accelerating the research and development and manufacturing process of UAVs, and facilitates later use and cooperation. maintain. [0003] The flight control module (hereinafter collectively referred to as the flight control module) is an important subsystem in the UAV system. Its main function is to measure the status information such as the flight attitude of the UAV, and to control the flight of the UAV in real time. In order to ensure the accuracy of the measurement, after the drone is installed with the flight control module, the calibration and calibration of the f...

AI Technical Summary

Problems solved by technology

The glue-type installation scheme has low reliability, while the screw-fixed installation scheme improves reliability, but it still cannot guarantee the positioning accuracy of the flight control module in the mass production assembly process

That is, in mass production, the installation positions of the flight control modules in different UAVs cannot be guaranteed to be exactly the same

Therefore, for each UAV in mass production, it takes a lot of time to calibrate and calibrate the flight control module, which undoubtedly reduces the assembly efficiency

And in the use and maintenance of the flight control module in the later stage, it is impossible to achieve "one calibration and calibration, multiple loading and unloading maintenance"

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