Structure design method of refined waypoint based on multi-circuit tower

A technology of refined aviation and structural design, applied in the field of transmission line towers and unmanned aerial vehicles, can solve the problems of route waste, inconvenient data organization, route data, image data management, etc., so as to reduce excessive route waste, simplify and avoid route redundancy. Effect

Pending Publication Date: 2022-03-29
江苏卓月云智能科技有限公司
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the problem that the current existing technology mainly uses the electric tower as a whole to form the route, which is not convenient for the management of route data and image data in data organization, and causes excessive waste of route in actual flight, etc., and proposes a Structural design method of refined waypoint based on multi-echo tower

Method used

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  • Structure design method of refined waypoint based on multi-circuit tower
  • Structure design method of refined waypoint based on multi-circuit tower
  • Structure design method of refined waypoint based on multi-circuit tower

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Effect test

Embodiment 1

[0020] refer to Figure 1-2 , a method for structural design of refined waypoints based on multi-echo towers, including the following steps:

[0021] S1: Design type method: design different waypoint types, and randomly split and combine flight routes of multiple loop tower routes, wherein the waypoint types are divided into first-level split points, second-level split points, and turning points Waypoints and task waypoints, the route types are divided into forward route and return route;

[0022] S2: Design split points: Design the first-level split point design and the second-level split point design, and perform the first-level split point design, where the first-level split points are divided according to the direction of public parts and non-public parts, and the first-level split point There are two levels of split points under the split point, the second level split points of public components are associated with public components, and the second level split points of ...

Embodiment 2

[0025] refer to Figure 1-2 , a method for structural design of refined waypoints based on multi-echo towers, including the following steps:

[0026] S1: Design type method: design different waypoint type methods, and randomly split and combine flight routes for each route of multiple loop towers;

[0027] S2: Design split points: Design the first-level split point design and the second-level split point design, and perform the first-level split point design, where the first-level split points are divided according to the direction of public parts and non-public parts, and the first-level split point There are two levels of split points under the split point, the second level split points of public components are associated with public components, and the second level split points of non-public components are associated with one or more lines in this direction;

[0028] S3: Design route: After the split point design is completed, design turning waypoints and mission waypoints...

Embodiment 3

[0030] refer to Figure 1-2 , a method for structural design of refined waypoints based on multi-echo towers, including the following steps:

[0031] S1: Design type method: design different waypoint types, and randomly split and combine flight routes of multiple loop tower routes, wherein the waypoint types are divided into first-level split points, second-level split points, and turning points Waypoints and task waypoints, the route types are divided into forward route and return route;

[0032] S2: Design split point: Design the first-level split point design and the second-level split point, carry out the first-level split point design, and set the second-level split point under the first-level split point;

[0033] S3: Design route: After the split point design is completed, design turning waypoints and mission waypoints to form the forward route according to the component shooting sequence and waypoint design rules, and after all mission waypoints and turning waypoints ...

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Abstract

The invention relates to the technical field of unmanned aerial vehicles and power transmission line towers, in particular to a structure design method of refined waypoints based on a multi-circuit electric tower, and aims to solve the problems that in the prior art, an electric tower is mainly used as a whole to form a route, route data and image data management is inconvenient in data organization, and the data organization is inconvenient. In order to solve the problem of excessive wastage of the route in actual flight, the invention provides the following scheme which comprises the following steps: S1, designing a type mode, S2, designing a splitting point and S3, designing the route, the invention aims to solve the problems of storage and classification of multi-circuit tower line data through an improved method, simplify a flight path to avoid route redundancy, and improve the reliability of the multi-circuit tower line data storage and classification. And the excessive wastage of the route caused in the actual flight is reduced.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles and transmission line towers, in particular to a method for structural design of refined waypoints based on multi-circuit towers. Background technique [0002] The full name of UAV is "unmanned aerial vehicle", and the English abbreviation of "Unmanned Aerial Vehicle" is "UAV". It is an unmanned aircraft controlled by radio remote control equipment and its own program control device. It involves sensor technology, communication technology, information processing technology, intelligent control technology and aerodynamic propulsion technology, etc., and is a product of high-tech content in the information age. The value of UAVs lies in forming an aerial platform, combining with other components to expand applications, and replacing humans to complete aerial operations. With the gradual maturity of UAV research and development technology and the significant reduction in manufacturi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 王楠王银王皓梁爽
Owner 江苏卓月云智能科技有限公司
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