WO2022220461A1 - 지능형 첨단 항공기 지상유도관제 시스템 및 방법 - Google Patents
지능형 첨단 항공기 지상유도관제 시스템 및 방법 Download PDFInfo
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- WO2022220461A1 WO2022220461A1 PCT/KR2022/004822 KR2022004822W WO2022220461A1 WO 2022220461 A1 WO2022220461 A1 WO 2022220461A1 KR 2022004822 W KR2022004822 W KR 2022004822W WO 2022220461 A1 WO2022220461 A1 WO 2022220461A1
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- aircraft
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- landing
- apron
- guidance control
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- 238000000034 method Methods 0.000 title claims abstract description 31
- 238000012544 monitoring process Methods 0.000 claims description 8
- 238000013459 approach Methods 0.000 claims description 7
- 101100536250 Homo sapiens TMEM120A gene Proteins 0.000 claims description 4
- 102100028548 Ion channel TACAN Human genes 0.000 claims description 4
- 206010000369 Accident Diseases 0.000 claims description 3
- 101000629913 Homo sapiens Translocon-associated protein subunit beta Proteins 0.000 claims description 3
- 102100026229 Translocon-associated protein subunit beta Human genes 0.000 claims description 3
- 238000004891 communication Methods 0.000 claims description 3
- 230000005856 abnormality Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
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Classifications
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0004—Transmission of traffic-related information to or from an aircraft
- G08G5/0013—Transmission of traffic-related information to or from an aircraft with a ground station
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/06—Traffic control systems for aircraft, e.g. air-traffic control [ATC] for control when on the ground
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
- G08G5/0026—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located on the ground
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0043—Traffic management of multiple aircrafts from the ground
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0047—Navigation or guidance aids for a single aircraft
- G08G5/0065—Navigation or guidance aids for a single aircraft for taking-off
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0073—Surveillance aids
- G08G5/0082—Surveillance aids for monitoring traffic from a ground station
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
- G08G5/025—Navigation or guidance aids
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/04—Anti-collision systems
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/06—Traffic control systems for aircraft, e.g. air-traffic control [ATC] for control when on the ground
- G08G5/065—Navigation or guidance aids, e.g. for taxiing or rolling
Definitions
- the present invention relates to an aircraft ground-guided control system and method, and more particularly, to an aircraft ground-guided control system and method capable of accurately identifying a location where an aircraft passes, and guiding and controlling aircraft and aviation.
- air traffic control by air traffic controllers is becoming increasingly difficult due to the enlargement of the airport, the increase in the number of departures and arrivals, and the complexity of traffic near the airport runway.
- a radar that detects only the ground of the airport is absolutely necessary even in the case of poor visibility due to the lack of visibility.
- the radar used for this purpose is called Airport Surface Detection Equipment (ASDE).
- ASDE Airport Surface Detection Equipment
- air traffic service is divided into approach control service, airfield control service, and regional control service
- airfield control service includes apron control service.
- the apron control service is responsible for guiding the aircraft to the ground at the apron of the airport, and is the task of controlling the movement of the apron between departure and arrival aircraft.
- the ground controller performs this task.
- An aerodrome such as an airport is generally divided into a movement area and a non-movement area, and the movement area consists of a maneuvering area and an apron. A part of an aerodrome used for guidance purposes.
- Aprons are designated areas of land aerodromes where passengers, mail and cargo may be loaded and unloaded, or where refueling, parking or maintenance may be performed.
- Non-moving areas are taxiway and apron areas that are not under air traffic control.
- Airfield control is divided into apron control (Ramp Control) and ground control (Ground Control).
- Apron control is a control service provided to aircraft moving within the ground apron area during the aerodrome control service, and the apron control service is performed together with the control tower that normally performs the aerodrome control service.
- Apron control duties include engine start-up, push back, and ground movement permission for entering the taxiway and control of ground handling vehicles and personnel within the apron control area.
- control should be transferred to the ground controller.
- the ground controller must hand over control to the ramp controller before the aircraft exits the taxiway and enters the apron.
- control tower acquires airport object information through radar to designate the aircraft's route, and directs the aircraft to its destination through guidance lights (aviation lights) of the designated route. induced.
- the object received through the radar has a disadvantage in that it is difficult to quickly grasp the required information of the aircraft as it receives all the information of a plurality of objects residing on the airport runway in addition to the aircraft.
- the present invention has been devised to solve the above-mentioned problems in the prior art, and an object of the present invention is to input and manage fixed location information GPS coordinate values of aviation, etc. to a server, and coordinate information of an aircraft moving in a radar in real time and
- the purpose of this invention is to provide an aircraft ground guidance control system and method that can accurately identify the location where the aircraft passes when the coordinates of the fixed aerial lights are crossed, and guide and control the aircraft and the aerial lights.
- the aircraft ground-guided control system and method for achieving the above object is to input and manage fixed location information GPS coordinate values of all aircraft that can be controlled and monitored installed in the airfield to the server, and to move from the radar in real time. It is characterized by determining whether the coordinate information of the aircraft and the coordinates of the fixed aviation, etc. are crossed, and when the coordinate information of the aircraft and the coordinates of the fixed aviation, etc. are crossed, the position of the aircraft is specified and the aircraft passing through is guided and controlled. do.
- the GPS coordinate values are input to the server at regular intervals in the apron where the guidance lights are not installed, and the position of the aircraft is tracked when the coordinate information of the aircraft and the GPS coordinate values in the apron are crossed.
- a zoom camera or drone camera is provided in the center of the landing pad and runway in the aerodrome, which is the take-off route and landing route of the aircraft, respectively, so that the fuselage, lights, landing gear, and engine of the aircraft taking off and landing can be checked even at low visibility. It is characterized in that it provides to the controller.
- 5G lidar installed on the high-speed escape route of the runway and parallel taxiway, interworking with the ground monitoring radar in real time, and accurately tracking the positions of aircraft and vehicles moving on the runway, parallel taxiway, and apron.
- the call sign is automatically attached to the aircraft to the bridge or spot. It is characterized in that the server tracks the position of the aircraft after the cycle until takeoff.
- the infrared camera is used to monitor the stopping distance according to the aircraft type and left and right driving guidance for landing It is characterized by providing information to the pilot so that the pilot can approach safely.
- the aircraft moving from the bridge for takeoff is detected by the camera sensor, and the aircraft moving from the spot detects a signal that the fixed coordinates and the moving GPS coordinates are crossed.
- the server automatically tags the call sign of the turning aircraft. It is characterized in that the server tracks the position of the aircraft until takeoff.
- tracking the location of vehicles moving within the aerodrome and apron prevents collisions between aircraft and vehicles by attaching a GPS device with two-way communication to the vehicle. characterized.
- a system linking various aviation lights installed on the ground and navigation safety equipment (ILS, VOR, DME, GP, TACAN, AMOS, PAPI) is built on the server, and the equipment malfunctions in real time. It is characterized by providing presence and absence information to the controller.
- the server calculates the landing time of the aircraft and the time of the aircraft taking off by linking the aerial radar and the ground surveillance radar to automatically control take-off and landing.
- fixed position information such as aviation, etc.
- the server and managed the coordinate information of the aircraft moving on the radar in real time and the coordinates of the fixed flight are crossed. It provides the effect of accurately identifying the location of the aircraft passing by and guiding and controlling the aircraft and aviation lights.
- FIG. 1 is a view showing an aircraft ground guidance control system according to the present invention.
- FIG. 2 is a view showing a landing pad and a runway of an aircraft ground guidance control system according to the present invention.
- FIG 3 is a view showing a state in which the 5g lidar is applied to the aircraft ground guidance control system according to the present invention.
- FIG. 4 is a view showing the apron of the aircraft ground guidance control system according to the present invention.
- FIG. 5 is a view showing a 3D image of the aircraft ground guidance control system according to the present invention.
- FIG. 1 is a view showing an aircraft ground guidance control system according to the present invention
- FIG. 2 is a view showing a landing pad and a runway of an aircraft ground guidance control system according to the present invention
- FIG. 3 is an aircraft ground guidance control system according to the present invention. It is a view showing a state in which 5g lidar is applied to the control system
- FIG. 4 is a view showing the apron of the aircraft ground guided control system according to the present invention
- FIG. 5 is a 3D image of the aircraft ground guided control system according to the present invention is a diagram showing
- the aircraft ground guided control system according to the present invention, the SSR secondary surveillance radar (100, SSR: Secondary Surveillance Radar) for monitoring the aircraft, and the ASDE ground surveillance radar for monitoring the aircraft (200).
- SSR Secondary Surveillance Radar
- ASDE ASDE ground surveillance radar
- control unit 300 for receiving the position data of the aircraft from the SSR secondary surveillance radar 100 and the ASDE ground surveillance radar 200 is further provided.
- control unit 300 monitors the equipment status such as navigation safety equipment (ALS, VOR, DME, TACAN, ILS) and weather information (AMOS) interlocking with the aviation system, and immediately delivers information to the controller when an abnormality occurs.
- equipment status such as navigation safety equipment (ALS, VOR, DME, TACAN, ILS) and weather information (AMOS) interlocking with the aviation system, and immediately delivers information to the controller when an abnormality occurs.
- AMOS weather information
- a zoom camera 500 or a drone camera 600 is provided on a landing pad in an aerodrome that is a take-off path and a landing path of an aircraft, as shown in FIG. 2 .
- the 5G lidar 700 is provided on the high-speed escape route parallel to the runway as shown in FIG.
- an infrared camera 810 and a monitor 820 are provided in the apron.
- a 3D image 900 that can accurately determine the situation of the apron in real time with the runway and the parallel taxiway is provided to the controller.
- the fixed location information GPS coordinate values of all aircraft that can be controlled and monitored installed in the aerodrome are input to the server 400 and managed, and the coordinate information of the aircraft moving from the radar 100 and 200 in real time and the fixed aviation lights It is determined whether the coordinates of are crossed, and when the coordinate information of the aircraft and the coordinates of the fixed aviation light are crossed, the position of the aircraft is specified, and the control unit 300 guides and controls the flight light through which the aircraft passes.
- the GPS coordinate values are input to the server at regular intervals in the apron where the guidance lights are not installed, and when the coordinate information of the aircraft and the GPS coordinate values in the apron are crossed, the position of the aircraft is tracked.
- the arrival and departure of the aircraft on the bridge or spot without the aviation lights in the apron are tracked in real time.
- a zoom camera 500 or a drone camera 600 is provided at the center of the landing pad and runway in the aerodrome that is the take-off path and landing path of the aircraft, respectively, so that even at low visibility, the fuselage and lights of the landing aircraft, landing gear, and engine video information that can be checked is provided to the controller.
- the 5G lidar 700 is installed on the high-speed escape route with the runway and the parallel taxiway, and it is linked with the ground monitoring radar 200 in real time to accurately track the positions of aircraft and vehicles moving on the runway and the parallel taxiway and the apron. .
- the SSR2 secondary surveillance radar 100 by linking the SSR2 secondary surveillance radar 100, the ground surveillance radar 200, and the 5G lidar 700 to track the call sign of the aircraft that has received landing permission from the air, the call sign is automatically signed even if the landing aircraft turns off the transponder.
- the server After the aircraft is parked on a bridge or spot, the server tracks the position of the aircraft until it takes off.
- the infrared camera 810 is used to guide the stopping distance according to the aircraft type and left and right driving guidance for landing to provide information to the monitor 820 so that the pilot can safely approach it.
- the aircraft moving from the bridge for takeoff is detected by the camera sensor, and the aircraft moving from the spot detects a signal that the fixed coordinates and the moving GPS coordinates cross.
- the server automatically tags the call sign of the turning aircraft The server tracks the position of the aircraft until takeoff.
- the location tracking of the vehicle moving within the aerodrome and apron prevents collisions between aircraft and vehicles by attaching a two-way communication GPS device to the vehicle, and in the event of an aircraft accident, fire trucks and ambulances entering from the outside are guided to the accident site.
- a system linking various aviation lights installed on the ground and navigation safety equipment (ILS, VOR, DME, GP, TACAN, AMOS, PAPI) is built on the server 400 and real-time Provides information on the presence or absence of equipment abnormalities to the controller.
- the server 400 calculates the landing time of the aircraft and the time of the aircraft taking off by interlocking the SSR secondary surveillance radar 100 and the ground surveillance radar 200 to automatically control take-off and landing.
- a 3D image 900 that can accurately determine the situation of the apron in real time on the runway and the parallel taxiway is provided to the controller.
- fixed location information such as aviation, etc.
- GPS coordinate values are input to the server and managed, and when the coordinate information of an aircraft moving in the radar and the coordinates of a fixed flight light are crossed in real time, the position of the aircraft is accurately identified and It guides and controls aircraft and aviation lights.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Traffic Control Systems (AREA)
Abstract
Description
Claims (12)
- 비행장내에 설치된 제어 및 감시가 가능한 모든 항공등의 고정된 위치정보 GPS 좌표값을 서버에 입력하여 관리하며,실시간으로 레이더에서 이동하는 항공기의 좌표정보와 고정된 항공등의 좌표가 크로스 되는지를 판단하며,항공기의 좌표정보와 고정된 항공등의 좌표가 크로스 되면 항공기의 위치를 특정하며 항공기가 지나는 항공등을 유도 제어하는 것을 특징으로 하는 항공기 지상유도관제 방법.
- 제 1항에 있어서,유도등화가 설치되지 않은 계류장 내에 일정한 간격으로 GPS 좌표값을 서버에 입력하고,항공기의 좌표정보와 계류장 내 GPS 좌표값이 크로스 되면 항공기의 위치를 추적하는 것을 특징으로 하는 항공기 지상유도관제 방법.
- 제 2항에 있어서,항공기를 감시하는 레이더로부터 전송되는 위도, 경도 좌표를 GPS정보로 환산하여 계류장내 항공등이 없는 브릿지나 스파트에 있는 항공기의 도착과 이탈을 실시간으로 위치를 추적하는 것을 특징으로 하는 항공기 지상유도관제 방법.
- 제 1항에 있어서,항공기의 이륙 경로, 착륙 경로인 비행장 내의 착륙대와 활주로 중심부에는 각각 줌 카메라 또는 드론 카메라를 구비하여 저시정시에도 이, 착륙하는 항공기의 동체와 라이트, 랜딩기어, 엔진을 확인할 수 있는 영상정보를 관제사에게 제공하는 것을 특징으로 하는 항공기 지상유도관제 방법.
- 제 1항에 있어서,활주로와 평행유도로 고속탈출로에 5G 라이다를 설치하여 실시간으로 지상감시 레이더와 연동하며 활주로와 평행유도로, 계류장에서 이동하는 항공기와 차량의 위치를 정확하게 추적하는 것을 특징으로 하는 항공기 지상유도관제 방법.
- 제 5항에 있어서,SSR2차감시 레이더와 지상감시 레이더, 5G 라이다를 연계하여 공중에서부터 착륙허가를 받은 항공기의 콜싸인을 추적하여 착륙하는 항공기가 트랜스 폰더를 OFF 하더라도 자동으로 콜싸인을 부착하여 항공기가 브릿지나 스파트에 주기 후 이륙할 때까지 서버에서 항공기의 위치를 추적하는 것을 특징으로 하는 항공기 지상유도관제 방법.
- 제 6항에 있어서,터치다운된 항공기가 활주로에서 고속탈출로 - 유도로 - 평행유도로 - 계류장 - 접현 장치에 접근하면 적외선 카메라를 이용하여 항공기 기종에 따른 정지거 리와 접현을 위한 좌, 우측 주행안내를 모니터에 정보를 제공하여 조종사가 안전 하게 접현 할수 있는 것을 특징으로 하는 항공기 지상유도관제 방법.
- 제 7항에 있어서,이륙을 위하여 브릿지에서 이동하는 항공기는 카메라 센서에 감지되고 스파트에서 이동하는 항공기는 고정좌표와 이동하는 GPS좌표가 크로스 되는 신호를 감 지하며 이때에는 회항하는 항공기의 콜싸인을 서버에서 자동으로 테그하여 이륙할 때까지 서버에서 항공기 위치를 추적하는 것을 특징으로 하는 항공기 지상유도관제 방법.
- 제 8항에 있어서,비행장과 계류장내에서 이동하는 차량의 위치추적은 양방향통신의 GPS장치를 차량에 부착하여 항공기와 차량의 충돌을 예방하고 항공기 사고시에는 외부로부터 진입하는 소방차와 구급차량을 사고현장으로 유도하는 것을 특징으로 하는 항공기 지상유도관제 방법.
- 제 9항에 있어서,항공기를 자동으로 안전하게 유도하기 위하여 지상에 설치한 각종항공등화와 항행안전장비(ILS, VOR, DME, GP, TACAN, AMOS, PAPI)를 연동하는 시스템을 서버에 구축하고 실시간으로 장비의 이상유, 무 정보를 관제사에게 제공하는 것을 특징으로 하는 항공기 지상유도관제 방법.
- 제 10항에 있어서,공중레이더와 지상감시레이더를 연동하여 항공기의 착륙시간과 이륙하는 항공기의 시간을 서버에서 계산하여 자동으로 이, 착륙을 관제하는 것을 특징으로 하는 항공기 지상유도관제 방법.
- 제 11항에 있어서,관제사에게 활주로와 평행유도로, 계류장의 상황을 실시간으로 정확하게 판단할 수 있는 3D영상을 제공하는 것을 특징으로 하는 항공기 지상유도관제 방법.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
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US18/554,794 US20240119850A1 (en) | 2021-04-15 | 2022-04-05 | Intelligent high-tech system and method for aircraft ground guidance and control |
CN202280027835.9A CN117157688A (zh) | 2021-04-15 | 2022-04-05 | 智能型尖端飞机地面引导管制***及方法 |
EP22788317.0A EP4325464A1 (en) | 2021-04-15 | 2022-04-05 | Intelligent high-tech system and method for aircraft ground guidance and control |
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KR1020210049131A KR102315546B1 (ko) | 2021-04-15 | 2021-04-15 | 지능형 첨단 항공기 지상유도관제 시스템 및 방법 |
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TWI828368B (zh) * | 2022-10-14 | 2024-01-01 | 訊力科技股份有限公司 | 用於偵測航空器於停機坪的行為的方法與其系統 |
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JP2007240190A (ja) * | 2006-03-06 | 2007-09-20 | Toshiba Corp | 空港用気象レーダ装置とその運用方法 |
WO2016017883A1 (ko) * | 2014-07-29 | 2016-02-04 | 한국공항공사 | 능동형 항공등화 장치 및 능동형 항공등화 방법 |
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JP2007240190A (ja) * | 2006-03-06 | 2007-09-20 | Toshiba Corp | 空港用気象レーダ装置とその運用方法 |
WO2016017883A1 (ko) * | 2014-07-29 | 2016-02-04 | 한국공항공사 | 능동형 항공등화 장치 및 능동형 항공등화 방법 |
KR20160090483A (ko) * | 2015-01-22 | 2016-08-01 | 엘에스산전 주식회사 | 항공등화제어 및 지상유도관제 시스템 |
KR101650905B1 (ko) * | 2016-04-04 | 2016-08-24 | 선진조명 주식회사 | 드론을 이용한 항공기 지상유도관제 시스템 및 방법 |
KR101656280B1 (ko) * | 2016-04-05 | 2016-09-09 | 선진조명 주식회사 | 드론을 이용한 첨단 항공기 지상유도관제 시스템 및 방법 |
KR102315546B1 (ko) * | 2021-04-15 | 2021-10-21 | 최병관 | 지능형 첨단 항공기 지상유도관제 시스템 및 방법 |
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US20240119850A1 (en) | 2024-04-11 |
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