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A method and device for trajectory planning of an unmanned aerial vehicle

A trajectory planning and unmanned aerial vehicle technology, which is applied in three-dimensional position/course control, vehicle position/route/height control, complex mathematical operations, etc., can solve problems such as low efficiency and large amount of calculation, so as to improve efficiency and reduce calculation volume effect

Active Publication Date: 2022-03-29
BEIJING UNIV OF POSTS & TELECOMM +1
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Problems solved by technology

[0005] Embodiments of the present invention provide a UAV trajectory planning method and device, which are used to solve the defects of large amount of calculation and low efficiency in the UAV trajectory design process in the prior art, and realize the reduction of calculation in the UAV trajectory planning process. The purpose of improving the efficiency of UAV trajectory planning

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  • A method and device for trajectory planning of an unmanned aerial vehicle
  • A method and device for trajectory planning of an unmanned aerial vehicle
  • A method and device for trajectory planning of an unmanned aerial vehicle

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Embodiment Construction

[0034] 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. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0035] This method proposes to perform function fitting on the trajectory of the UAV, and obtain the corresponding trajectory of the UAV by designing the fitting coefficient. Compared with the traditional method, the design variable scale of this method is small and constant, and does not increase with the flight time and flight distance of the UA...

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Abstract

An embodiment of the present invention provides a UAV trajectory planning method and device. The method includes: decomposing the trajectory variable of the UAV in a mission cycle in a Cartesian coordinate system to obtain trajectory variable components in three directions; based on The trajectory variable component obtains a fitting coefficient of the fitting trajectory variable; based on the fitting coefficient, the UAV trajectory is planned. By decomposing the trajectory variable of the UAV in the Cartesian coordinate system to obtain the trajectory variable components in three directions, and obtaining the fitting coefficient of the fitting trajectory variable, the trajectory of the UAV is planned according to the fitting coefficient , which reduces the amount of calculation in the process of UAV trajectory planning and improves the efficiency of UAV trajectory planning.

Description

technical field [0001] The invention relates to the technical field of UAV trajectory planning, in particular to a UAV trajectory planning method and device. Background technique [0002] UAVs are widely used in auxiliary communication scenarios due to their advantages such as mobility and high flexibility. Compared with the traditional facility communication system, a key issue of UAV-assisted communication system is how to design the flight trajectory of UAV to obtain better communication performance. The UAV trajectory design problem is generally solved by modeling to obtain the maximum utility function value, but it is very difficult to design the UAV trajectory with the largest utility function, because the UAV trajectory is a continuous function of time and contains infinitely many design variables . [0003] Existing solutions are to discretize the continuous trajectory into a limited number of discrete trajectory variables, and assume that the position of the UAV i...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10G06F17/17
CPCG05D1/101G06F17/17
Inventor 郭一珺李敬华郝建军尹斯星张志龙何欣欣尹长川刘丹谱罗涛李剑峰
Owner BEIJING UNIV OF POSTS & TELECOMM
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