Parameter-independent aircraft flight path clustering method based on contour coefficients

A technology of contour coefficient and flight trajectory, applied in the direction of electrical digital data processing, instruments, special data processing applications, etc., can solve problems such as non-optimal values, poor generalization ability, and lack of quantitative evaluation indicators

Pending Publication Date: 2019-11-01
CIVIL AVIATION UNIV OF CHINA
View PDF4 Cites 7 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The first method relies on expert experience or domain knowledge. The disadvantage is that it relies on expert experience, is highly subjective, and lacks objective quantitative evaluation indicators.
The second method relies on the data characteristics of trajectory samples. The disadvantages are strong limitations and poor generalization ability. When the characteristics of trajectory test samples and training samples are significantly different, the clustering quality of the algorithm using training samples to set parameters will inevitably decline.
The third method is adjusted through multiple experiments. There are two disadvantages. One is that multiple experiments significantly increase the user's time cost; not the theoretical optimum

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
  • Parameter-independent aircraft flight path clustering method based on contour coefficients
  • Parameter-independent aircraft flight path clustering method based on contour coefficients
  • Parameter-independent aircraft flight path clustering method based on contour coefficients

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0090] A total of 365 real aircraft approach flight trajectories for 48 consecutive hours on runway 28L of San Francisco International Airport are selected to illustrate the method.

[0091] A track is shown in Table 1:

[0092] Table 1 Trajectory data

[0093] serial number Abscissa Y-axis altitude coordinates time 1 18483 -74632 3996 0 2 18225 -73838 3963 5 3 17959 -73048 3930 10 4 17696 -72265 3895 14 5 17426 -71486 3858 19 6 17148 -70711 3820 23 7 16864 -69937 3781 28 8 16585 -69165 3741 33 9 16317 -68395 3700 37 10 16052 -67627 3659 42 …… …… …… …… …… 126 -10768 -10962 82 578 127 -11037 -10817 65 583 128 -11302 -10672 47 587 129 -11561 -10526 29 592 130 -11817 -10381 11 597

[0094] The complete process of the algorithm is as follows figure 1 As shown, the specific method steps are as follows:

[0095] (1), normalized spati...

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 discloses a parameter-independent aircraft flight path clustering method based on contour coefficients. The parameter-independent aircraft flight path clustering method comprises the following steps: firstly, normalizing spatial position coordinates of all tracks in a track set; then, establishing a track similarity, a track distance matrix, a degree matrix and a Laplace matrix basedon the dynamic time bending distance and a Gaussian kernel function; next, clustering the track feature subspaces cluster by cluster in a given interval by utilizing a k-means algorithm; and finally,determining the optimal cluster, the optimal cluster number and the maximum average contour coefficient by taking the average contour coefficient of the track set as an evaluation standard of clustering quality. Compared with an existing method, the parameter-independent aircraft flight path clustering method has the advantages that expert experience or domain knowledge is not needed; human intervention is eliminated; the objectivity of the clustering process and result is high; and the parameter-independent aircraft flight path clustering method is not influenced by flight path length, speed, horizontal and vertical coordinates and height coordinate value domain difference, and is suitable for various data formats; the workload of user parameter adjustment is reduced, and the time cost is saved.

Description

technical field [0001] The invention relates to a time-space trajectory clustering method, in particular to a parameter-independent aircraft flight trajectory clustering method based on silhouette coefficients. Background technique [0002] Most of the current flight trajectory clustering algorithms require one or more input parameters, and their clustering results usually depend heavily on these parameters, but it is difficult to determine reasonable parameters. Generally, there are three methods and basis to determine the necessary parameters of the algorithm. The first method relies on expert experience or domain knowledge. The disadvantage is that it relies on expert experience, is highly subjective, and lacks objective quantitative evaluation indicators. The second method relies on the data characteristics of trajectory samples. The disadvantages are strong limitations and poor generalization ability. When the characteristics of trajectory test samples and training sam...

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): G06F17/50G06K9/62
CPCG06F18/23
Inventor 孙石磊王超赵元棣
Owner CIVIL AVIATION UNIV OF CHINA
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