Method for calculating radar scattering properties of stable section of aircraft wake flow in clear sky

A technology of radar scattering and characteristic calculation, which is applied in the direction of using re-radiation, reflection/re-radiation of radio waves, measurement devices, etc., which can solve the problems of difficult modeling, slow progress, and large amount of calculation.

Inactive Publication Date: 2014-01-15
NAT UNIV OF DEFENSE TECH
View PDF4 Cites 13 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The wake scattering characteristics of clear-air aircraft are generally studied as heterogeneous medium targets, but the electrical size of the aircraft wake is particularly large (up to hundreds of meters in the direction of wingspan and aircraft height, and even up to kilometers in the direction of aircraft flight) And the structure is complex, which makes the theoretical research on wake radar scattering characteristics slow down for a long time due to technical bottlenecks such as difficult modeling and huge amount of calculation.
It is precisely because of this that people's current understanding of the wake scattering characteristics is not deep enough, which makes the research on existing detection methods and detection experiments very blind, and many results of detection experiments cannot give reasonable explanations at the level of mechanism

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
  • Method for calculating radar scattering properties of stable section of aircraft wake flow in clear sky
  • Method for calculating radar scattering properties of stable section of aircraft wake flow in clear sky
  • Method for calculating radar scattering properties of stable section of aircraft wake flow in clear sky

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0013] In order to better understand the technical solutions of the present invention, the implementation manners of the present invention will be further described below in conjunction with the accompanying drawings.

[0014] figure 1 It is a flow chart of the calculation solution for aircraft wake radar scattering characteristics. The first step is to establish the coordinate system between the radar and the wake; the second step is to calculate the distribution of the relative permittivity difference between the aircraft wake and the background air; the third step is to calculate the total electric field inside the aircraft wake; the fourth step is to calculate The high oscillation integral corresponding to the Hertz vector; the fifth step is to calculate the far-field scattering field of the aircraft wake; the sixth step is to calculate the radar cross section of the aircraft wake. Each step is described below.

[0015] Step 1: Establish the coordinate system of radar an...

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 provides a method for calculating the radar scattering properties of a stable section of aircraft wake flow in clear sky. According to the technical scheme, the method includes the steps of firstly, calculating dielectric constant distribution and internal electric field distribution of the aircraft wake flow, and then calculating the high vibration integration derived from a scattering integral equation to obtain the radar scattering cross section of the aircraft wake flow. Compared with a conventional method for calculating the electromagnetic scattering properties, the method has the advantages that the calculated amount and the storage amount are lowered in a magnitude mode, the relationship between the radar scattering cross section of the aircraft wake flow and the frequency of incident waves can be calculated and obtained through the method, and theory supports and model supports are provided for the development of the related radar detection technologies.

Description

technical field [0001] The invention belongs to the technical field of radar target characteristics, and relates to the calculation of radar scattering characteristics of aircraft wakes and other special super-large electrical size non-uniform medium targets, and can provide technical support for the research of aircraft wake scattering mechanism and the development of radar detection technology. Background technique [0002] Aircraft wake is a strong spiral airflow formed behind the aircraft during flight. It has the characteristics of large spatial scale, long duration, and strong rotation. It has a serious impact on the flight safety of subsequent aircraft (rolling, shaking, stalling, etc. Wait). In order to ensure flight safety, the International Civil Aviation Organization established a set of aircraft safety separation standards in the early 1970s. This standard does not distinguish between weather conditions and relies on parameters such as the size, speed, and weight...

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
Patent Type & Authority Applications(China)
IPC IPC(8): G01S7/41
CPCG01S7/412G01S13/933
Inventor 王雪松王涛李健兵李军刘忠训屈龙海庞晨
Owner NAT UNIV OF DEFENSE TECH
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products