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High-precision unmanned aerial vehicle flight control system

A flight control system and UAV technology, applied in aircraft, information technology support systems, motor vehicles, etc., can solve problems such as unmanned aerial vehicles cannot be charged, UAV inspection radius restrictions, etc., to increase the voyage and inspection radius, The effect of reducing my time cost and labor cost

Inactive Publication Date: 2019-07-30
SUN HAWK HENAN AVIATION IND CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Based on the above problems, the present invention provides a high-precision unmanned aerial vehicle flight control system, which is used to solve the problem that the existing unmanned aerial vehicle cannot be charged halfway, which leads to the limitation of the inspection radius of the unmanned aerial vehicle

Method used

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  • High-precision unmanned aerial vehicle flight control system
  • High-precision unmanned aerial vehicle flight control system
  • High-precision unmanned aerial vehicle flight control system

Examples

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Embodiment 1

[0026] Such as Figure 1-4 As shown, the high-precision UAV flight control system includes a charging base station system and a fuselage docking system. The charging base station system includes a matrix landing platform 1, and a plurality of rechargeable grids 2 are installed on the matrix landing platform 1. Each grid A charging power supply 3 is connected to the grid 2; the fuselage docking system includes a plurality of belly contacts 4 installed on the bottom surface of the fuselage and capable of docking with the grid 2.

[0027] In the present invention, the staff is required to establish a matrix landing platform 1 connected to the charging power supply 3 at an appropriate position in advance, and install a plurality of belly contacts 4 that can be docked with the grid 2 on the bottom surface of the fuselage; When there is almost no power, the staff can remotely control the UAV to land on the matrix landing platform 1, dock with the grid 2 through the belly contact 4, ...

Embodiment 2

[0030] Such as Figure 1-4 As shown, the high-precision UAV flight control system includes a charging base station system and a fuselage docking system. The charging base station system includes a matrix landing platform 1, and a plurality of rechargeable grids 2 are installed on the matrix landing platform 1. Each grid A charging power supply 3 is connected to the grid 2; the fuselage docking system includes a plurality of belly contacts 4 installed on the bottom surface of the fuselage and capable of docking with the grid 2.

[0031] In this embodiment, the shape of the grid 2 is square, and the polarity of the electrodes in each grid 2 is the same, so that each side length of the grid 2 can be equal, which helps the belly contact 4 to be connected to the grid 2. butt.

[0032] Preferably, the distance between two adjacent fuselage contacts 4 is greater than the length of the diagonal of a single grid 2, which can ensure that the two fuselage contacts 4 will not land in the...

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Abstract

The invention relates to the technical field of unmanned aerial vehicle charging, in particular to a high-precision unmanned aerial vehicle flight control system which is used for solving the problemthat the patrol radius of an existing unmanned aerial vehicle is limited because the unmanned aerial vehicle cannot be charged halfway. The high-precision unmanned aerial vehicle flight control systemcomprises a charging base station system and a vehicle body docking system, wherein the charging base station system comprises a matrix landing platform, a plurality of grids are installed on the matrix landing platform, and a charging power supply is connected in each grid; and the vehicle body docking system includes a plurality of vehicle belly contacts mounted on the bottom surface of the vehicle body and capable of docking with the grids. According to the high-precision unmanned aerial vehicle flight control system, the matrix landing platform is established at an appropriate position, when the unmanned aerial vehicle is almost out of power, the unmanned aerial vehicle can be remotely controlled to land on the matrix landing platform for charging, so that the unmanned aerial vehicledoes not need to return for charging, thus the patrol radius of the unmanned aerial vehicle is larger, and the range that the unmanned aerial vehicle can travel is longer.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicle charging, and more specifically relates to a high-precision unmanned aerial vehicle flight control system. Background technique [0002] UAV is an unmanned aircraft operated by radio remote control equipment and self-contained program control device, or completely or intermittently operated autonomously by on-board computer. UAV can be divided into military and civilian according to the application field. For military use, drones are divided into reconnaissance aircraft and target drones; for civilian use, drones plus industry applications are the real rigid needs of drones; currently, they are used in aerial photography, agriculture, plant protection, miniature selfies, express transportation, disaster relief, and observation Applications in fields such as wild animals, infectious disease monitoring, surveying and mapping, news reports, power inspections, disaster relief, film and...

Claims

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Application Information

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IPC IPC(8): B64F1/00B60L53/14
CPCB64F1/00B60L53/14B60L2200/10Y02T90/167Y02T10/70Y02T90/14Y02T10/7072Y04S30/12
Inventor 李文明
Owner SUN HAWK HENAN AVIATION IND CO LTD