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Method, device and equipment for controlling unmanned aerial vehicle and storage medium

A control method and technology of UAV, applied in the field of UAV, can solve problems such as loss

Active Publication Date: 2020-01-10
SHENZHEN AUTEL INTELLIGENT AVIATION TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The defect in the prior art is: when the UAV returns to the voyage, or in any flight process that is not related to the mission performed by the UAV, there are still some situations that consume extra battery power of the UAV. is an ineffective attrition for the mission the UAV is currently performing

Method used

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  • Method, device and equipment for controlling unmanned aerial vehicle and storage medium
  • Method, device and equipment for controlling unmanned aerial vehicle and storage medium
  • Method, device and equipment for controlling unmanned aerial vehicle and storage medium

Examples

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Embodiment 1

[0026] figure 1 It is a schematic flow chart of a UAV control method provided by Embodiment 1 of the present invention. This embodiment can be applied to turning off the functional modules on the UAV that are not related to maintaining the normal flight of the UAV, so as to reduce the ineffective loss of battery power. In the case of extending the battery life, the method can be executed by the UAV control device, which can be implemented by hardware and / or software, and is generally integrated on the UAV. The method specifically includes the following steps:

[0027] It can be understood that the UAV control method provided by the embodiment of the present invention is mainly to add a power-saving flight mode on the basis of the original flight mode of the UAV. The power-saving flight mode does not target certain or certain models The drone, that is, the embodiment of the present invention does not limit the model of the drone.

[0028] Step S101, receiving a mode switching...

Embodiment 2

[0050] figure 2 It is a schematic flowchart of a UAV control method provided by Embodiment 2 of the present invention. This embodiment is further optimized on the basis of Embodiment 1. In this embodiment, the control drone enters the power-saving flight mode corresponding to the mode switching command, which is embodied as: analyzing and determining the power-saving level corresponding to the mode switching command; searching the preset power-saving mode information table , obtain the corresponding power-saving flight mode under the power-saving level; switch the drone to the power-saving flight mode; wherein, the power-saving level includes: light power-saving level, medium power-saving level and extreme power saving levels.

[0051] This embodiment is also optimized and added: sending a communication transmission adjustment instruction to the communication transmission module of the drone; controlling the communication transmission module to reduce the communication frequ...

Embodiment 3

[0075] image 3 It is a schematic structural diagram of a UAV control device provided by Embodiment 3 of the present invention. This embodiment can be applied to this embodiment. In case of invalid loss of battery power and extended battery life, the UAV control device can be implemented by software and / or hardware, specifically including: a mode switching module 301, a determination module 302 to be turned off, and a control shutdown module 303. in,

[0076] The mode switching module 301 is used to receive the mode switching instruction sent by the first control terminal, and control the UAV to enter the power-saving flight mode corresponding to the mode switching instruction;

[0077] The to-be-closed determination module 302 is configured to determine the corresponding to-be-closed module of the UAV in the power-saving flight mode, and generate a corresponding module shutdown instruction, the to-be-closed module is the current flight of the UAV Non-essential function modu...

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Abstract

The embodiment of the invention discloses a method, device and equipment for controlling an unmanned aerial vehicle and a storage medium. The method comprises the steps of receiving a mode switching instruction sent from a first control terminal and controlling the unmanned aerial vehicle to enter a power-saving flight mode corresponding to the mode switching instruction; determining to-be-closedmodules corresponding to the unmanned aerial vehicle in the power-saving flight mode and generating a corresponding mode closing instruction, wherein the to-be-closed modules are non-essential functional modules of the unmanned aerial vehicle when flying in current flight state; and controlling the to-be-closed modules to be closed through the module closing instruction to make the to-be-closed modules stop working. The functional modules which are irrelevant to keeping normal flight of the unmanned aerial vehicle on the unmanned aerial vehicle can be closed through being switched into the power-saving flight mode, thereby reducing invalid loss of battery power, prolonging the battery life and simultaneously reducing the risk that the unmanned aerial vehicle cannot return or even crashes due to low battery power.

Description

technical field [0001] Embodiments of the present invention relate to the technical field of drones, and in particular, to a method, device, device and storage medium for controlling drones. Background technique [0002] At present, the general flight time of drones is about 30 minutes. At the same time, with long-term use, the batteries of drones will gradually wear out, and the battery life will gradually decrease. Therefore, it will be difficult to control the use of batteries. If the battery power is seriously low during the flight of the drone, or even not enough to support the drone to fly back to the home point, the risk of crash will be greatly increased. [0003] In order to reduce the risk of crash, the existing technical solutions generally adopt: setting low battery automatic return; sound alarm reminder through remote control or mobile phone application software; setting maximum flight distance, etc. [0004] The defect in the prior art is: when the UAV returns...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 彭志坤
Owner SHENZHEN AUTEL INTELLIGENT AVIATION TECH CO LTD
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