Wind resistant cube unmanned aerial vehicle device and control method

A cube and UAV technology, applied in three-dimensional position/channel control, vehicle position/route/altitude control, attitude control and other directions, can solve the problems of inconvenient maintenance, high damage failure rate, poor wind resistance, etc. Good protection, solve the complex control, improve the effect of wind resistance

Inactive Publication Date: 2016-12-21
IANGSU COLLEGE OF ENG & TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] Purpose of the invention: the purpose of the present invention is to overcome the deficiencies in the structure design and control method of the existing multi-rotor UAV, and by designing a cube-shaped multi-rotor UAV device with an outer cover buffer pad, it can effectively solve the problem of the multi-rotor UAV in the air. Defects such as difficult operation, inconvenient maintenance, poor wind resistance, high damage failure rate, etc.

Method used

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  • Wind resistant cube unmanned aerial vehicle device and control method
  • Wind resistant cube unmanned aerial vehicle device and control method
  • Wind resistant cube unmanned aerial vehicle device and control method

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Embodiment Construction

[0025] Such as Figure 1 to Figure 3 A kind of wind-resistant cubic unmanned aerial vehicle device as shown, comprises the cube body that is made of six shell panels 1, each corner and edge of described body outer cube all wraps outer cover cushion 5, makes unmanned aerial vehicle regardless of From which angle it lands, it can be effectively protected by the cushion. The thickness of the cube UAV cover buffer pad 5 exceeds the height of the propellers on each plane of the UAV, ensuring the safety protection of each propeller when landing. Each shell panel 1 is provided with a through hole, and the through hole is provided with a propeller 2 and a propeller motor 4, and each propeller motor 4 is connected to the flight control box 6 at the center of the cube through a support rod 3, the flight control box 6 A UAV flight intelligent control module is installed inside.

[0026] A propeller 2 and a propeller motor 4 are installed outside each UAV shell panel, so that there are ...

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Abstract

The invention discloses a wind resistant cube unmanned aerial vehicle device and a control method. The wind resistant cube unmanned aerial vehicle device comprises a cube vehicle body composed of six shell panels. All corner angles and corner edges of an outer cube of the vehicle body are coated with outer cover buffer pads. Each shell panel is provided with a through hole provided with a propeller and a propeller motor. All propeller motors are connected with a flight control box in the center in the cube through support rods. An unmanned aerial vehicle flight intelligent control module is installed in the flight control box. According to the wind resistant cube unmanned aerial vehicle device and the control method, through the adoption of the cube-shaped multi-rotor unmanned aerial vehicle device with the outer cover buffer pads, the defects of large manipulation difficulty, inconvenient maintenance, poor wind resistance, the high damage and fault rate and the other aspects of a multi-rotor unmanned aerial vehicle can be overcome.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle and a control method thereof, in particular to a wind-resistant cubic unmanned aerial vehicle device and a control method thereof. Background technique [0002] At present, the application of UAVs in aerial photography, detection, reconnaissance and other tasks has made great progress. Its outstanding advantages such as easy operation, low flight and maintenance costs, and high work efficiency have been widely recognized. Among the main types of UAVs, fixed-wing UAVs have their specific limitations, such as flight site requirements and performance limitations such as poor low-speed performance. In contrast, multi-rotor drones have the advantages of small size and mass, good concealment and safety, flexible vertical take-off and landing, low flying height, strong maneuverability, simple structure, flexible operation, and low cost. [0003] Ordinary multi-rotor UAVs used for aerial photography, detect...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/08B64C1/00G05D1/08G05D1/10
CPCG05D1/0808G05D1/0816G05D1/101B64C1/068B64C27/08B64C2001/0045B64U10/10
Inventor 孙兵
Owner IANGSU COLLEGE OF ENG & TECH
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