Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Aircraft longitudinal interval calculation method and system and readable storage medium

A calculation method and longitudinal separation technology, applied in flight plan management, aircraft traffic control, traffic control system, etc., can solve problems such as the maximum wake vortex strength of the rear aircraft and the reduction of airspace capacity without reasonable consideration, and achieve strong versatility and improved The effect of aircraft capacity

Inactive Publication Date: 2021-09-21
CIVIL AVIATION FLIGHT UNIV OF CHINA +2
View PDF6 Cites 5 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to overcome the problem in the prior art that there is no reasonable consideration of the maximum wake vortex strength that the rear aircraft can bear, so that the longitudinal interval between the front and rear aircraft is set too large and the airspace capacity is reduced; and a kind of A method and system for calculating the dynamic actual interval of aircraft landing, through which the longitudinal interval between the front and rear aircraft can be reasonably reduced, thereby increasing the airspace capacity

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Aircraft longitudinal interval calculation method and system and readable storage medium
  • Aircraft longitudinal interval calculation method and system and readable storage medium
  • Aircraft longitudinal interval calculation method and system and readable storage medium

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0053] figure 1 A flowchart of a method for calculating the longitudinal separation of an aircraft according to an exemplary embodiment of the present invention is shown, including:

[0054] A. The improved Reich collision model is obtained by adding the influence length of the wake of the strong eddy current field to the longitudinal dimension of the traditional Reich collision model;

[0055] Specifically, different meteorological conditions will affect the dissipation speed of the wake of the front aircraft, and then affect the longitudinal safety separation between the front and rear aircraft. The main meteorological parameter that will affect the wake vortex dissipation rate is the dimensionless turbulent dissipation rate ε * and dimensionless Frequency N * as an input parameter to the dimensionless wake vortex intensity dissipation curve In order to consider the influence of meteorological factors.

[0056] where the dimensionless turbulent dissipation rate ε * T...

Embodiment 2

[0096] Further, on the basis of Embodiment 1, solve the calculation example of the longitudinal separation of aircraft, and the meteorological parameters obtained by the meteorological monitoring equipment of the airport can establish the dimensionless wake vortex intensity dissipation curve under the airspace meteorological conditions of the airport at a certain moment The wake vortex dissipates relatively slowly in the initial dissipating stage, and then enters the fast dissipating stage

[0097] Such as image 3 As shown, it is the dimensionless wake vortex intensity dissipation curve established by the present invention under the meteorological conditions of an airport in Southwest China at a certain moment

[0098] For the convenience of statistics, the aircraft that took off and landed on the day are classified; the calculation parameters of different aircraft types are shown in Table 1

[0099]

[0100] Table 1 Calculation parameters

[0101] In this embodiment ...

Embodiment 3

[0107] Figure 5 Shown is an aircraft longitudinal separation calculation system according to an exemplary embodiment of the present invention, that is, an electronic device 310 (such as a computer server with a program execution function), which includes at least one processor 311, a power supply 314, and at least one A processor 311 is communicatively connected to a memory 312 and an input / output interface 313; the memory 312 stores instructions that can be executed by the at least one processor 311, and the instructions are executed by the at least one processor 311, so that all The at least one processor 311 can execute the method disclosed in any of the foregoing embodiments; the input-output interface 313 can include a display, a keyboard, a mouse, and a USB interface for inputting and outputting data; the power supply 314 is used to power the electronic device 310 Provide electrical energy.

[0108] At the same time, this embodiment also provides a readable storage med...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention belongs to the technical field of air control, and relates to an aircraft longitudinal interval calculation method and system and a readable storage medium. The airplane longitudinal interval calculation method provided by the invention comprises the following steps of: adding a strong vortex field wake influence length into a longitudinal size of a traditional Reich collision model to obtain an improved Reich collision model; and solving aircraft longitudinal intervals corresponding to different front and rear aircraft combinations through the improved Reich collision model on the basis of CNS performance in an airspace environment, the aircraft longitudinal intervals being used for airspace planning. According to the aircraft longitudinal interval calculation method and system and the readable storage medium, the strong vortex field wake influence length is added into the longitudinal size of the traditional Reich collision model, the strength of the trailing vortex capable of being borne by a rear aircraft is reasonably considered, and the strength is combined with the CNS performance in the airspace, so that an aircraft longitudinal interval shorter than an interval formulated by ICAO is obtained; and a controller uses the method to guide the interval between a front aircraft and the rear aircraft, so that the interval between the front aircraft and the rear aircraft is reasonably shortened, and the aircraft capacity of the airspace is improved.

Description

technical field [0001] The invention belongs to the technical field of air control, and in particular relates to a method, a system and a readable storage medium for calculating an aircraft longitudinal interval. Background technique [0002] In recent years, my country's civil aviation industry has developed rapidly, and the air traffic capacity is increasing day by day. In order to cope with the increasing flight volume, all parties have made various efforts. On the one hand, some airports adopt the method of laying parallel runways on the basis of the original infrastructure to cope with the difficulties brought about by the increase in flight volume; on the other hand, control units adopt smaller vertical intervals in the terminal control area to improve the operational efficiency of the airport , the longitudinal interval can be the interval expressed by distance between aircraft tracks at the same altitude. At the same time, the International Civil Aviation Organizat...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): G08G5/02G08G5/00
CPCG08G5/02G08G5/003G08G5/0043
Inventor 潘卫军许亚星
Owner CIVIL AVIATION FLIGHT UNIV OF CHINA
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com