CN109302580A - A kind of aircraft disengaging berth automatic testing method based on video monitoring - Google Patents

A kind of aircraft disengaging berth automatic testing method based on video monitoring Download PDF

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Publication number
CN109302580A
CN109302580A CN201811048478.6A CN201811048478A CN109302580A CN 109302580 A CN109302580 A CN 109302580A CN 201811048478 A CN201811048478 A CN 201811048478A CN 109302580 A CN109302580 A CN 109302580A
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CN
China
Prior art keywords
aircraft
frame
video monitoring
testing method
automatic testing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201811048478.6A
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Chinese (zh)
Inventor
曾啸天
刘刚
张红日
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hefei Juqing Information Technology Co Ltd
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Hefei Juqing Information Technology Co Ltd
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Priority to CN201811048478.6A priority Critical patent/CN109302580A/en
Publication of CN109302580A publication Critical patent/CN109302580A/en
Pending legal-status Critical Current

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    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N7/00Television systems
    • H04N7/18Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
    • H04N7/181Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a plurality of remote sources
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06VIMAGE OR VIDEO RECOGNITION OR UNDERSTANDING
    • G06V20/00Scenes; Scene-specific elements
    • G06V20/40Scenes; Scene-specific elements in video content
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N5/00Details of television systems
    • H04N5/14Picture signal circuitry for video frequency region
    • H04N5/144Movement detection

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  • Engineering & Computer Science (AREA)
  • Multimedia (AREA)
  • Signal Processing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Image Analysis (AREA)
  • Traffic Control Systems (AREA)

Abstract

The invention belongs to technical field of video monitoring, berth automatic testing method is passed in and out more particularly to a kind of aircraft based on video monitoring, including video monitoring system, the video monitoring system includes monitoring center, video analytics server, data acquisition is carried out to more front ends, data processing and data are shown, the aircraft disengaging berth automatic testing method based on video monitoring includes the following steps: airplane motion detection and aircraft state detection, overcome the deficiencies in the prior art, utilize computer picture Visual analysis techniques, by acquiring front-end camera information, background in scene (airport) and target (aircraft or other moving objects) are separated and then analyze the concrete behavior of specific objective (aircraft) by system;It can accurately differentiate the behavior (push-in releases berth) of aircraft, and automatically by data inputting server-side management system.

Description

A kind of aircraft disengaging berth automatic testing method based on video monitoring
Technical field
The invention belongs to technical field of video monitoring, and in particular to a kind of aircraft disengaging berth based on video monitoring is automatic Detection method.
Background technique
The development of civil aviaton of China service business was very rapid in recent years, was pushed away based on the manually recorded airport aircraft of support personnel The management mode for entering, releasing berth has increasingly been not suitable with the demand in market, manually recorded easy misdescription, error of omission, and after finding not It is traceable to check and verify.With the rapid development of computer intellectual technology, artificial intelligence analysis's management mode is also come into being therewith.Just It is using computer picture Visual analysis techniques, by by background in scene (airport) and target (aircraft or other moving objects) Separate and then analyze the concrete behavior of specific objective (aircraft).It can accurately differentiate the behavior (push-in releases berth) of aircraft, and Automatically by data inputting server-side management system.And there is presently no add the algorithm of template matching to use exclusively with motion detection In the aircraft behavioral value of Commercial Air Service.
Summary of the invention
The purpose of the present invention is to provide a kind of, and the aircraft based on video monitoring passes in and out berth automatic testing method, overcomes The deficiencies in the prior art, using computer picture Visual analysis techniques, by acquiring front-end camera information, system will be in scene Background (airport) and target (aircraft or other moving objects) separate and then analyze the concrete behavior of specific objective (aircraft);It can be with The accurate behavior (push-in releases berth) for differentiating aircraft, and automatically by data inputting server-side management system.
To solve the above problems, the technical solution used in the present invention is as follows:
A kind of aircraft disengaging berth automatic testing method based on video monitoring, including video monitoring system, the video monitoring System includes monitoring center, video analytics server, carries out data acquisition, data processing and data to more front ends and shows;
The aircraft disengaging berth automatic testing method based on video monitoring includes the following steps:
(1) airplane motion detects
The boundary rectangle frame of aircraft profile is obtained by operations such as MOG2 algorithm, gaussian filtering, morphology;
(2) aircraft state detects
Steps are as follows:
A, each frame judges that boundary rectangle frame area accounts for the certain threshold value of interface drawing area area, and default has big object to enter runway Range, from adding 1, continuous each frame all meets flag bit;
B, after step a meets, record aircraft continuously moves the aggregate-value n of pixel;
C, aircraft stops head detection frame and drawing area phase and acquisition intersecting area, it is ensured that small frame is inside big frame;
D, record phase and total pixel value m2 in region;
E, when m2 accounts for the certain area of the total pixel of small frame or more, from adding 1, continuous each frame all meets for trigger flag position;
F, n meets n and is equal to when drawing the total pixel certain percentage of frame, records the total pixel value m1 of airplane motion rectangle frame at this time, Judgment criteria when stopping as aircraft;
G, when n is greater than drawing area total pixel certain value, the total pixel value m of airplane motion rectangle frame detection block is recorded;
H, the position for starting airplane motion rectangle frame in a period of time is recorded;
I, when m is less than certain percentage m1, it is believed that aircraft is mobile to be stopped;
J, judge on the basis of step i: 1. airplane motion frame positions and lqrect phase with and mutually with area to account for the gross area certain More than percentage, successive frame all meets then fjstate=1, show that aircraft is leave state planestate=2;2. working as flag bit When big Mr. Yu's numerical value (default) and the big Mr. Yu's numerical value in trigger flag position, obtain aircraft for arrival state planestate=1;3. When the small Mr. Yu's numerical value of flag bit or the small Mr. Yu's numerical value in trigger flag position, aircraft is that aircraft does not go out present condition planestate=3.
Further, the video analytics server is connected by LAN/Internet with monitoring center.
Further, the front end multichannel video camera is fixed wide angle cameras, passes through interchanger and video analytics server It is connected, carries out signal acquisition, completes video decoding.
Further, it is added in template samples picture in each framing of drawing area;According to planestate numerical value Template matching is carried out, matching result preserves;When adaptation function calculates matching degree small Mr. Yu's coefficient, current region and mould are judged Plate mismatches, and is judged as that aircraft enters the region at this time, while call back function being called to notify interface;Airport is similar in order to prevent Truck is by drawing area and does not stop and false triggering detection function function logics, and spy is by the way of template matching.
The present invention compared with prior art, has the advantages that
A kind of aircraft based on video monitoring of the present invention passes in and out berth automatic testing method, utilizes computer picture vision point Analysis technology, by acquiring front-end camera information, system is by background in scene (airport) and target (aircraft or other moving objects Body) separate the concrete behavior for analyzing specific objective (aircraft) in turn;It can accurately differentiate the behavior (push-in releases berth) of aircraft, And automatically by data inputting server-side management system.
Detailed description of the invention
Fig. 1 is a kind of system schematic that the aircraft disengaging berth based on video monitoring is detected automatically.
Fig. 2 is a kind of logical schematic that the aircraft disengaging berth based on video monitoring is detected automatically.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other Embodiment shall fall within the protection scope of the present invention.
As shown, a kind of aircraft based on video monitoring of the present invention passes in and out berth automatic testing method, including view Frequency monitoring system, the video monitoring system include monitoring center, video analytics server, to more front ends carry out data acquisition, Data processing and data are shown;
The aircraft disengaging berth automatic testing method based on video monitoring includes the following steps:
(1) airplane motion detects
The boundary rectangle frame of aircraft profile is obtained by operations such as MOG2 algorithm, gaussian filtering, morphology;
(2) aircraft state detects
Steps are as follows:
A, each frame judges that boundary rectangle frame area accounts for the certain threshold value of interface drawing area area, and default has big object to enter runway Range, from adding 1, continuous each frame all meets flag bit;
B, after step a meets, record aircraft continuously moves the aggregate-value n of pixel;
C, aircraft stops head detection frame and drawing area phase and acquisition intersecting area, it is ensured that small frame is inside big frame;
D, record phase and total pixel value m2 in region;
E, when m2 accounts for the certain area of the total pixel of small frame or more, from adding 1, continuous each frame all meets for trigger flag position;
F, n meets n and is equal to when drawing the total pixel certain percentage of frame, records the total pixel value m1 of airplane motion rectangle frame at this time, Judgment criteria when stopping as aircraft;
G, when n is greater than drawing area total pixel certain value, the total pixel value m of airplane motion rectangle frame detection block is recorded;
H, the position for starting airplane motion rectangle frame in a period of time is recorded;
I, when m is less than certain percentage m1, it is believed that aircraft is mobile to be stopped;
J, judge on the basis of step i: 1. airplane motion frame positions and lqrect phase with and mutually with area to account for the gross area certain More than percentage, successive frame all meets then fjstate=1, show that aircraft is leave state planestate=2;2. working as flag bit When big Mr. Yu's numerical value (default) and the big Mr. Yu's numerical value in trigger flag position, obtain aircraft for arrival state planestate=1;3. When the small Mr. Yu's numerical value of flag bit or the small Mr. Yu's numerical value in trigger flag position, aircraft is that aircraft does not go out present condition planestate=3.
Further, the video analytics server is connected by LAN/Internet with monitoring center.
Further, the front end multichannel video camera is fixed wide angle cameras, passes through interchanger and video analytics server It is connected, carries out signal acquisition, completes video decoding.
Further, it is added in template samples picture in each framing of drawing area;According to planestate numerical value Template matching is carried out, matching result preserves;When adaptation function calculates matching degree small Mr. Yu's coefficient, current region and mould are judged Plate mismatches, and is judged as that aircraft enters the region at this time, while call back function being called to notify interface;Airport is similar in order to prevent Truck is by drawing area and does not stop and false triggering detection function function logics, and spy is by the way of template matching.
It is obvious to a person skilled in the art that invention is not limited to the details of the above exemplary embodiments, Er Qie In the case where without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the present invention is by appended power Benefit requires rather than above description limits, it is intended that all by what is fallen within the meaning and scope of the equivalent elements of the claims Variation is included within the present invention.Any reference signs in the claims should not be construed as limiting the involved claims.

Claims (4)

1. a kind of aircraft based on video monitoring passes in and out berth automatic testing method, including video monitoring system, it is characterised in that: The video monitoring system includes monitoring center, video analytics server, carries out data acquisition, data processing sum number to more front ends According to displaying;
The aircraft disengaging berth automatic testing method based on video monitoring includes the following steps:
(1) airplane motion detects
The boundary rectangle frame of aircraft profile is obtained by operations such as MOG2 algorithm, gaussian filtering, morphology;
(2) aircraft state detects
Steps are as follows:
A, each frame judges that boundary rectangle frame area accounts for the certain threshold value of interface drawing area area, and default has big object to enter runway Range, from adding 1, continuous each frame all meets flag bit;
B, after step a meets, record aircraft continuously moves the aggregate-value n of pixel;
C, aircraft stops head detection frame and drawing area phase and acquisition intersecting area, it is ensured that small frame is inside big frame;
D, record phase and total pixel value m2 in region;
E, when m2 accounts for the certain area of the total pixel of small frame or more, from adding 1, continuous each frame all meets for trigger flag position;
F, n meets n and is equal to when drawing the total pixel certain percentage of frame, records the total pixel value m1 of airplane motion rectangle frame at this time, Judgment criteria when stopping as aircraft;
G, when n is greater than drawing area total pixel certain value, the total pixel value m of airplane motion rectangle frame detection block is recorded;
H, the position for starting airplane motion rectangle frame in a period of time is recorded;
I, when m is less than certain percentage m1, it is believed that aircraft is mobile to be stopped;
J, judge on the basis of step i: 1. airplane motion frame positions and lqrect phase with and mutually with area to account for the gross area certain More than percentage, successive frame all meets then fjstate=1, show that aircraft is leave state planestate=2;2. working as flag bit When big Mr. Yu's numerical value (default) and the big Mr. Yu's numerical value in trigger flag position, obtain aircraft for arrival state planestate=1;3. When the small Mr. Yu's numerical value of flag bit or the small Mr. Yu's numerical value in trigger flag position, aircraft is that aircraft does not go out present condition planestate=3.
2. a kind of aircraft based on video monitoring according to claim 1 passes in and out berth automatic testing method, feature exists In: the video analytics server is connected by LAN/Internet with monitoring center.
3. a kind of aircraft based on video monitoring according to claim 1 passes in and out berth automatic testing method, feature exists In: the front end multichannel video camera is fixed wide angle cameras, is connected by interchanger with video analytics server, and signal is carried out Video decoding is completed in acquisition.
4. a kind of aircraft based on video monitoring according to claim 1 passes in and out berth automatic testing method, feature exists In: it is added in template samples picture when in each framing of drawing area;Template matching is carried out according to planestate numerical value, Matching result preserves;When adaptation function calculates matching degree small Mr. Yu's coefficient, judge that current region and template mismatch, at this time It is judged as that aircraft enters the region, while call back function is called to notify interface.
CN201811048478.6A 2018-09-10 2018-09-10 A kind of aircraft disengaging berth automatic testing method based on video monitoring Pending CN109302580A (en)

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CN201811048478.6A CN109302580A (en) 2018-09-10 2018-09-10 A kind of aircraft disengaging berth automatic testing method based on video monitoring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811048478.6A CN109302580A (en) 2018-09-10 2018-09-10 A kind of aircraft disengaging berth automatic testing method based on video monitoring

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109887343A (en) * 2019-04-04 2019-06-14 中国民航科学技术研究院 It takes to a kind of flight and ensures node automatic collection monitoring system and method
CN111401311A (en) * 2020-04-09 2020-07-10 苏州海赛人工智能有限公司 High-altitude parabolic recognition method based on image detection
CN114822084A (en) * 2021-01-28 2022-07-29 阿里巴巴集团控股有限公司 Traffic control method, target tracking method, system, device, and storage medium

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109887343A (en) * 2019-04-04 2019-06-14 中国民航科学技术研究院 It takes to a kind of flight and ensures node automatic collection monitoring system and method
CN111401311A (en) * 2020-04-09 2020-07-10 苏州海赛人工智能有限公司 High-altitude parabolic recognition method based on image detection
CN114822084A (en) * 2021-01-28 2022-07-29 阿里巴巴集团控股有限公司 Traffic control method, target tracking method, system, device, and storage medium

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Application publication date: 20190201