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Aircraft early warning method and device, electronic equipment and readable storage medium

A technology of aircraft and equipment status, applied in the field of aircraft safety, can solve the problems that cannot reduce the personal safety risk of ground personnel in the drone operating area, and achieve the effect of reducing personal safety risk

Inactive Publication Date: 2021-04-23
BEIJING AIRLANGO TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] Embodiments of the present invention provide an aircraft early warning method, device, electronic equipment, and readable storage medium, to at least solve the problem of inability to reduce the personal safety of ground personnel in unmanned aerial vehicle operating areas in the related art without adding early warning hardware. Technical issues with security risks

Method used

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  • Aircraft early warning method and device, electronic equipment and readable storage medium
  • Aircraft early warning method and device, electronic equipment and readable storage medium
  • Aircraft early warning method and device, electronic equipment and readable storage medium

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Embodiment 1

[0026] According to an aspect of an embodiment of the present invention, an aircraft early warning method is provided. Optionally, as an optional implementation, the above aircraft early warning method can be applied to, but not limited to, such as figure 1 environment shown, where, figure 1 It is a schematic diagram of the hardware environment of the aircraft early warning method according to the embodiment of the present invention. Such as figure 1 As shown, data interaction can be performed between the target aircraft 10 and the terminal 20, the distance between the target aircraft 10 and the terminal 20 is less than the preset distance threshold, and the target aircraft 10 includes but is not limited to a power unit, an image acquisition unit and a communication unit, Terminal 20 includes, but is not limited to, a communication unit.

[0027] In this embodiment, the target aircraft 10 is kept flying by the power unit, and during the flight, the navigation information and...

Embodiment 2

[0065] According to an embodiment of the present invention, there is also provided an aircraft early warning device for implementing the above aircraft early warning method, such as image 3 As shown, the device includes:

[0066] 1) The acquisition unit 30 is used to acquire navigational information and sensor data of the target aircraft every preset time, wherein the navigational information includes the position information, navigational speed and navigational angle;

[0067] 2) A determining unit 32, configured to determine the equipment state of the target aircraft according to the navigation information and the sensor data.

[0068] 3) an acquisition unit 34, configured to acquire failure information and location information of the target aircraft when the equipment state is failure;

[0069] 4) A communication unit 36, configured to send an alarm signal corresponding to the fault information to a terminal in a target area, wherein the target area is determined accordin...

Embodiment 3

[0091] According to an embodiment of the present invention, there is also provided an electronic device for implementing the above aircraft early warning, the electronic device includes a processor, a memory, and a program or instruction stored in the memory and operable on the processor, When the program or instruction is executed by the processor, the steps of the aircraft early warning method described in Embodiment 1 are realized.

[0092] Optionally, in this embodiment, the memory is configured to store program codes for performing the following steps:

[0093] S1, acquiring navigational information and sensor data of the target aircraft at preset intervals, wherein the navigational information includes the position information, navigational speed and navigational angle;

[0094] S2. Determine the equipment status of the target aircraft according to the navigation information and the sensor data;

[0095] S3, when the equipment state of the target aircraft is faulty, acq...

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Abstract

The invention discloses an aircraft early warning method and device, electronic equipment and a readable storage medium. The method comprises the steps of obtaining navigation information and sensor data of a target aircraft every other preset time, wherein the navigation information comprises position information, navigation speed and navigation angle; determining the equipment state of the target aircraft according to the navigation information and the sensor data; under the condition that the equipment state is a fault, obtaining fault information and position information of the target aircraft; and sending an alarm signal corresponding to the alarm information to a terminal in the target area. According to the invention, the technical problem that the personal safety risk of ground personnel in an unmanned aerial vehicle operation area cannot be reduced under the condition of not increasing early warning hardware in related technologies is solved.

Description

technical field [0001] The present invention relates to the technical field of aircraft safety, in particular to an aircraft early warning method, device, electronic equipment and a readable storage medium. Background technique [0002] In recent years, there are more and more applications of drones, such as aerial photography, logistics, surveying and mapping, etc., and the number of drones is also increasing. While the large-scale application of drones improves efficiency, it also brings many security risks to the public, such as interfering with civil aviation operations and exposing sensitive facilities. [0003] For such hidden dangers, there are many solutions, such as setting up multiple receiving stations to complete the collection, processing, identification, feature extraction and parameter estimation of UAV transmission signals, and then complete the positioning and tracking of UAVs. Feature information, automatically identify whether it is an illegal target, and...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G08B21/02G08G5/00
CPCG08B21/0233G08B21/0225G08B21/0261G08G5/0073
Inventor 崔书林刘伟建王超孙涛
Owner BEIJING AIRLANGO TECH CO LTD
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