Control device and method for integrated unmanned aerial vehicle (UAV) flight

Abstract

The invention discloses a control device and method for integrated unmanned aerial vehicle (UAV) flight. The control device comprises a data link communication unit, an acquisition unit, a processing unit and a control unit, wherein the data link communication unit is used for interacting with a ground station, acquiring a flight task of a UAV and monitoring the flight state of the UAV; the acquisition unit is used for acquiring current flight acceleration and angular speed of the UAV, static air pressure on the UAV, motion speed of the UAV relative to surrounding air, magnetic field intensity of geomagnetic field on the UAV and positioning information of the UAV; the processing unit is used for processing data acquired by the acquisition unit to acquire the flight attitude of the UAV, and comparing the flight attitude with the flight task received by the data link communication unit so as to give flight height, flight speed and flight direction which need to be adjusted by the UAV; and the control unit is used for controlling a steering engine controller of the UAV to adjust according to the flight height, flight speed and flight direction which need to be adjusted by the UAV and are given by the processing unit, so that the UAV meets the requirement of the flight task. The device and the method can effectively and quickly control the flight of the UAV.

Description

technical field [0001] The invention belongs to the technical field of automatic control, and further relates to a highly integrated control device and method for the flight of an integrated unmanned aerial vehicle. Background technique [0002] UAV is a low-cost, high-efficiency, and task-customizable aircraft. By carrying different loads, it can achieve various specified tasks. It overcomes the shortcomings of manned machines, harsh operating conditions, and complex life support systems. Since UAV flight control is a newly developed technology, the previous flight controllers have a wide variety of equipment and complex systems. In response to this market gap, an integrated UAV flight controller has been developed and designed for flight control of various UAVs. Contents of the invention [0003] The purpose of the present invention is to provide a control device and method for unmanned aerial vehicle flight, which fills the blank of small-scale integrated unmanned aer...

AI Technical Summary

Problems solved by technology

It overcomes the shortcomings of previous manned machines, harsh operating conditions, and complex life support systems.

Since UAV f

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