Controlling method and system for unmanned aircrafts

A technology of unmanned aerial vehicle and control method, which is applied in three-dimensional position/course control and other directions, and can solve problems such as safety accidents of unmanned aerial vehicles

Inactive Publication Date: 2016-07-27
高域(北京)智能科技研究院有限公司
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  • Application Information

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Problems solved by technology

[0010] The embodiment of the present invention provides a control method and system for an unmanned aerial vehicle, which is used to solve the problem in the prior art that the unmanned aerial vehicle performs take-off and landing behavior at the same place, which leads to the safety accident of the unmanned aerial vehicle

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  • Controlling method and system for unmanned aircrafts
  • Controlling method and system for unmanned aircrafts
  • Controlling method and system for unmanned aircrafts

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Embodiment Construction

[0048] An embodiment of the present invention provides a method for controlling an unmanned aerial vehicle. The method includes: when receiving the landing information of the unmanned aerial vehicle, analyzing the position coordinates in the landing information, and detecting whether the position coordinates have been marked, and if so, Then send a control instruction prohibiting landing to the UAV; if not, send a control instruction allowing landing to the UAV. This avoids the problem of taking off and landing at the same site at the same time, thereby avoiding the occurrence of safety accidents of unmanned aerial vehicles.

[0049] The technical solutions of the present invention will be described in detail below through the accompanying drawings and specific embodiments. It should be understood that the embodiments of the present invention and the specific technical features in the embodiments are only descriptions of the technical solutions of the present invention, rather ...

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Abstract

The invention discloses a controlling method and a system for unmanned aircrafts. The method is performed through the following steps: decoding the position coordinates of a point contained in the landing information when receiving the landing information of an aircraft, detecting whether the position coordinates have been marked or not, and sending to the aircraft the controlling instruction of wave-off if the position coordinates are marked; and otherwise, sending to the aircraft the controlling instruction of landing. With such a system, the problem that aircrafts take off or land on ground at the same time at the same position can be addressed, therefore, unmanned aircraft accidents can be avoided.

Description

technical field [0001] The present application relates to the technical field of unmanned aerial vehicles, in particular to a control method and system for unmanned aerial vehicles. Background technique [0002] At present, when small and micro unmanned aerial vehicles, especially multi-rotor unmanned aerial vehicles, due to the vortex effect of the air flow, when the landing speed is not controlled properly, it is easy to cause the risk of crash or loss of control. Therefore, the automatic landing technology of small and micro unmanned aerial vehicles is very convenient. This automatic landing is mainly aimed at the control of the landing speed and the landing point, ensuring that the landing is carried out within a safe and rapid speed range, and at the same time ensuring that the landing is within a predetermined Area. [0003] In simple terms, the above-mentioned automatic landing technology can be that after the unmanned aerial vehicle flies to a certain position, it r...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/10
Inventor 谭圆圆
Owner 高域(北京)智能科技研究院有限公司
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