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Anti-yaw control method and device for unmanned aerial vehicle, control equipment and unmanned aerial vehicle

A technology of yaw control and unmanned aerial vehicles, applied in the field of unmanned aerial vehicles, can solve problems such as flight accidents, inconvenient understanding and calculation, and inability to successfully complete inspection and shooting tasks, so as to improve accuracy and control effect Effect

Active Publication Date: 2021-04-16
北京云圣智能科技有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, when multi-rotor UAVs perform flight guidance, they usually control the flight based on the geometric relationship between the UAV and the route in space. It is also difficult to overlap the route, and it is difficult to obtain a better control effect, so that the inspection and shooting tasks cannot be successfully completed. When the UAV cannot fly strictly according to the route, it is easy to cause serious damage to the UAV without the obstacle avoidance function. flight accident

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  • Anti-yaw control method and device for unmanned aerial vehicle, control equipment and unmanned aerial vehicle
  • Anti-yaw control method and device for unmanned aerial vehicle, control equipment and unmanned aerial vehicle
  • Anti-yaw control method and device for unmanned aerial vehicle, control equipment and unmanned aerial vehicle

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Embodiment Construction

[0023] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. The components of the embodiments of the invention generally described and illustrated in the figures herein may be arranged and designed in a variety of different configurations.

[0024] Accordingly, the following detailed description of the embodiments of the invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but merely represents selected embodiments of the invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art wi...

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Abstract

The invention provides an anti-yaw control method and device for an unmanned aerial vehicle, control equipment and the unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The method comprises the steps: obtaining a targe route, wherein the target route comprises an initial waypoint; establishing a preset conversion coordinate system at the initial waypoint, and determining first direction information of the preset conversion coordinate system relative to the navigation coordinate system; determining second direction information of a preset fuselage horizontal coordinate system relative to a preset conversion coordinate system based on the first direction information; and determining a target flight speed of unmanned aerial vehicle route flight based on the second direction information so as to execute an unmanned aerial vehicle flight task on the target route according to the target flight speed. According to the invention, the anti-yawing control effect of the unmanned aerial vehicle is better improved, so that the flight accuracy of the unmanned aerial vehicle along the target route is improved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an anti-yaw control method, device, control device and unmanned aerial vehicle. Background technique [0002] With the rapid development of drones today, the demand for automatic flight of drones is getting higher and higher. The most common in automatic flight is route flight, that is, to plan a series of waypoints in three-dimensional space for the UAV in advance, and to design the tasks of the UAV in flight, such as flight speed, shooting angle, arrival time, etc. Dwell time after waypoint, etc. [0003] At present, when multi-rotor UAVs perform flight guidance, they usually control the flight based on the geometric relationship between the UAV and the route in space. It is also difficult to overlap the route, and it is difficult to obtain a better control effect, so that the inspection and shooting tasks cannot be successfully completed. When the UAV cannot...

Claims

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Application Information

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IPC IPC(8): G05D1/08G05D1/10
Inventor 陈方平倪学斌高明覃光勇
Owner 北京云圣智能科技有限责任公司
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