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A flight push-out status monitoring method based on multimodal data fusion

A data fusion and multi-modal technology, applied in the direction of neural learning methods, text database query, and other database retrieval, can solve potential safety hazards, inability to prevent conflicts, lagging efficiency, etc., to prevent conflicts and improve status monitoring ability, the effect of preventing taxiway conflicts

Active Publication Date: 2021-12-17
THE 28TH RES INST OF CHINA ELECTRONICS TECH GROUP CORP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This process has huge safety hazards, that is, the flight may not be discovered until it taxis to the taxiway. If there is a taxiway conflict or the scene is busy, there will be serious consequences
In response to this problem, controllers can only rely on the scene surveillance system for real-time tracking, resulting in lag and inefficiency in problem discovery
[0003] The difficulty of this problem is that currently there is no system that can identify the intention of the controller and the intention of the flight, so it is difficult to judge whether the two intentions are consistent, and it is impossible to prevent conflicts caused by non-executed instructions or unauthorized execution of instructions

Method used

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  • A flight push-out status monitoring method based on multimodal data fusion
  • A flight push-out status monitoring method based on multimodal data fusion

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0073] Flight CES3485 is parked at stand 12 and is ready and waiting to be launched. The controller issued a control instruction at 8:30 Beijing time: Dongfang 3485, push out from stand 12, and wait at Alpha. The captain pushed out of the gate immediately after hearing the instruction and reached the taxiway 4 minutes later.

[0074] Step 1: The control automation system monitors the call system in real time, uses the control speech recognition system to convert the control voice into control instruction text, traverses the flight action dictionary in the keyword dictionary, and matches words such as "push", "drive" or "push drive" , filter out this instruction, and extract the keyword "launch". Extract other information through dictionary traversal, obtain the flight number dictionary according to the plan information in the control automation system, traverse the flight number dictionary to match the flight number as CES3485, match it from the airport basic information in th...

Embodiment 2

[0094] Flight CES3485 stopped at gate 12 and was being rolled out, but the controller had already issued a control order 10 minutes ago, that is, at 8:30 Beijing time: East 3485, push out from gate 12, and wait at Alpha. The captain did not push out of the parking stand immediately after hearing the instruction, but started to push out after 10 minutes.

[0095] Step 1: The control automation system monitors the call system in real time, uses the control speech recognition system to convert the control voice into control instruction text, traverses the flight action dictionary in the keyword dictionary, and matches words such as "push", "drive" or "push drive" , filter out this instruction, and extract the keyword "launch". Extract other information through dictionary traversal, obtain the flight number dictionary according to the plan information in the control automation system, traverse the flight number dictionary to match the flight number as CES3485, match it from the ai...

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PUM

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Abstract

The invention discloses a multi-modal data fusion-based method for monitoring flight status, belonging to the technical field of air traffic control automation systems. 1. Build a flight intention recognition model, extract aircraft actions from real-time surveillance video, and capture flight intentions; 3. Build intention alignment fusion rules to determine whether there is a conflict between control intention information and flight intention information. By fusing control intentions and flight intentions, this method can realize the following auxiliary functions: timely judge whether the aircraft follows the push-off instructions issued by the controller, if the captain does not act in accordance with the control instructions, or acts without control instructions , the inconsistency alarm will be issued to realize the monitoring function of the flight launch status.

Description

technical field [0001] The invention belongs to the technical field of air traffic control automation systems, and in particular relates to a multi-mode data fusion-based method for monitoring the flight status. Background technique [0002] With the vigorous development of China's civil aviation industry in the past 30 years, the demand for air traffic management has continued to expand, resulting in increasingly prominent safety hazards. Among them, the flight on the parking stand did not implement the controller's push-out instructions, and pushed out after a period of time without authorization, which would cause taxiway conflicts and cause safety hazards. The current handling process is as follows: If a flight rolls out of the parking stand after a certain period of time and slides onto the taxiway, it is considered an invalid behavior, and the controller will issue an order to let the flight slide into the parking stand again. There is a huge safety hazard in this pro...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F16/33G06F16/903G06F40/242G06K9/00G06K9/62G06N3/04G06N3/08
CPCG06F16/3344G06F16/90344G06F40/242G06N3/08G06N3/045G06F18/214G06F18/24
Inventor 王煊汤闻易丁辉黄吉波刘岩徐秋程
Owner THE 28TH RES INST OF CHINA ELECTRONICS TECH GROUP CORP
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