Unmanned aerial vehicle dual-redundancy system control method

A dual-redundant, unmanned aerial vehicle technology, applied in the field of aircraft, to achieve the effect of avoiding collision and crash accidents and quickly obtaining azimuth

Active Publication Date: 2021-07-20
GUANGZHOU NANYANG POLYTECHNIC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, providing a dual-redundant power supply module can improve the reliability and safety of the UAV to a certain extent, but it is far from enough, and it cannot prevent the UAV from having a backup in the event of a failure. The scheme works fine

Method used

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  • Unmanned aerial vehicle dual-redundancy system control method

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Embodiment

[0033] Refer to attached Figure 1-9 , a dual redundant system for unmanned aerial vehicles, the system includes a power supply module, a video transmission module, a power module, a compass module and a flight controller, the power supply module is powered by dual batteries in parallel, and the video transmission module uses dual The image transmission unit of the road, the power module adopts a four-rotor structure with coaxial twin propellers, the coaxial twin propellers are an existing structure, the compass module adopts internal and external dual compass settings, and the video transmission module , power module and compass module are all connected to the flight controller.

[0034] The power supply module includes a first battery, a second battery and a DC / DC step-down module, the voltages of the first battery and the second battery are both 25V, and the first battery and the second battery are connected in parallel to multiple sets of The motor provides electric energ...

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Abstract

The invention relates to the field of aircraft, in particular to an unmanned aerial vehicle dual-redundancy system control method. The system comprises a power supply module, a video transmission module, a power module, a compass module and a flight controller, the power supply module adopts a double-battery parallel connection mode to supply power, the video transmission module adopts a double-path image transmission unit, the power module adopts a coaxial double-propeller rotor wing structure, the compass module adopts an internal compass and an external compass, and the video transmission module, the power module and the compass module are all connected with the flight controller. According to the unmanned aerial vehicle, dual-redundancy setting is adopted on the power supply module, dual-redundancy setting is adopted on the video transmission module, the power module and the compass module, the probability of shutdown or crash after the unmanned aerial vehicle breaks down is greatly reduced, and it is guaranteed that the unmanned aerial vehicle can smoothly complete work in some special and key fields.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to a control method for a dual redundant system of an unmanned aerial vehicle. Background technique [0002] UAVs are easily affected by various factors during the flight movement, such as weather factors, wind factors, electromagnetic factors, flight environment factors and human factors, which make the UAV prone to failure. The failure of the UAV will delay the work, and cause the crash of the UAV, resulting in certain property losses. [0003] At present, there is a patent titled "A Dual-redundant Aviation Power Supply and Its Power Supply Mode", with the application number 201110258227.2, which discloses a dual-redundancy aviation power supply and its power supply mode, which is realized on the power supply module of the drone. The dual-redundant design ensures that as long as two batteries do not fail at the same time, the power supply module can provide stable and continuous power to ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D27/24H02J9/06H02P5/46H04N7/18H04B7/185H04L1/22
CPCB64D27/24H02J9/068H02P5/46H04N7/183H04B7/18506H04L1/22B64U50/19
Inventor 陈友鹏赖刘生杨嘉贤高阳徐勋梁英标李雷
Owner GUANGZHOU NANYANG POLYTECHNIC
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