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Unmanned aerial vehicle fault management method and device, and storage medium

A fault management and drone technology, applied in the field of drones, can solve the problems of reducing the accuracy of fault information push, wasting human resources, and not conducive to fault information analysis, avoiding repeated acquisition, improving accuracy, and effective analysis. Effect

Pending Publication Date: 2021-05-04
SZ DJI TECH CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

When a component of the UAV fails, the component directly pushes the fault information to the remote terminal, and when the same fault A causes multiple components to fail, the multiple components push fault A information to the remote terminal respectively, resulting in There are repeated pushes in the fault push, so that the remote control terminal receives redundant fault information, which reduces the accuracy of the fault information push, and is not conducive to the follow-up maintenance personnel to analyze the fault information, so that the maintenance personnel need to analyze multiple fault information Duplicate analysis, waste of human resources

Method used

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  • Unmanned aerial vehicle fault management method and device, and storage medium
  • Unmanned aerial vehicle fault management method and device, and storage medium
  • Unmanned aerial vehicle fault management method and device, and storage medium

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Embodiment Construction

[0058] The following will clearly and completely describe the technical solutions in the embodiments of the present application with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, not all of them. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the scope of protection of this application.

[0059] The flow charts shown in the drawings are just illustrations, and do not necessarily include all contents and operations / steps, nor must they be performed in the order described. For example, some operations / steps can be decomposed, combined or partly combined, so the actual order of execution may be changed according to the actual situation.

[0060] Some implementations of the present application will be described in detail below in conjunction with the acco...

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Abstract

The invention discloses an unmanned aerial vehicle fault management method and device and a storage medium. The method comprises that a remote control terminal sends, to an unmanned aerial vehicle, fault request information for acquiring each component of the unmanned aerial vehicle (S101); the unmanned aerial vehicle acquires fault information sent by each component in response to the fault request information, generates a fault identifier according to the fault information of each component, and sends the fault identifier to the remote control terminal, the fault identifier comprising component information and fault information (S102); and after the remote control terminal receives the fault identifier, component information and fault information corresponding to the fault identifier are displayed in a display interface of the remote control terminal (S103). And the accuracy of obtaining the fault information is improved.

Description

technical field [0001] The present application relates to the technical field of drones, and in particular to a fault management method, device and storage medium for drones. Background technique [0002] With the development of drone technology, the application of drones is becoming more and more extensive. During the use of the UAV, some failures will inevitably occur as the usage time increases. At this time, it is often necessary to obtain the failure information of the UAV in order to analyze the failure. [0003] In the prior art, drones often include many different components, and each component has its own fault handling mechanism. For example, the fault push mechanism and push content of each component are different, which may make the same fault The expressions are different in different parts. When a component of the UAV fails, the component directly pushes the fault information to the remote terminal, and when the same fault A causes multiple components to fail...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 龙召李兴毛慧袁嘉樑
Owner SZ DJI TECH CO LTD
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