Control device of unmanned aerial vehicle and unmanned aerial vehicle

A technology of unmanned aerial vehicle and control device, applied in the field of unmanned aerial vehicle, can solve the problems of large influence of control device and low degree of integration, and achieve the effect of improving the degree of integration, avoiding wrong interface insertion, and improving accuracy

Active Publication Date: 2018-09-21
SHANGHAI TOPXGUN ROBOT CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The object of the present invention is to provide a control device for an unmanned aerial vehicle to solve the problems that the existing unmanned aerial vehicle control device has a low degree of integration and vibration has a great influence on the control device

Method used

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  • Control device of unmanned aerial vehicle and unmanned aerial vehicle
  • Control device of unmanned aerial vehicle and unmanned aerial vehicle
  • Control device of unmanned aerial vehicle and unmanned aerial vehicle

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Embodiment Construction

[0040] The technical solutions of the present invention will be further described below in conjunction with the accompanying drawings and through specific implementation methods.

[0041] The invention provides a control device for an unmanned aerial vehicle, such as figure 1 As shown, the control device includes a housing, an interface plug-in 2, an inertial measurement device 3, a flight control main circuit board 4, an interface soft board 5 and a limit frame 6, wherein:

[0042] Above-mentioned shell comprises upper shell 1 and bottom cover 7, as figure 2 with image 3 As shown, the four corners of the upper case 1 and the bottom cover 7 are provided with connection holes, and the upper case 1 and the bottom cover 7 can be fixedly connected by connecting pieces through the connection holes of the upper case 1 and the bottom cover 7 .

[0043] The above-mentioned upper shell 1 is arranged in an internal hollow structure, such as figure 2 As shown, two limiting bosses 1...

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Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and discloses a control device for an unmanned aerial vehicle, which includes a casing, an inertial measurement device fixed in the casing, a flight control main circuit board electrically connected to the inertial measurement device, and a flight control main circuit board electrically connected to the The main circuit board of the flight control and the interface soft board that is close to the inner wall of the housing, and the two sides of the interface soft board pass through the housing and are electrically connected to external devices. The invention also discloses an unmanned aerial vehicle comprising the control device. The present invention adopts the above-mentioned structural arrangement, which makes the structure of each component compact, improves the integration degree of the whole control device, reduces the influence of vibration on the inertial measurement device, and improves the measurement stability of the inertial measurement device. The interface soft board is pasted in the shell, and the interface soft board integrates multiple existing interface boards that are separately set up, which can improve the stability of its installation in the shell, and can be folded at will, saving installation space and reducing the overall size. The volume of the control device.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a control device for an unmanned aerial vehicle and the unmanned aerial vehicle. Background technique [0002] An unmanned aerial vehicle is an unmanned aerial vehicle operated by radio remote control equipment or its own program control device. At present, with the development of science and technology, the technology of unmanned aerial vehicles is becoming more and more mature, and unmanned aerial vehicles are widely used due to their fast speed and flexible operation. [0003] During the flight of the unmanned aerial vehicle, the control device is required to control and navigate it. The control device controls the attitude of the unmanned aerial vehicle and feeds back the position of the unmanned aerial vehicle to realize the attitude control and positioning functions of the unmanned aerial vehicle. The existing UAV control device usually analyzes the attitu...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0808G05D1/101H05K1/148H05K2201/10303H05K7/1417H05K3/4691H05K2201/047H05K2201/056H05K2201/042B64U2201/00B64C39/024H05K1/14
Inventor 尹亮亮高廉洁李少斌张羽
Owner SHANGHAI TOPXGUN ROBOT CO LTD
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