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Flight control method and system for unmanned aerial vehicle cluster under fault condition

A UAV and swarm technology, applied in the field of flight control, can solve the problems of poor control effect and single control function, and achieve the effect of reducing losses, solving disconnection, and enriching the possibility of operation.

Pending Publication Date: 2021-10-01
HEBEI UNIVERSITY OF SCIENCE AND TECHNOLOGY
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Embodiments of the present invention provide a flight control method and system for unmanned aerial vehicle clusters under fault conditions to solve the problems of single control function and poor control effect in the control mode of unmanned aerial vehicle clusters

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  • Flight control method and system for unmanned aerial vehicle cluster under fault condition
  • Flight control method and system for unmanned aerial vehicle cluster under fault condition
  • Flight control method and system for unmanned aerial vehicle cluster under fault condition

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Embodiment Construction

[0050] In the following description, specific details such as specific system structures, techniques such as specific system structures, such as specific system structures are presented in order to illustrate, in order to thorns the embodiments of the present invention. However, those skilled in the art will appreciate that the present invention may be implemented in other embodiments without these specific details. In other cases, detailed description of well-known systems, devices, circuits, and methods is omitted to prevent unnecessary details to prevent the description of the present invention.

[0051] In order to make the objects, technical solutions, and advantages of the present invention, the following will be described with reference to the accompanying drawings.

[0052] With the continuous development of military theory of various countries and the rapid development of modern science and technology, the role of drone is increasingly discovered, and its unique value is ...

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Abstract

The invention provides a flight control method and system for an unmanned aerial vehicle cluster under a fault condition. The method comprises the steps that a ground platform terminal periodically monitors the operation state of each unmanned aerial vehicle; when the target unmanned aerial vehicle is monitored, the ground platform terminal judges whether to establish a remote connection channel with the target unmanned aerial vehicle through a preset remote desktop program, wherein the operation state of the target unmanned aerial vehicle is a fault state; if yes, the ground platform terminal sends the control information to the target unmanned aerial vehicle through the remote connection channel; and the target unmanned aerial vehicle executes a flight action corresponding to the control information. The control effect of the unmanned aerial vehicle cluster can be improved.

Description

Technical field [0001] The present invention relates to the field of drone technology, and more particularly to a flight control method and system of drone clusters under fault conditions. Background technique [0002] With the continuous development of military theory and the rapid development of modern science and technology, drones showed its importance in military fields and civilian fields, which have attracted extensive attention from researchers of various countries, especially in civilians, such as traffic monitoring and geology. Exploration, agricultural plant protection, high-altitude operation, etc., the market demand of drone continues to expand. Due to the diversity of flight tasks and the uncertainty of the environment, flight tasks are usually implemented in the form of a unmanned cluster. [0003] At present, the control method of drone clusters, there is a problem of single function, poor control effect. Inventive content [0004] Embodiments of the present inve...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/104
Inventor 邵士凯赵新福赵渊洁
Owner HEBEI UNIVERSITY OF SCIENCE AND TECHNOLOGY
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