EP0613110A1 - Système pour éviter l'incursion d'un aéroport - Google Patents

Système pour éviter l'incursion d'un aéroport Download PDF

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Publication number
EP0613110A1
EP0613110A1 EP94301262A EP94301262A EP0613110A1 EP 0613110 A1 EP0613110 A1 EP 0613110A1 EP 94301262 A EP94301262 A EP 94301262A EP 94301262 A EP94301262 A EP 94301262A EP 0613110 A1 EP0613110 A1 EP 0613110A1
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EP
European Patent Office
Prior art keywords
airport
light
incursion
recited
providing
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.)
Withdrawn
Application number
EP94301262A
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German (de)
English (en)
Inventor
Peter L. Hoover
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Raytheon Co
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Raytheon Co
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Publication of EP0613110A1 publication Critical patent/EP0613110A1/fr
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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
    • 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
    • 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

  • This invention relates to an airport ground collision avoidance system and in particular to an apparatus and method for monitoring, controlling and predicting aircraft or other vehicle movement primarily on airport taxiways and runways to avoid runway incursions.
  • a runway incursion is defined as "any occurrence at an airport involving an aircraft, vehicle, person, or object on the ground that creates a collision hazard or results in loss of separation with an aircraft taking off, intending to take off, landing, or intending to land.”
  • the U.S. Federal Administration Agency (FAA) has estimated that it can only justify the cost of ground surface radar at 29 of the top 100 airports in the United States. However, such radar only provides location information; it cannot alert the controller to possible conflicts between aircraft.
  • an airport control and monitoring system has been used to sense when an airplane reaches a certain point on a taxiway and controls switching lights on and off to indicate to the pilot when he may proceed on to a runway.
  • a system sends microwave sensor information to a computer in the control tower.
  • the computer comprises software for controlling the airport lighting and for providing fault information on the airport lighting via displays or a control panel to an operator.
  • Such a system is described in sales information provided on a Bidirectional Series 7 Transceiver (BRITEE) produced by ADB-ALNACO, Inc., A Siemens Company, of Columbus, Ohio.
  • BITEE Bidirectional Series 7 Transceiver
  • a well known approach to airport surface traffic control has been the use of scanning radars operating at high frequencies such as K-band in order to obtain adequate definition and resolution.
  • An existing airport ground traffic control equipment of that type is known in the art as Airport Surface Detection Equipment (ASDE).
  • ASDE Airport Surface Detection Equipment
  • ASDE Airport Surface Detection Equipment
  • Such equipment provides surveillance only, no discrete identification of aircraft on the surface being available. Also there is a need for a relatively high antenna tower and a relatively large rotation antenna system thereon.
  • an airport incursion avoidance system comprising a plurality of light circuits on an airport, each of the light circuits comprises a plurality of light assembly means, means for providing power to each of the plurality of light circuits and to each of the light assembly means, means in each of the light assembly means for sensing ground traffic on the airport, means for processing data received from each of the light assembly means, means for providing data communication between each of the light assembly means and the processing means, the processing means comprises means for providing a graphic display of the airport including symbols representing the ground traffic, each of the symbols having direction and velocity data displayed, the processing means further comprises means for predicting an occurrence of an airport incursion in accordance with the data received from the sensing means, and means for alerting an airport controller or aircraft pilot of the predicted airport incursion.
  • the sensing means comprises infrared detectors.
  • the light assembly means comprises light means coupled to the lines of the power providing means for lighting the airport, the infrared detectors sensing means, microprocessor means coupled to the light means, the sensing means, and the data communication means for providing processing, communication and control for the light assembly means, the microprocessor controlling a plurality of lighting patterns of the light means on the airport, and the data communication means being coupled to the microprocessor means and the lines of the power providing means.
  • the light assembly means further comprises a photocell means coupled to the microprocessor means for detecting the light intensity of the light means.
  • the light assembly means further comprises a strobe light coupled to the microprocessor means.
  • the processing means comprises redundant computers for fault tolerance operation.
  • the symbols representing the ground traffic comprise icons having a shape indicating type of aircraft or vehicle.
  • the processing means determines the locations of the symbols on the graphic display of the airport in accordance with the data receive from the light assembly means.
  • the processing means further determines a future path of the ground traffic based on a ground clearance command, the future path being shown on the graphic display.
  • the processing means for predicting an occurrence of an airport incursion comprises means for comparing position, direction and velocity of the ground traffic to predetermined separation minimums for the airport.
  • the power providing means comprises constant current power means for providing a separate line to each of the plurality of light circuits, and network bridge means coupled to the constant current power means for providing a communication channel to the processing means for each line of the constant current power means.
  • the alerting means comprises a speech synthesis unit connected to a speaker, and the alerting means also comprises a speech synthesis unit connected to a radio transmitter.
  • a method of providing an airport incursion avoidance system comprising the steps of providing a plurality of light circuits on the airport, each of the light circuits comprises a plurality of light assembly means, providing power to each of the plurality of light circuits, sensing ground traffic on the airport with means in each of the light assembly means, processing data received from each of the light assembly means in computer means, providing a graphic display of the airport comprising symbols representing the ground traffic, each of the symbols having direction and velocity data displayed, providing data communication between the computer means and each of the light assembly means, predicting an occurrence of an airport incursion in accordance with the data received from the sensing means, and alerting an airport controller or aircraft pilot of the predicted airport incursion.
  • the step of sensing the ground traffic on the airport comprises the steps of lighting the airport with a light means coupled to the microprocessor means and the power lines, providing infrared detectors for sensing the ground traffic, performing processing, communication and control within the light assembly means with a microprocessor means coupled to the light means, the sensing means and data communication means, and coupling the data communication means between the microprocessor means and the power lines.
  • the step of processing data comprises the step of operating redundant computers for fault tolerance.
  • the step of providing power comprises the steps of providing a separate line to each of the plurality of light circuits with a constant current power means, and providing a communication channel to the computer means for each line of the constant current power means using a network bridge means.
  • the step of providing a graphic display comprising symbols representing the ground traffic comprise the step of indicating a type of aircraft or vehicle with icons of various shapes.
  • the step of processing the data from each of the light assembly means comprises the step of determining a location of the symbols on the graphic display of the airport in accordance with the data.
  • the step of predicting an occurrence of an airport incursion comprises the step of determining a future path of the ground traffic in accordance with a ground clearance command and showing the future path on the graphic display.
  • FIG. 1 a block diagram of the invention of an airport vehicle incursion avoidance system 10 is shown comprising a plurality of light circuits 18 1-n , each of said light circuits 18 1-n comprises a plurality of edge light assemblies 20 1-n connected via wiring 21 1-n to a lighting vault 16 which is connected to a central computer system 12 via a wide area network 14.
  • Each of the edge light assemblies 20 1-n comprises an infrared (IR) detector vehicle sensor 50 (FIG. 2).
  • IR infrared
  • the edge light assemblies 20 1-n are generally located along side the runways and taxiways of the airport with an average 100 foot spacing and are interconnected to the lighting vault 16 by single conductor series edge light wiring 21 1-n . Each of the edge light circuits 18 1-n is powered via the wiring 21 1-n by a constant current supply 24 1-n located in the lighting vault 16.
  • LON Bridges 22 1-n interconnecting the edge light wiring 21 1-n with the Wide Area Network 14.
  • Information from a microprocessor 44 located in edge light assembly 20 1-n is coupled to the edge light wiring 21 1-n via a power line modem 54.
  • the LON bridges 22 1-n transfers message information from the edge light circuits 18 1-n via the wiring 21 1-n to the wide area network 14.
  • the wide area network 14 provides a transmission path to the central computer system 12.
  • the edge light assemblies 20 1-n and the central computer system 12 may be employed, such as radio techniques, but the present embodiment of providing data communication on the edge light wiring 21 1-n provides a low cost system for present airports.
  • the LON Bridge 22 may be embodied by devices manufactured by Echelon Corporation of Palo Alto, California.
  • the wide area network 14 may be implemented by one of ordinary skill in the art using standard Ethernet or Fiber Distributed Data Interface (FDDI) components.
  • the constant current supply 24 may be embodied by devices manufactured by Crouse-Hinds of Winslow, Connecticut.
  • FIG. 3 shows a pictorial diagram of the edge light assembly 20 1-n .
  • the edge light assembly 20 1-n comprises a bezel including an incandescent lamp 40 and an optional strobe light assembly 48 (FIG. 2) which are mounted above an electronics enclosure 43 comprising the vehicle sensor 50.
  • the electronics enclosure 43 sits on the top of a tubular shaft extending from a base support 56.
  • the light assembly bezel with lamp 40 and base support 56 may be embodied by devices manufactured by Crouse-Hinds of Winslow, Connecticut.
  • FIG. 2 A block diagram of the contents of the electronics enclosure 43 is shown in FIG. 2 which comprises a coupling transformer 53 connected to the edge light wiring 21 1-n .
  • the coupling transformer 53 provides power to both the incandescent lamp 40 via the lamp control triac 42 and the microprocessor power supply 52; in addition, the coupling transformer 53 provides a data communication path between the power line modem 54 and the LON Bridges 22 1-n via the edge light wiring 21 1-n .
  • the microprocessor 44 provides the computational power to run the internal software program that controls the edge light assemblies 20 1-n .
  • the microprocessor 44 is powered by the microprocessor power supply 52.
  • the microprocessor 44 is also connected to the microprocessor 44.
  • the microprocessor 44 is used to control the incandescent edge light 40 intensity and optional strobe light assembly 48.
  • the use of the microprocessor 44 in each light assembly 20 1-n allows complete addressable control over every light on the field.
  • the microprocessor 44 may be embodied by a VLSI device manufactured by Echelon Corporation of Palo Alto, California 94304, called the Neuron® chip.
  • the senor 50 in the present embodiment comprises an infrared (IR) detector and in other embodiments may comprise other devices such as proximity detectors, CCD cameras, microwave motion detectors, inductance loops, or laser beams.
  • the program in the microprocessor 44 is responsible for the initial filtering of the sensor data received from the sensor 50 and responsible for the transmission of such data to the,central computer system 12.
  • the sensor 50 must perform the following functions: detect a stationary object, detect a moving object, have a range at least half the width of the runway or taxiway, be low power and be immune to false alarms. This system design does not rely on just one type of sensor. Since sensor fusion functions are performed within the central computer system 12, data inputs from all different types of sensors are acceptable.
  • Each sensor relays a different view of what is happening on the airfield and the central computer system 12 combines them.
  • the initial sensor used is an IR proximity detector based around a piezoelectric strip. These are the kind of sensors you use at home to turn on your flood lights when heat and/or movement is detected.
  • an analog-to-digital converter readily known in the art may be used to interface with the microprocessor 44.
  • Another proximity detector that can be used is based around a microwave Gunn diode oscillator. These are currently in use in such applications as Intrusion Alarms, Door Openers, Distance Measurement, Collision Warning, Rail Switching, etc. These types of sensors have a drawback because they are not passive devices and care needs to be taken to select frequencies that would not interfere with other airport equipment. Finally, in locations such as the hold position lines on taxiways, solid state laser and detector combinations could be used between adjacent taxiway lights. These sensor systems create a beam that when broken would identify the location of the front wheel of the airplane. This type of detector would be used in those locations where the absolute position of a vehicle was needed. The laser beam would be modulated by the microprocessor 44 to avoid the detector being fooled by any other stray radiation.
  • FIG. 2 and FIG. 4 a portion of an airport runway 64 or taxiway is shown having a plurality of edge light assemblies 201 ⁇ 8 positioned along each side of the runway or taxiway for detecting various size airplanes or vehicles 60, 62.
  • the dashed lines represent the coverage area of the sensors 50 located in each edge light assembly 201 ⁇ 8 positioned along each side of the runway 64 or taxiway to insure detection of any airplane 60, 62 or other vehicles traveling on such runway 64 or taxiway.
  • the edge light assemblies 20 1-n comprising the sensor 50 are logically connected together in such a way that an entire airport is sensitized to the movement of vehicles. Node to node communication takes place to verify and identify the location of the vehicles.
  • Edge light assemblies without a sensor electronics unit 43
  • taxiway power wiring currently exist along taxiways, runways and open areas of airports, therefore, the sensor electronics unit 43 is readily added to existing edge lights and existing taxiway power wiring without the inconvenience and expense of closing down runways and taxiways while installing new cabling.
  • the central computer system 12 is generally located at a control tower or terminal area of an airport and is interconnected to the LON Bridges 22 1-n located in the lighting vault 16 with a Wide Area Network 14.
  • the central computer system 12 comprises two redundant computers, computer #1 26 and computer #2 28 for fault tolerance, the display 30, speech synthesis units 29 & 31, alert lights 34, keyboard 27 and a speech recognition unit 33, all of these elements being interconnected by the wide area network 14 for the transfer of information.
  • the two computers 26 and 28 communicate with the microprocessors 44 located in the edge light assemblies 20 1-n . Data received from the edge light assembly 20 1-n microprocessors 44 are used as an input to a sensor fusion software module 101 (FIG.
  • the central computer system 12 may be embodied by devices manufactured by IBM Corporation of White Plains, New York.
  • the Wide Area Network 14 may be embodied by devices manufactured by 3Com Corporation of Santa Clara, California.
  • the speech synthesis units 29, 31 and the speech recognition unit 33 may be embodied by devices manufactured by BBN of Cambridge, Massachusetts.
  • the speech synthesis unit 29 is coupled to a speaker 32. Limited information is sent to the speech synthesis unit 29 via the wide area network 14 to provide the capability to give an air traffic controller a verbal alert.
  • the speech synthesis unit 31 is coupled to a radio 37 having an antenna 39 to provide the capability to give the pilots a verbal alert.
  • the voice commands from the air traffic controller to the pilots are captured by microphone 35 and sent to the pilots via radio 36 and antenna 38.
  • a tap is made and the speech information is sent to both the radio 36 and the speech recognition unit 33 which is programmed to recognize the limited air traffic control vocabulary used by a controller. This includes airline names, aircraft type, the numbers 0-9, the name of the taxiways and runways and various short phrases such as "hold short", "expedite” and "give way to.”
  • the output of the speech recognition unit 33 is fed to the computers 26, 28.
  • the power line modem 54 provides a data communication path over the edge light wiring 21 1-n for the microprocessor 44. This two way path is used for the passing of command and control information between the various edge light assemblies 20 1-n and the central computer system 12.
  • a power line transceiver module in the power line modem 54 is used to provide a data channel. These modules use a carrier current approach to create the data channel. Power line modems that operate at carrier frequencies in the 100 to 450 Khz band are available from many manufacturers. These modems provide digital communication paths at data rates of up to 10,000 bits per second utilizing direct sequence spread spectrum modulation. They conform to FCC power line carrier requirements for conducted emissions, and can work with up to 55 dB of power line attenuation.
  • the power line modem 54 may be embodied by a device manufactured by Echelon Corporation of Palo Alto, California 94304, called the PLT-10 Power Line Transceiver Module.
  • the data channel provides a transport layer or lowest layer of the open system interconnection (OSI) protocol used in the data network.
  • OSI open system interconnection
  • the Neuron® chip which implements the microprocessor 44 contains all of the firmware required to implement a 7 layer OSI protocol.
  • the Neuron® chips When interconnected via an appropriate medium the Neuron® chips automatically communicate with one another using a robust Collision Sense Multiple Access (CSMA) protocol with forward error corrections, error checking and automatic retransmission of missed messages (ARQ).
  • CSMA Collision Sense Multiple Access
  • the command and control information is placed in data packets and sent over the network in accordance with the 7 Layer OSI protocol. All messages generated by the microprocessor 44 and destined for the central computer system 12 are received by the network bridge 22 via the power lines 21 1-n and routed to the central computer system 12 over the wide area network 14.
  • the Neuron® chip of the microprocessor 44 comprises three processors (not shown) and the firmware required to support a full 6 layer open systems interconnection (OSI) protocol.
  • OSI layer open systems interconnection
  • the user is allocated one of the processors for the application code.
  • the other two processors give the application program access to all of the other Neuron® chips in the network. This access creates a Local Operating Network or LON.
  • a LON can be thought of as a high level local area network LAN.
  • the use of the Neuron® chip for the implementation of this invention reduces the amount of custom hardware and software that otherwise would have to be developed.
  • Data from the sensor electronic unit 43 of the edge light assemblies 20 1-n is coupled to the central computer system 12 via the existing airport taxiway lighting power wiring 21.
  • Using the existing edge light power line to transfer the sensor data into a LON network has many advantages. As previously pointed out, the reuse of the existing edge lights eliminates the inconvenience and expense of closing down runways and taxiways while running new cable and provides for a low cost system.
  • the Neuron® chip allows the edge light assemblies 20 1-n to automatically communicate with each other at the applications level. This is accomplished through network variables which allow individual Neuron® chips to pass data between themselves.
  • Each Neuron® 'C' program comprises both local and network variables.
  • the local variables are used by the Neuron® program as a scratch pad memory.
  • the network variables are used by the Neuron® program in one of two ways, either as a network output variables or a network input variables. Both kinds of variables can be initialized, evaluated and modified locally. The difference comes into play in that once a network output variable is modified, network messages are automatically sent to each network input variable that is linked to that output variable. This variable linking is done at installation time.
  • the sensor 50 function has two output variables: prelim_detect 70 and confirmed_detect 72.
  • the idea here is to have one output trigger whenever the sensor 50 detects movement. The other output does not trigger unless the local sensor and the sensor on the edge light across the runway both spot movement. Only when the detection is confirmed will the signal be fed back to the central computer system 12.
  • This technique of confirmation helps to reduce false alarms in order to implement this technique the adjacent sensor 50 has an input variable called adj_prelim_detect 78 that is used to receive the other sensors prelim_detect output 70.
  • Other input variables are upstream_detect 74 and downstream_detect 76 which are used when chaining adjacent sensors together. Also needed is a detector_sensitivity 80 input that is used by the central computer system 12 to control the detection ability of the sensor 50.
  • the incandescent light 40 requires two network variables, one input and the other an output variable.
  • the input variable light_level 84 would be used to control the light's brightness. The range would be OFF or 0% all the way to FULL ON or 100%. This range from 0% to 100% would be made in 0.5% steps. Since the edge light assembly 20 1-n also contains the photocell 46, an output variable light_failure 84 is created to signal that the lamp did not obtain the desired brightness.
  • the strobe light 48 requires three input variables.
  • the strobe-mode 86 variable is used to select either the OFF, SEQUENTIAL, or ALTERNATE flash modes. Since the two flash modes require a distinct pattern to be created, two input variables active_delay 88 and flash_delay 90 are used to time align the strobe flashes. By setting these individual delay factors and then addressing the Neuron® chips as a group, allows the creation of a field strobe pattern with just one command.
  • FIG. 7 a block diagram of an interconnection of network variables for a plurality of edge light assemblies 20 1-n located on both sides of a runway is shown, each of the edge light assemblies 20 1-n comprising a microprocessor 44.
  • Each Neuron® program in the microprocessor 44 is designed with certain network input and output variables. The user writes the code for the Neurone® chips in the microprocessor 44 assuming that the inputs are supplied and that the outputs are used. To create an actual network the user has to "wire up" the network by interconnecting the individual nodes with a software linker. The resulting distributed process is best shown in schematic form, and a portion of the network interconnect matrix is shown in Figure 7.
  • the prelim_detect 70 output of a sensor node 441 is connected to the adj_primary_detect 92 input of the sensor node 444 across the taxiway. This is used as a means to verify actual detections and eliminate false reports.
  • the communications link between these two nodes 441 and 444 is part of the distributed processing. The two nodes communicate among themselves without involving the central computer system 12. If in the automatic mode or if instructed by the controller, the system will also alert the pilots via audio and visual indications.
  • the central computer system 12 tracks the movement of vehicles as they pass from the sensor 50 to sensor 50 in each edge light assembly 20 1-n .
  • the system can track position, velocity and heading of all aircraft or vehicles based upon the sensor 50 readings. New vehicles are entered into the system either upon leaving a boarding gate or landing. Unknown vehicles are also tracked automatically. Since taxiway and runway lights are normally across from each other on the pavement (as shown in FIG. 4 and FIG. 7), the microprocessor 44 in each edge lights assembly 20 1-n is programmed to combine their sensor 50 inputs and agree before reporting a contact.
  • a further refinement is to have the microprocessor 44 check with the edge light assemblies 20 1-n on either side of them to see if their sensors 50 had detected the vehicle. This allows a vehicle to be handed off from sensor electronic unit 43 to sensor electronic unit 43 of each edge light assembly 20 1-n as it travels down the taxiway. This also assures that vehicle position reports remain consistent. Vehicle velocity may also be calculated by using the distance between sensors, the sensor pattern and the time between detections.
  • the display 30 is a color monitor which provides a graphical display of the airport, a portion of which is shown in FIG. 8. This is accomplished by storing a map of the airport in the redundant computers 26 and 28 in a digital format.
  • the display 30 shows the location of airplanes or vehicles as they are detected by the sensors 50 mounted in the edge light assemblies 20 1-n along each taxiway and runway or other airport surface areas. All aircraft or vehicles on the airport surface are displayed as icons, with the shape of the icons being determined by the vehicle type. Vehicle position is shown by the location of the icon on the screen. Vehicle direction is shown by either the orientation of the icon or by an arrow emanating from the icon. Vehicle status is conveyed by the color of the icon. The future path of the vehicle as provided by the ground clearance command entered via the controllers microphone 35 is shown as a colored line on the display 30. The status of all field lights including each edge light 20 1-n in each edge light circuit 18 1-n is shown via color on the display 30.
  • object orientated software provides the basis for building a model of an airport.
  • the automatic inheritance feature allows a data structure to be defined once for each object and then replicated automatically for each instance of that object. Automatic flow down assures that elements of the data base are not corrupted due to typing errors. It also assures that the code is regular and structured.
  • Rule based object oriented programming makes it difficult to create unintelligible "spaghetti code.”
  • Object oriented programming allows the runways, taxiways, aircraft and sensors, to be decoded directly as objects.
  • Each of these objects contains attributes. Some of these attributes are fixed like runway 22R or flight UA347, and some are variable like vehicle status and position.
  • Table 1 shows a list of objects with corresponding attributes. Each physical object that is important to the runway incursion problem is modeled.
  • the basic airplane or vehicle tracking algorithm is shown in Table 2 in a Program Design Language (PDL).
  • PDL Program Design Language
  • the algorithm which handles sensor fusion, incursion avoidance and safety alerts is shown in a single program even though it is implemented as distributed system using both the central computer system 12 and the sensor microprocessors 44.
  • the control of taxiway lighting intensity is usually done by placing all the lights on the same series circuit and then regulating the current in that circuit.
  • the intensity of the lamp 40 is controlled by sending a message with the light intensity value to the microprocessor 44 located within the light assembly 20 1-n .
  • the message allows for intensity settings in the range of 0 to 100% in 0.5% steps.
  • the use of photocell 46 to check the light output allows a return message to be sent if the bulb does not respond. This in turn generates a maintenance report on the light.
  • the strobe light 48 provides an additional optional capability under program control of the microprocessor 44.
  • Each of the microprocessors 44 in the edge light assemblies 20 is individually addressable. This means every lamp on the field is controlled individually by the central computer system 12.
  • the system 10 can be programmed to provide an Active Runway Indicator by using the strobe lights 48 in those edge light assemblies 20 1-n located on the runway 64 to continue the approach light "rabbit" strobe pattern all the way down the runway.
  • This lighting pattern could be turned-on as a plane is cleared for landing and then turned-off after the aircraft has touched down. A pilot approaching the runway along an intersecting taxiway would be alerted in a clear and unambiguous way that the runway was active and should not be crossed.
  • the main computers 26, 28 could switch the runway strobe lights 48 from the "rabbit" pattern to a pattern that alternatively flashes either side of the runway in a wig-wag fashion.
  • a switch to this pattern would be interpreted by the pilot of an arriving aircraft as a wave off and a signal to go around.
  • the abrupt switch in the pattern of the strobes would be instantaneously picked up by the air crew in time for them to initiate an aborted landing procedure.
  • the main computers 26,28 can control the taxiway lamps 40 as the means for guiding aircraft on the ground during CAT III conditions. Since the intensity of the taxiway lamps 40 can be controlled remotely, the lamps just in front of an aircraft could be intensified or flashed as a means of guiding it to the terminal.
  • a short sequence of the "rabbit" pattern may be programmed into the taxiway strobes just in front of the aircraft. At intersections, either the unwanted paths may have their lamps turned off or the entrance to the proper section of taxiway may flash directing the pilot to head in that direction.
  • the unwanted paths may have their lamps turned off or the entrance to the proper section of taxiway may flash directing the pilot to head in that direction.
  • FIG. 9 a block diagram is shown of the data flow within the system 10 (as shown in FIG. 1 and FIG. 5).
  • the software modules are shown that are used to process the data within the computers 26, 28 of the central computer system 12.
  • the tracking of aircraft and other vehicles on the airport operates under the control of a sensor fusion software module 101 which resides in the computers 26, 28.
  • the sensor fusion software module 101 receives data from the plurality of sensors 50, a sensor 50 being located in each edge light assembly 20 1-n which reports the heat level detected, and this software module 101 combines this information through the use of rule based artificial intelligence to create a complete picture of all ground traffic at the airport on a display 30 of the central computer system 12.
  • the tracking algorithm starts a track upon the first report of a sensor 50 detecting a heat level that is above the ambient background level of radiation. This detection is then verified by checking the heat level reported by the sensor directly across the pavement from the first reporting sensor. This secondary reading is used to confirm the vehicle detected and to eliminate false alarms. After a vehicle has been confirmed the sensors adjacent to the first reporting sensor are queried for changes in their detected heat level. As soon as one of the adjacent sensors detects a rise in heat level a direction vector for the vehicle can be established. This process continues as the vehicle is handed off from sensor to sensor in a bucket brigade fashion as shown in FIG. 7. Vehicle speed can be roughly determined by calculating the time between vehicle detection by adjacent sensors.
  • This information is combined with information from a system data base on the location of each sensor to calculate the velocity of the target. Due to hot exhaust or jet blast, the sensors behind the vehicle may not return to a background level immediately. Because of these condition, the algorithm only uses the first four sensors (two on either side of the taxiway) to calculate the vehicles position. The vehicle is always assumed to be on the centerline of the pavement and between the first four reporting sensors.
  • Vehicle identification can be added to the track either manually or automatically by an automated source that can identify a vehicle by its position. An example would be prior knowledge of the next aircraft to land on a particular runway.
  • Tracks are ended when a vehicle leaves the detection system. This can occur in one of two ways. The first way is that the vehicle leaves the area covered by the sensors 50. This is determined by a vehicle track moving in the direction of a gateway sensor and then a lack of detection after the gateway sensor has lost contact. A second way to leave the detection system is for a track to be lost in the middle of a sensor array. This can occur when an aircraft departs or a vehicle runs onto the grass. Takeoff scenarios can be determined by calculating the speed of the vehicle just before detection was lost. If the vehicle speed was increasing and above rotation speed then the aircraft is assumed to have taken off. If not then the vehicle is assumed to have gone on to the grass and an alarm is sounded.
  • the ground clearance routing function is performed by the speech recognition unit 33 along with the ground clearance compliance verifier software module 103 running on the computers 26, 28.
  • This software module 103 comprises a vehicle identification routine, clearance path routing, clearance checking routine and a path checking routine.
  • the vehicle identification routine is used to receive the airline name and flight number (i.e. "Delta 374") from the speech recognition unit 33 and it highlights the icon of that aircraft on the graphic display of the airport on display 30.
  • the airline name and flight number i.e. "Delta 374”
  • the clearance path routine takes the remainder of the controller's phrase (i.e. "outer taxiway to echo, hold short of runway 15 Left") and provides a graphical display of the clearance on the display 30 showing the airport.
  • the clearance checking routine checks the clearance path for possible conflict with other clearances and vehicles. If a conflict is found the portion of the path that would cause an incursion is highlighted in a blinking red and an audible indication is given to the controller via speaker 32.
  • the path checking routine checks the actual path of the vehicle as detected by the sensors 50 after the clearance path has been entered into the computers 26, 28 and it monitors the actual path for any deviation. If this routine detects that a vehicle has strayed from the assigned course, the vehicle icon on the graphic display of the airport flashes and an audible indicator is given to the controller via speaker 32 and optionally the vehicle operator via radio 37.
  • the airport vehicle incursion avoidance system 10 operates under the control of safety logic routines which reside in the collision detection software module 104 running on computers 26, 28.
  • the safety logic routines receive data from the sensor fusion software module 101 via the tracker software module 102 location program and interpret this information through the use of rule based artificial intelligence to predict possible collisions or runway incursions. This information is then used by the central computer system 12 to alert tower controllers, aircraft pilots and truck operators to the possibility of a runway incursion.
  • the tower controllers are alerted by the display 30 along with a computer synthesized voice message via speaker 32.
  • Ground traffic is alerted by a combination of traffic lights, flashing lights, stop bars and other alert lights 34, lamps 40 and 48, and computer generated voice commands broadcast via radio 36.
  • Knowledge based problems are also called fuzzy problems and their solutions depend upon both program logic and an interface engine that can dynamically create a decision tree, selecting which heuristics are most appropriate for the specific case being considered.
  • Rule based systems broaden the scope of possible applications. They allow designers to incorporate judgement and experience, and to take a consistent solution approach across an entire problem set.
  • the programming of the rule based incursion detections software is very straight forward.
  • the rules are written in English allowing the experts, in this case the tower personnel and the pilots, to review the system at an understandable level.
  • Another feature of the rule based system is that the rules stand alone. They can be added, deleted or modified without affecting the rest of the code. This is almost impossible to do with code that is created from scratch.
  • the block diagram shows the data flow between the functional elements within the system 10 (FIG. 1).
  • Vehicles are detected by the sensor 50 in each of the edge light assemblies 20 1-n .
  • This information is passed over the local operating network (LON) via edge light wiring 21 1-n to the LON bridges 22 1-n .
  • the individual message packets are then passed to the redundant computers 26 and 28 over the wide area network (WAN) 14 to the WAN interface 108.
  • the message packet is checked and verified by a message parser software module 100.
  • the contents of the message are then sent to the sensor fusion software module 101.
  • the sensor fusion software module 101 is used to keep track of the status of all the sensors 50 on the airport; it filters and verifies the data from the airport and stores a representative picture of the sensor array in a memory. This information is used directly by the display 30 to show which sensors 50 are responding and used by the tracker software module 102.
  • the tracker software module 102 uses the sensor status information to determine which sensor 50 reports correspond to actual vehicles. In addition, as the sensor reports and status change, the tracker software module 102 identifies movement of the vehicles and produces a target location and direction output. This information is used by the display 30 in order to display the appropriate vehicle icon on the screen.
  • the location and direction of the vehicle is also used by the collision detection software module 104.
  • This module checks all of the vehicles on the ground and plots their expected course. If any two targets are on intersecting paths, this software module generates operator alerts by using the display 30, the alert lights 34, the speech synthesis unit 29 coupled to the associated speaker 32, and the speech synthesis unit 31 coupled to radio 37 which is coupled to antenna 39.
  • this software module 103 receives the ground clearance commands from the controller's microphone 35 via the speech recognition unit 33. Once the cleared route has been determined, it is stored in the ground clearance compliance verifier software module 103 and used for comparison to the actual route taken by the vehicle. If the information received from the tracker software module 102 shows that the vehicle has deviated from its assigned course, this software module 103 generates operator alerts by using the display 30, the alert lights 34, the speech synthesis unit 29 coupled to speaker 32, and the speech synthesis unit 31 coupled to radio 37 which is coupled to antenna 39.
  • the keyboard 27 is connected to a keyboard parser software module 109.
  • a command has been verified by the keyboard parser software module 109, it is used to change display 30 options and to reconfigure the sensors and network parameters.
  • a network configuration data base 106 is updated with these reconfiguration commands. This information is then turned into LON message packets by the command message generator 107 and sent to the edge light assemblies 20 1-n via the WAN interface 108 and the LON bridges 22 1-n .
EP94301262A 1993-02-26 1994-02-23 Système pour éviter l'incursion d'un aéroport Withdrawn EP0613110A1 (fr)

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US6161097A (en) * 1997-08-11 2000-12-12 The United Sates Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Automated traffic management system and method
US7667647B2 (en) 1999-03-05 2010-02-23 Era Systems Corporation Extension of aircraft tracking and positive identification from movement areas into non-movement areas
US7739167B2 (en) 1999-03-05 2010-06-15 Era Systems Corporation Automated management of airport revenues
US7777675B2 (en) 1999-03-05 2010-08-17 Era Systems Corporation Deployable passive broadband aircraft tracking
US7782256B2 (en) 1999-03-05 2010-08-24 Era Systems Corporation Enhanced passive coherent location techniques to track and identify UAVs, UCAVs, MAVs, and other objects
US7889133B2 (en) 1999-03-05 2011-02-15 Itt Manufacturing Enterprises, Inc. Multilateration enhancements for noise and operations management
US7908077B2 (en) 2003-06-10 2011-03-15 Itt Manufacturing Enterprises, Inc. Land use compatibility planning software
US7965227B2 (en) 2006-05-08 2011-06-21 Era Systems, Inc. Aircraft tracking using low cost tagging as a discriminator
US8072382B2 (en) 1999-03-05 2011-12-06 Sra International, Inc. Method and apparatus for ADS-B validation, active and passive multilateration, and elliptical surveillance
US8203486B1 (en) 1999-03-05 2012-06-19 Omnipol A.S. Transmitter independent techniques to extend the performance of passive coherent location
US8446321B2 (en) 1999-03-05 2013-05-21 Omnipol A.S. Deployable intelligence and tracking system for homeland security and search and rescue
CN110654558A (zh) * 2018-06-28 2020-01-07 劳斯莱斯有限公司 航空站系统和方法
CN111867202A (zh) * 2020-06-23 2020-10-30 中国民用航空总局第二研究所 防止跑道侵入的禁止进入排灯控制方法以及系统
CN115599125A (zh) * 2022-12-14 2023-01-13 电子科技大学（Cn） 一种基于边缘计算的助航灯光控制策略选择方法

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RU2158963C1 (ru) * 1999-12-21 2000-11-10 Закрытое акционерное общество "ИСТ ЛАЙН-ХЭНДЛИНГ" Способ оперативного сопровождения и управления наземными транспортными средствами аэропорта
KR101119887B1 (ko) * 2010-01-27 2012-02-29 한국교통연구원 지능형 항공등화 제어시스템

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US6161097A (en) * 1997-08-11 2000-12-12 The United Sates Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Automated traffic management system and method
US8072382B2 (en) 1999-03-05 2011-12-06 Sra International, Inc. Method and apparatus for ADS-B validation, active and passive multilateration, and elliptical surveillance
US8446321B2 (en) 1999-03-05 2013-05-21 Omnipol A.S. Deployable intelligence and tracking system for homeland security and search and rescue
US7777675B2 (en) 1999-03-05 2010-08-17 Era Systems Corporation Deployable passive broadband aircraft tracking
US7782256B2 (en) 1999-03-05 2010-08-24 Era Systems Corporation Enhanced passive coherent location techniques to track and identify UAVs, UCAVs, MAVs, and other objects
US8203486B1 (en) 1999-03-05 2012-06-19 Omnipol A.S. Transmitter independent techniques to extend the performance of passive coherent location
US7739167B2 (en) 1999-03-05 2010-06-15 Era Systems Corporation Automated management of airport revenues
US7667647B2 (en) 1999-03-05 2010-02-23 Era Systems Corporation Extension of aircraft tracking and positive identification from movement areas into non-movement areas
US7889133B2 (en) 1999-03-05 2011-02-15 Itt Manufacturing Enterprises, Inc. Multilateration enhancements for noise and operations management
US7908077B2 (en) 2003-06-10 2011-03-15 Itt Manufacturing Enterprises, Inc. Land use compatibility planning software
US7965227B2 (en) 2006-05-08 2011-06-21 Era Systems, Inc. Aircraft tracking using low cost tagging as a discriminator
CN110654558A (zh) * 2018-06-28 2020-01-07 劳斯莱斯有限公司 航空站系统和方法
EP3590848A1 (fr) * 2018-06-28 2020-01-08 Rolls-Royce plc Système et procédé d'aérodrome
US11113979B2 (en) 2018-06-28 2021-09-07 Rolls-Royce Plc Aerodrome system and method
CN111867202A (zh) * 2020-06-23 2020-10-30 中国民用航空总局第二研究所 防止跑道侵入的禁止进入排灯控制方法以及系统
CN115599125A (zh) * 2022-12-14 2023-01-13 电子科技大学（Cn） 一种基于边缘计算的助航灯光控制策略选择方法
CN115599125B (zh) * 2022-12-14 2023-04-07 电子科技大学 一种基于边缘计算的助航灯光控制策略选择方法

Also Published As

Publication number Publication date
CA2114610A1 (fr) 1994-08-27
NO940625L (no) 1994-08-29
NO940625D0 (no) 1994-02-24
JPH06301898A (ja) 1994-10-28

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