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Aircraft flight path jump removing method

A flight trajectory and aircraft technology, applied in the field of aircraft flight trajectory jump removal, to achieve the effect of solving longitude, latitude or altitude jumps and accurate real-time positioning data

Active Publication Date: 2017-03-22
FEIYOU TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention is aimed at the deficiencies in the prior art, and provides a method for removing the flight track jump of an aircraft, which solves the problem of positioning longitude and latitude or altitude jumps, makes the real-time positioning data more accurate, and displays the aircraft's position with smoother data. flight path

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Embodiment Construction

[0027] The content of the present invention will be described below in conjunction with specific embodiments.

[0028] After observing the historical data, the longitude and latitude issued by ADS-B have a small probability of jumping to a fixed position and a large range for a long time.

[0029] The data presents a regular jump to a fixed position every two positioning points, and because ADS-B only sends one status value each time, such as latitude and longitude, altitude, angle, ground speed, and vertical speed a value.

[0030] Based on the above-mentioned rules and rules, a method for removing the flight trajectory jump of an aircraft provided in this embodiment includes the following specific steps:

[0031] 1. After receiving the latitude and longitude ,altitude ,angle , ground speed , vertical speed , t represents the timestamp when the data is received, and the metadata is recorded in a collection corresponding to the data of the last three minutes middl...

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Abstract

The invention discloses an aircraft flight path jump removing method, which comprises the following steps: constructing a cubic polynomial fitting algorithm in corresponding type and at non-fixed time intervals, and calculating predicted values corresponding to altitude, angle, ground velocity and vertical velocity and storing the predicted values; when receiving latitude and longitude values, and if the number of latitude and longitude elements in a set within a time range 1 minute before the current time is smaller than 3, not carrying out calculating and quitting; or otherwise, comparing the longitude and latitude at the current time with longitude and latitude at a previous time point and longitude and latitude at a time point before the previous time point: calculating predicted distance and actual distance, and comparing the difference between the predicted distance and the actual distance and larger one of the predicted distance and the actual distance to obtain data credibility weight; and if the data credibility weight is smaller than 1, regarding the data as credibility data and storing the data. The method can solve the problem of longitude and latitude or height positioning jump, so that real-time positioning data is allowed to be more accurate, and the flight path of an aircraft is allowed to be displayed with smoother data.

Description

technical field [0001] The invention relates to a method for removing flight track jumps of aircraft, and belongs to the technical field of aircraft flight track optimization methods. Background technique [0002] With the continuous development and growth of China's aviation industry, problems such as airspace and flow have become more and more prominent. Flight delays and flow control have caused complaints from passengers. The emergence of this new technology, ADS-B, can automatically obtain parameters from relevant airborne equipment and broadcast the aircraft's position, altitude, speed, heading, identification number and other information to other aircraft or ground stations, so that the controller can monitor the status of the aircraft. monitor. [0003] With the increasing popularity of ADS-B in aircraft applications, the feasibility of aircraft position monitoring through ADS-B is becoming stronger and stronger; however, due to the limited range of ADS-B transmissi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G08G5/00
CPCG08G5/0004
Inventor 张重阳宣彤郑洪峰
Owner FEIYOU TECH CO LTD