Method and device for obtaining dynamic information of flight

A flight dynamics and acquisition method technology, applied in flight plan management, aircraft traffic control, instruments, etc., can solve the problem that the original data source cannot meet the integrity and accuracy of flight data

Inactive Publication Date: 2016-03-30
北京合众思壮时空物联科技有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] The technical problem to be solved by the present invention is: to overcome the problem that a single original data source in the prior art cannot satisfy the integrity and accuracy of flight data, and to provide a method and device for obtaining flight dynamic information. The way of data source integration is to analyze the data according to the characteristics of each data source, which can meet the needs of data integrity, accuracy and ease of use, and provide passengers with national flight information that can accurately predict flight times

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  • Method and device for obtaining dynamic information of flight
  • Method and device for obtaining dynamic information of flight
  • Method and device for obtaining dynamic information of flight

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[0035] Such as figure 1 As shown, the first embodiment of a method for obtaining flight dynamic information of the present invention includes the following steps:

[0036] Step 1, receiving flight information from multiple data interfaces in real time;

[0037] Step 2, analyze the flight information received from different data interface sources, and convert according to the predetermined data format to obtain flight information in a unified data format;

[0038] Step 3, update the flight information in real time according to the flight information in the unified data format.

[0039] The step 3 is further to update the flight information in real time according to the flight information in the unified data format and the priority corresponding to each flight information.

[0040] The priority corresponding to each flight information is determined by the data source of the information.

[0041] The step 1 is further: judging whether the flight information currently received ...

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Abstract

The invention relates to a method and device for obtaining the dynamic information of flight. The method comprises the following steps: 1, receiving flight information from a plurality of data interfaces in real time; 2, analyzing the received flight information from different interfaces, converting the information according to a preset data format, and obtaining the flight information at the unified data format; 3, updating the flight information in real time according to the flight information at the unified data format. The device comprises a real-time receiving module, an analysis module, and a flight information updating module. The method and device are flexible in configuration, can achieve the integration of a plurality of types of data sources, and are high in accuracy of provided flight information.

Description

technical field [0001] The invention relates to an information acquisition method and device, in particular to a flight dynamic information acquisition method and device. Background technique [0002] With the development of the times, more and more people choose to travel by air, and the delays and cancellations of flights due to weather, traffic control and other reasons have attracted more and more attention. In addition to knowing the dynamic information of the flight at the airport, passengers can also check the flight dynamics anytime, anywhere on the PC and mobile terminals through the Internet. At present, there are many related application software on the Internet, such as: Feichang Zhun, Flight Manager and some APPs launched by the airport itself. But no matter what kind of application it is, the accuracy and timeliness of flight dynamic information are the most critical. Only when the flight dynamic data is accurate and timely can it bring real help to passengers...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G08G5/00
CPCG08G5/003
Inventor 杨孙丽马钶佳郝文威郎斌王雪娜
Owner 北京合众思壮时空物联科技有限公司
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