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Control device of unmanned aerial vehicle and unmanned aerial vehicl

A technology of unmanned aerial vehicles and control devices, which is applied in the field of unmanned aerial vehicles, can solve the problems of large influence of control devices and low integration degree, and achieve the effects of improving the integration degree, avoiding wrong interface insertion, and improving accuracy

Active Publication Date: 2017-06-27
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 vehicl
  • Control device of unmanned aerial vehicle and unmanned aerial vehicl
  • Control device of unmanned aerial vehicle and unmanned aerial vehicl

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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 and 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 of an unmanned aerial vehicle. The control device comprises a housing, an inertial measurement device fixed within the housing, a flight control main circuit board electrically connected with the inertial measurement device, and an interface soft board electrically connected to the flight control main circuit board and tightly attached to the inner wall of the housing. The two sides of the interface soft board pass through the housing to be electrically connected to an external device. The invention further discloses an unmanned aerial vehicle provided with the above control device. According to the invention, based on the above structural arrangement, all parts are compact in structure, and the integration degree of the whole control device is improved. The influence of the shock to the inertial measurement device is reduced and the measurement stability of the inertial measurement device is improved. The interface soft board is attached inside the housing, and all split type interface boards are integrated as one piece by the interface soft board. Therefore, the installation stability of the interface soft board inside the housing is improved. Meanwhile, the interface soft board can be freely folded, and the interface space is saved. The volume of the entire control device is reduced.

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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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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