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Unmanned aerial vehicle control method and device

A control method and control device technology, applied in the field of unmanned aerial vehicles, can solve the problems of unmanned aerial vehicle flight controllers with high control technology requirements and inability to achieve precise control, so as to achieve the effect of reducing control technical requirements and precise control

Inactive Publication Date: 2015-12-23
SHENZHEN AEE AVIATION TECH
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  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

[0003] The main purpose of the present invention is to provide a control method and device for unmanned aerial vehicles, aiming to solve the problem that the altitude-fixed flight function of the prior art unmanned aerial vehicles requires very high control technology for the flight controller, and precise control cannot be achieved.

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  • Unmanned aerial vehicle control method and device

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Embodiment Construction

[0023] It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0024] Such as figure 1 As shown, an unmanned aerial system is provided. The unmanned aerial system includes a controller 100 and a drone 200 .

[0025] The UAV 200 mainly refers to an unmanned aircraft, which may include a fuselage, a wing, and a driving device, a communication device, a power supply, etc. in the fuselage. The wireless communication device is used for communication between the UAV 200 and the controller 100 . The communication device is used to send the current flight status of the UAV 200, such as flight direction, flight altitude, flight speed, power supply status, etc. to the controller 100, and the controller 100 is used to send control instructions or pre-planned routes to UAV 200, so that the driving device of UAV 200 controls the flight of UAV 200 according to the control instruction, or ca...

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Abstract

The invention discloses an unmanned aerial vehicle (UAV) control method comprising the steps of making a UAV enter a fixed-height flight mode, acquiring the current flight height of the UAV, and controlling flight of the UAV according to the current flight height and the flight height set for the fixed-height flight mode. The invention further discloses a UAV control device. Automatic fixed-height flight is realized only by setting the fixed-height flight mode. The requirement on the control technology of flight controllers is lowered, and precise control is realized.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a control method and device for an unmanned aerial vehicle. Background technique [0002] UAVs refer to unmanned aircraft controlled by wireless remote control equipment and their own control devices, such as unmanned helicopters, unmanned fixed-wing aircraft, unmanned paragliders, etc. The UAV can be used to mount a shooting device for aerial photography, surveying and mapping, reconnaissance and so on. When the UAV is working, it can realize the fixed-altitude flight of the UAV, but the fixed-altitude flight of the UAV is through the controller to first adjust the flying height of the UAV, and then control the flight of the UAV after the current adjustment. flight altitude. This requires very high control technology for the flight controller, so that the drone's altitude-fixed flight function cannot be widely used, and precise control cannot be achieved. Contents of ...

Claims

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Application Information

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IPC IPC(8): G05D1/10
Inventor 张显志
Owner SHENZHEN AEE AVIATION TECH
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