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A suspended UAV debugging device

An unmanned aerial vehicle (UAV) and suspension type technology is applied in the field of suspension type UAV debugging device, which can solve the problems that the UAV debugging platform cannot better simulate the flying condition of the UAV and the debugging is not comprehensive, so as to achieve the purpose of experiment and power supply. Safe and convenient, material saving, wide range of environmental effects

Active Publication Date: 2021-07-02
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0006] In view of this, the present invention provides a suspended UAV debugging device to solve the problem that the existing UAV debugging platform cannot better simulate the flight status of the UAV, so that the debugging is not comprehensive

Method used

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  • A suspended UAV debugging device
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  • A suspended UAV debugging device

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Embodiment Construction

[0028] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only for illustration and are not intended to limit the present invention.

[0029] The present invention provides a suspended unmanned aerial vehicle debugging device, such as Figure 1 ~ Figure 3 As shown, it includes: a slip ring structure 1, a bracket 2 and a fixed part 3; where,

[0030] The support 2 includes a hollow bent strut 4, a plurality of end-to-end hollow straight struts 5 and a plurality of hollow connecting shafts 6; two adjacent straight struts 5 are hinged by connecting shafts 6, and are located between two Among the two straight struts 5 at the end, one straight strut 5 is hingedly connected with the bent strut 4 through the connecting shaft 6, and the other straight strut 5 is fixedly connected with the fix...

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Abstract

The invention discloses a suspension type unmanned aerial vehicle debugging device, which uses a slip ring to connect the unmanned aerial vehicle, and the slip ring is in a hanging state, so that the unmanned aerial vehicle is suspended in the air. A certain degree of freedom, in this way, on the premise of ensuring the double safety of personnel and UAVs, the flight status of UAVs can be simulated to a greater extent, and the UAVs can be debugged more comprehensively. The application environment is more extensive, especially suitable for Debugging for micro UAVs. Moreover, according to the needs of the environment, the angle between two adjacent straight poles and the angle between the straight pole and the bent pole can be adjusted, and the shape of the debugging device can be changed for debugging. Compared with the debugging platform, it is more portable and saves materials. In addition, the debugging device is provided with a first power socket and a first USB socket, and the power cord and the data cable are inserted into the two sockets respectively, and the debugging device is connected with the electronic equipment to debug the drone, so as to ensure that the experiment and power supply are more convenient. Safe and convenient.

Description

technical field [0001] The invention relates to the technical field of UAV debugging equipment, in particular to a suspended UAV debugging device. Background technique [0002] With the widespread application of drones in military, agriculture, emergency rescue and disaster relief, popular science education, etc. in recent years, drone technology has received more and more attention. UAV debugging is an important link before UAVs are put into use, and the research and development of debugging devices is becoming more and more important. Among them, the science education of micro-UAVs in primary and secondary schools has attracted much attention. The debugging device is generally a test-flight debugging. Since this kind of debugging cannot fully guarantee the safety of students and teachers, it has not been widely promoted in the teaching field for a long time. [0003] The UAV has the characteristics of complex system and many control variables. It is necessary to ensure th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F5/60
CPCB64F5/60B64U10/00
Inventor 富立于越李润夏王玲玲
Owner BEIHANG UNIV