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

A control device and unmanned aerial vehicle technology, applied in the direction of attitude control, control/regulation system, non-electric variable control, etc., can solve the problems of complex life support system, harsh use conditions, complex system, etc., to reduce complexity and improve operation Simple, low-cost effects

Pending Publication Date: 2016-12-14
西安瑞日电子发展有限公司
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  • Application Information

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 flight control is a newly developed technology, the previous flight controllers have a wide variety of equipment and complex systems.

Method used

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

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Embodiment Construction

[0029] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0030] see figure 1 , is an integrated unmanned aerial vehicle flight control device provided by the present invention, the control device includes a data link communication unit, an acquisition unit, a processing unit and a control unit, and the data link communication unit and the acquisition unit are respectively connected to the The input end of the processing unit is connected, and the control unit is connected with the input end of the processing unit; specif...

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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...

Claims

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Application Information

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IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0808G05D1/101
Inventor 王浩
Owner 西安瑞日电子发展有限公司
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