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Unmanned aerial vehicle control method

A control method, UAV technology, applied in directions such as non-electric variable control, control/regulation system, 3D position/channel control, etc., which can solve the problem of large airframe resistance, airframe tilt, UAV flight speed and endurance time Adverse effects and other problems, to achieve the effect of reducing labor intensity and reducing resistance

Pending Publication Date: 2021-05-14
尚良仲毅(沈阳)高新科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] However, when flying forward, the fuselage is tilted, causing the fuselage to generate greater resistance, which in turn has an adverse effect on the flight speed and endurance of the drone.

Method used

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  • Unmanned aerial vehicle control method
  • Unmanned aerial vehicle control method
  • Unmanned aerial vehicle control method

Examples

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Embodiment Construction

[0068] The core of the present invention is to provide a UAV control method, which reduces the labor intensity of the user in the UAV cruise mode while reducing the resistance generated by the fuselage when the UAV is in the cruise mode.

[0069] In order to enable those skilled in the art to better understand the technical solutions of the present invention, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0070] Please refer to Figure 1 to Figure 12 .

[0071] In a specific implementation, the UAV control method provided by a specific embodiment of the present invention includes the steps of:

[0072] Set the flight mode of the drone through the control system. The specific control system can be set on the fuselage of the drone.

[0073] The flight mode includes a cruise mode and a work mode. In the cruise mode, the upward extension direction of the propeller axis of the drone is an acute ang...

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PUM

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Abstract

The invention discloses an unmanned aerial vehicle control method. The method comprises the steps that the flight mode of an unmanned aerial vehicle is set through a control system; the flight mode comprises a cruising mode and a working mode, in the cruising mode, the included angle between the upward extending direction of the propeller axis of the unmanned aerial vehicle and the flying front horizontal plane of the unmanned aerial vehicle is an acute angle, and the fuselage of the unmanned aerial vehicle is horizontally arranged; and a flight path is planned before the unmanned aerial vehicle flies to the preset area, and the cruising mode is adopted before the unmanned aerial vehicle reaches the preset area. As the included angle between the upward extending direction of the propeller axis of the unmanned aerial vehicle in the cruise mode and the horizontal plane in front of the flying unmanned aerial vehicle is the acute angle, the inclination angle of the fuselage does not need to be actively adjusted, and the resistance generated by the fuselage in the flying process of the unmanned aerial vehicle in the cruise mode is effectively reduced. The flight path is planned before the unmanned aerial vehicle flies to the preset area, and the unmanned aerial vehicle adopts the cruise mode without manual operation before reaching the preset area, so that the labor intensity of a user in the cruise mode of the unmanned aerial vehicle is effectively reduced.

Description

technical field [0001] The invention relates to the technical field of UAV flight control, in particular to a UAV control method. Background technique [0002] The traditional drone mainly makes the drone fly forward by controlling the forward tilt of the fuselage. In the specific drone control method. [0003] However, when flying forward, the fuselage is tilted, causing the fuselage to generate greater resistance, which in turn has an adverse effect on the flight speed and endurance of the drone. And during the cruising process, staff are required to transmit control signals to the UAV to control the flight status of the UAV. [0004] Therefore, how to reduce the labor intensity of the user while reducing the resistance generated by the fuselage when the drone is in cruise mode is a technical problem to be solved urgently by those skilled in the art. Contents of the invention [0005] The object of the present invention is to provide a method for controlling a UAV, whi...

Claims

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Application Information

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IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 陈明非姜文辉丛闯闯吴成东张贺冀诗瑶
Owner 尚良仲毅(沈阳)高新科技有限公司
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