CN205451355U - Airport runway safety precaution system - Google Patents
Airport runway safety precaution system Download PDFInfo
- Publication number
- CN205451355U CN205451355U CN201620154677.5U CN201620154677U CN205451355U CN 205451355 U CN205451355 U CN 205451355U CN 201620154677 U CN201620154677 U CN 201620154677U CN 205451355 U CN205451355 U CN 205451355U
- Authority
- CN
- China
- Prior art keywords
- runway
- sensor
- receptor
- emitter
- data processing
- 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.)
- Expired - Fee Related
Links
Landscapes
- Traffic Control Systems (AREA)
Abstract
The utility model provides an airport runway safety precaution system, system include sensor network, data converting unit, data interface unit, switch, data processing service ware, human -computer interaction unit and acousto -optic warning unit, sensor network connects through data converting unit, data interface unit, switch and data processing service ware in proper order, human -computer interaction unit and acousto -optic warning unit all link to each other with the data processing service ware. Sensor network prevents invading a set of of protection zone perimeter or multiunit sensor including setting up at the runway, and every group sensor is including adorning at both sides transmitter and receiver by inspection path respectively. The protection zone is prevented invading by the runway, waits for the partial and runway end safety zone between position and the actual runway including tu mian district, the runway of each 75 meters within range of runway center line marking both sides. The utility model discloses a sensor network invades the runway and detects and alarm information, and economical and practical, safe and reliable, configuration are in a flexible way.
Description
Technical field
This utility model relates to a kind of airfield runway safety pre-warning system.
Background technology
Along with developing rapidly of global civil aviation business, flight flow constantly increases, and aerial and ground conflict is the most frequent, and especially ground runway safety problem is on the rise, and runway invades also to be increased year by year with the unsafe incidents such as exotic intrusion.Runway is safely the basis of whole air transport system safety, and runway intrusion is typical runway safety problem, and it very likely causes serious airport security accident.Existing as follows about runway intrusion research:
(1) definition that runway invades
In the U.S., runway is invaded and is defined as by FAA: occur in airfield runway environment, relating to ground aviation device, vehicle, personnel or object, to taking off, standby for takeoff, landing or preparing the airborne vehicle of landing produces risk of collision or causes losing any event of minimum personal distance.Civil aviation organization of Canada uses different methods to define runway and invades: unexpected or the airborne vehicle, vehicle or the personnel that authorize without permission or intended in the case of, enter or attempt close to any hazard event of runway being currently in use.Both definition all invade just for the runway activating runway, do not include that the substantial amounts of runway to inactive runway invades.
For promoting international cooperation; jointly improve runway and invade risk; on November 25th, 2004; International Civil Aviation Organization (ICAO) invades RI (RunwayIncursion) to runway and has carried out unified definition; definition regulation: runway invades any airborne vehicle, vehicle or the personnel referring to occur on airport and is strayed into and specifies for aircraft lands and the situation in land protection district taken off, invades for runway.Wherein, runway, taxiway and the part between runway holding fix and actual runway broadly fall into the protection zone specified.Hereafter, this definition comes into force in the world.
(2) reason that runway invades is caused
The reason causing runway to invade has a lot, and pilot, traffic controller, vehicle driver and pedestrian may cause runway to invade.After runway intrusion event is investigated by FAA, its reason is classified as three-type-person for error: pilot's deviation (PD), operation error (OE) and vehicle/pedestrian's deviation (V/PD).Pilot's deviation (PD) refers to the behavior that pilot causes runway to invade because violating Aircraft regulation.Such as: pilot, when by the entrance airport, course line specified, observes air traffic control (ATC) about forbidding passing through the instruction of the runway in being currently in use.Running error (OE) is owing to ATC cannot coordinate the result that orderly management causes to airborne vehicle.Such as: between a. two frame or multi rack airborne vehicle or between airborne vehicle and barrier (including the vehicle on runway, equipment and personnel), be less than applicable minimum interval；B. airborne vehicle is allowed to land or take off on the runway closed.Vehicle/pedestrian's deviation (V/PD) refers to that surface car and personnel ratify without ATC, enters runway zone of action, the behavior that interference airborne vehicle runs without authorization.
In actual environment, human error merely causes a part of reason that runway invades, it is responsible, such as that other factors many also invade event to runway: the air traffic amount etc. that severe meteorological condition, the complexity of computer aided, infrastructure and system design is unreasonable, growing.Being not isolated between these factors, runway intrusion accident is probably and is caused by chain of events, is many factors and artificial origin coefficient result.
(3) research is invaded about runway is anti-both at home and abroad
For the most serious runway penetration phenomenon, each research institution has the most put into substantial amounts of energy and has researched and developed the technical equipment preventing runway from invading.The emphasis made great efforts at present is concentrated mainly on two aspects: provide the particular device of positional information for pilot；Runway is provided to invade the warning device of alarm for air traffic controller in time.
In the U.S., FAA the runway formulated invades the generation preventing plan to be devoted to be reduced runway intrusion by American National spatial domain system (NAS).RIRP (RunwayIncursionReductionProgram runway invades and reduces plan) system is made up of parts such as flight navigation system, invasion display terminals, can be that pilot, air traffic controller and traffic above-ground facility etc. provide real-time status report.The blank of this system has put into engineering test and performance test in International airport, Butterworth fort, Dallas.RIRP needs the technology of a kind of advanced person to support, and present Local Area Augmentation System LAAS is the first-selection considered.
The RIPS (RunwayIncursionPreventionSystem runway invades anti-locking system) of NASA is the flight deck display system of a kind of advanced person, runway, taxiway and runway conflict warning etc. can be shown on head up displays, mainly improved the ability of the aspects such as state of ground real-time report, flight location and pilot's early warning by technological means.With the difference of RIRP, it is that it can pass through HUD (flat aobvious technology) and EMM (electronics moving map) in real time to aircraft report Current terrestrial state.The realization of this function is completed by the early warning technology such as ADS-B (Automatic dependent surveillance broadcast), STIS-B (traffic above-ground information service broadcast), LAAS.
The use of RIRP and RIPS both equipment will transform cost to spend substantial contribution as to aircraft cabin, and this has certain limitation for most airport, will be carried out promoting the use of of global range, in addition it is also necessary to a process the longest.
RWSLs (RunwayStateLamps runway status lamp) is another technology that FAA is testing.Status lamp by a series of be embedded in runway take off wait lamp and runway threshold lights form.Once detecting that potential runway invades event, runway status lamp can send direct visual alarm to pilot at once.They are full automatic warning systems, it is not necessary to controller is operated manually.If the runway entered or pass through is unsafe, red runway threshold lights will be lit；If it is unsafe that runway is used for taking off, red wait lantern festival of taking off is lit.RSWLs system can not be used alone, and it also needs the support of the runway condition detecting device of other advanced persons, and both combine, and could assess any potential conflict on airport.
The X-type airport surface detection equipment (ASDE-X) of Sensis company of U.S. exploitation is a kind of ground-based radar system, realize airport target by ground monitoring radar to position, and track route is passed on control display screen, the decision support about preventing runway from invading is provided for air traffic controller, FAA selectes 35 relatively busy airport of the U.S., progressively installs ASDE-X system equipment.AMASS (Aerodrome Traffic Zone territory security system) is significant signal based on radar, reduces at misty rain sky accuracy, and it is the additional intensifier of ASDE-3 radar, and they are all supermatic computer systems.Both combine, and controller can be made to observe the ruuning situation on airport more accurately, in order to take the necessary measure in time to avoid runway to invade the generation of event.The most domestic Guangzhou's Baiyun International Airport employs the ground radar alarm equipment based on scene surveillance radar of similar ASDE-X, can be reddened and play caution sound by label and be reminded the ground conflict being likely to occur, and plays the effect of auxiliary monitoring.
The another kind formulated by ICAO senior scene mobilizing exercises based on scene police radar guides control system A-SMGCS, can be on the premise of not changing the existing layout in airport, utilize advanced technological means, the equipment such as such as ground surveillance radar (SMR), multipoint location system (MDS), Automatic dependent surveillance broadcast (ADS-B), movement area and terminal area to whole airport realize seamless covering, provide a real time imaging clearly about traffic for controlling officer.A-SMGCS can be aircraft and Working vehicle provides accurate in Aerodrome Traffic Zone territory and guides and regulation and control, more can avoid causing because of visual error between aircraft and vehicle being spaced situation deviation occur.Owing to A-SMGCS system can be that various airdrome scene mobile management provides efficient and round-the-clock Managed Solution, American-European a lot of country is the most successively as the important component part of airport configuration, such as Munich, Germany airport, airport, Britain Heathrow and airport, Canadian Toronto etc., the busiest airport, Atlanta has used A-SMGCS to run.
Although anti-runway is invaded by these several airdrome scenes based on scene police radar management system can play some effects, but defect is, warning signal need to notify pilot by air traffic controller, and very limited for alerting the time of process.The airborne vehicle that one frame slides the most just may can be crossed runway and shut down line index, enters runway.In the shortest time, runway to be avoided to invade event by a series of event.First, system must detect intrusion conflict；Then warning is sent to controller；Controller to be analyzed after receiving warning signal judging, middle accepts through signal, processes, the link such as transmission, and collision accident may have occurred and that here.And scene surveillance radar covering power is less, clutter reflections the decoy produced is more, there is blind area, and more sensitive to weather, can produce a large amount of clutter, easily produce false alarm during blowing and raining.
In addition, those described above equipment all has a common feature, and these equipment manufacturing cost are the most sufficiently expensive, installs and occupation mode is the most sufficiently complex, only large airport just can try the expense that burden installation is safeguarded, is not appropriate for promoting the use of on a lot of middle-size and small-size airports.
For the defect of these above-mentioned equipment, there is research institution to consider increasingly mature technology of wireless sensing network and be incorporated in airport security management system.Radio sensing network, as a kind of brand-new Information acquisition technology, has reliability height, low cost, is prone to the features such as extension, is very suitable for managing for airport security.As domestic Civil Aviation University of China uses the airport special purpose vehicle alignment system of technology of wireless sensing network exploitation; by being placed on special vehicle and the sensor node of fixed position, airport; achieve the location of special vehicle in airplane parking area; dangerous vehicle is carried out early warning, to avoid the generation of vehicle collision aircraft accident.
Radio sensing network is applied to airdrome control, and the most anti-runway invades field, is a kind of brand-new trial, and existing achievement in research is the most little.Due to the particularity of airport environment, the existing certain advantage of application of technology of wireless sensing network, also there is the difficulty of realization, in addition it is also necessary to further further investigate.
Therefore, from technological means, develop a set of runway and invade detection warning system, grasp runway state in time, invading for runway provides a kind of solution economical and practical, flexibility and reliability imperative, this is invaded, by runway, the accident caused to reducing, and improves the safety of civil aviaton of China flight, and tool is of great significance.
Utility model content
This utility model is solved the technical problem that to be, for the deficiencies in the prior art, a kind of airfield runway safety pre-warning system and method are provided, carry out runway based on radio sensing network and invade detection alarm, invade for runway and a kind of economical and practical, safe and reliable technical solution is provided, and can carry out system configuration flexibly according to the practical situation on different airports, improve, with this, the level that China prevents runway from invading.
The technical solution of the utility model is:
A kind of airfield runway safety pre-warning system, including sensor network, Date Conversion Unit, data interface unit, switch, data processing server, man-machine interaction unit and acousto-optic warning unit；
Sensor network is connected with switch with data interface unit through Date Conversion Unit successively；Switch and data processing server connect；The detection signal of sensor network is sent to data processing server through Date Conversion Unit, data interface unit and switch successively；
Man-machine interaction unit is all connected with data processing server with acousto-optic warning unit；
Described sensor network includes one or more groups sensor being arranged on runway anti-intrusion protection zone circumference [i.e. border a, b, c, d, e, f, g, h, i, j, k, l in Fig. 2]; often group sensor includes emitter and the receptor being mutually matched a pair; emitter and receptor are attached separately to the both sides in detected path; when object is by detected path; signal between emitter and receptor is blocked, and receiver actions one control signal of output is to data processing server；Runway anti-intrusion protection zone; i.e. detected land protection district (arranging according to actual needs) includes the part between Tu Mianqu, runway holding fix and actual runway in the range of each L rice of runway center line marking both sides and runway end safety area; runway end safety area is that runway two ends respectively stretch out a length of 300 meters; width is the region of L rice, and runway end safety area is symmetrical in runway center line marking extended line；L value is 75, and when movement area index is F level (4F level runway), L value is 107.5；
The aircraft movement area reference code on airport is different with entering nearly mode, waits that level ground, runway holding fix or the road holding fix minimum range away from runway center line marking are the most different, specifically arranges as shown in table 1:
Table 1: wait level ground, runway holding fix or the road holding fix minimum range away from runway center line marking
Note: if a. waits that the height above sea level of level ground, runway holding fix or road holding fix, higher than runway threshold, the most often exceeds 1m, distance increases 5m；As this height above sea level can reduce 5m less than runway threshold, the lowest lm, this distance, but be as the criterion with prominent interior transition face.
B. in order to avoid interference radio aids equipment, particularly downslide navigation channel and course facility, distance should be increased when needing to avoid the sensitizing range of instrument landing system.
C., when movement area index is F level (4F level runway), this distance should be 107.5m.
Taxiway/runway intersection wait level ground, runway holding fix or and road holding fix and the runway center line marking of runway center line marking intersection between distance should meet the setting in table 1.For precision approach runway, it is necessary to make the aircraft of wait or vehicle not disturb the operating of radio aids equipment.
Described sensor network includes that being arranged on the first sensor outside runway holding fix [is i.e. arranged on the sensor 2 outside the runway holding fix of No. 18 runways in Fig. 4, and it is arranged on the sensor 1 outside the runway holding fix of No. 36 runways], the receptor of first sensor and emitter are attached separately to the outer both sides of runway holding fix, and receptor is parallel with runway centerline with the line of emitter；For detecting whether there is object (mainly including other exotics such as airborne vehicle, vehicle or personnel) to pass in and out runway；Data processing server obtains control license data by man-machine interaction unit, when not obtaining control license, detects that object passes in and out runway, then triggers acousto-optic warning unit and produce warning information.
The sensor network also includes that the second sensor being arranged on runway holding fix border is [as being arranged on the sensor inside sensor 2 in Fig. 5, and it is arranged on the sensor inside sensor 1], the receptor of the second sensor and emitter include being attached separately to runway holding fix boundaries on either side, and receptor is parallel with runway centerline with the line of emitter；
If the light path of the second sensor and first sensor is successively；It is blocked the most from inside to outside, object has been described from runway out, then trigger prompting message；If the light path of first sensor and the second sensor is successively；It is blocked the most from outside to inside, has illustrated that object enters runway, if not obtaining control license, then trigger acousto-optic warning unit and produce warning information；First sensor is blocked before the second sensor is blocked and does not alerts, and the second sensor is blocked before first sensor is blocked and does not alerts, and the most single being blocked does not alerts.
Time state sensor network and also include being arranged on the 3rd sensor on the runway boundary at distance runway head L1 rice [as Fig. 5 is arranged on the sensor 5 at the runway head L1 rice of No. 18 runways of distance, and it is arranged on the sensor 10 at the runway head L1 rice of No. 36 runways of distance], the receptor of the 3rd sensor and emitter are attached separately on border, runway both sides, and receptor is vertical with runway centerline with the line of emitter；For monitoring the aircraft takeoff state on this runway, if the light path of the 3rd sensor is blocked, triggers sliding race of aircraft takeoff and remind；The span of described L1 is 100 300；Preferably value is 150, and the 3rd sensor is arranged on the runway boundary at 150 meters of runway head of distance, has both considered the length of airborne vehicle, it is also considered that the promptness of warning, and the accuracy of warning is higher；
Described sensor network also includes being arranged on runway with front end, junction, road junction (according to direction of advance when aircraft takeoff or landing, after airborne vehicle through position be front end) runway boundary on the 4th sensor [in such as Fig. 5, be arranged on the sensor 6,7 of No. 36 runways and front end, junction, G, F road junction, and it is arranged on the sensor 8,9 of No. 18 runways and front end, junction, E, D road junction], the receptor of the 4th sensor and emitter include being attached separately on border, runway both sides, and receptor is vertical with runway centerline with the line of emitter；Land state for monitoring the airborne vehicle on this runway, if the light path of the 4th sensor is blocked, illustrates that this road junction broken through by airborne vehicle, do not depart from from this road junction, trigger airborne vehicle and do not depart from from this road junction and remind；
Described sensor network also includes two groups of the 5th adjacent sensors and the 6th sensor [sensor 11,12,13,14,15,16 in such as Fig. 6 being arranged on other road junction connected with runway in addition to road junction, runway holding fix place；11,12,13,14,15,16 respectively include adjacent two sensors], the emitter in the 5th sensor and the 6th sensor is all parallel with runway centerline with the line of receptor；In 5th sensor and the 6th sensor; the sensor nearer with runway centerline is the 5th sensor; 5th sensor distance runway centerline L rice [the i.e. the 5th sensor is arranged on the border of runway anti-intrusion protection zone, and the 6th sensor is arranged on the outside of runway anti-intrusion protection zone]；If the light path of the 5th sensor and the 6th sensor is successively；It is blocked the most from inside to outside, triggers the prompting message that airborne vehicle departs from from this road junction；6th sensor and the light path of the 5th sensor；The most successively it is blocked, triggers warning information；5th sensor is blocked before the 6th sensor is blocked and does not alerts, and the 6th sensor is blocked before the 5th sensor is blocked and does not alerts, and the most single being blocked does not alerts.
The sensor network also includes being arranged on 4 unidirectional emission probe [such as 3 in Fig. 5 and 4] of the assuming diamond in shape arrangement outside runway head, lands airborne vehicle for monitoring dynamic, triggers airborne vehicle and lands prompting.
The sensor network also includes being arranged on the 7th sensor [as being arranged on the sensor 31 on the border, runway anti-intrusion protection zone at runway 300 meters of the boundary in front of No. 36 runways of distance in Fig. 5, and being arranged on the sensor 32 on border, runway anti-intrusion protection zone at runway 300 meters of the boundary in front of No. 18 runways of distance] on the border, runway anti-intrusion protection zone at distance runway 300 meters of boundary in front；The emitter of the 7th sensor is vertical with runway centerline with receptor line, and the distance of emitter and receptor is 2L rice；
Described sensor network also includes the 8th sensor being arranged on the border, runway anti-intrusion protection zone in landing airdrome length direction；8th sensor is made up of the sensor of multiple segmentations；The detection path of the sensor of multiple segmentations is continuous, and the line in detection path is parallel with runway centerline, and the wire length (distance between the detection path ending end of the i.e. the 8th sensor) in detection path is that landing airdrome length adds 600 meters；
Described sensor network also includes borderline 9th sensor in part both sides that is separately positioned between runway holding fix and actual runway and the tenth sensor [such as the borderline sensor in part both sides 28 and 27 being arranged in Fig. 6 between the runway holding fix of No. 18 runways and actual runway, and the borderline sensor in part both sides 25 and 26 being arranged between the runway holding fix of No. 36 runways and actual runway]；The emitter of the 9th sensor and the tenth sensor is all vertical with runway centerline with the line of receptor, emitter and receptor one of both are arranged on runway holding fix, and the distance between emitter and receptor subtracts L rice equal to the distance of runway holding fix to runway centerline；
Described sensor network also includes that the 11st sensor of the portion outboard being arranged between runway holding fix and actual runway is [as being arranged on the sensor 30 of the portion outboard between the runway holding fix of No. 18 runways and actual runway in Fig. 6, and the sensor 29 of the portion outboard being arranged between the runway holding fix of No. 36 runways and actual runway], parallel with the extension line of runway centerline with the line of receptor and distance runway centerline the distance of the emitter of the 11st sensor is L rice, distance between emitter and receptor is 300 meters, emitter and receptor are arranged on border, runway anti-intrusion protection zone；
Being provided with the 12nd sensor [sensor 17,18,19,20,21,22 and 23 in such as Fig. 6] between road junction adjacent on border, runway anti-intrusion protection zone, the emitter of the 12nd sensor is parallel with runway centerline with the line of receptor；
If the light path of one of above-mentioned 7th sensor, the 8th sensor, the 9th sensor, the tenth sensor, the 11st sensor and the 12nd sensor is blocked, trigger warning information.
Above-mentioned airfield runway safety pre-warning system, also includes control tower operation management system (TOMS)；Data processing server communicates to connect with control tower operation management system (TOMS) through switch and fire wall；Air station flight flight is dynamically sent to data processing server by control tower operation management system (TOMS).
Above-mentioned airfield runway safety pre-warning system, also includes blank pipe many radars automated system；Data processing server communicates to connect with blank pipe many radars automated system；Blank pipe many radars automated system obtains airport in real time and lands the elevation information of flight, and sends data processing server to.
Airfield runway safety pre-warning system work process of the present utility model is:
The Database Lists stored on data processing server, preserves alarm set in advance and controls logic in Database Lists；
Data processing server obtains the airborne vehicle real-time dynamic data on control tower operation management system (TOMS) by network through fire wall, tower controller controls logic according to the alarm of airborne vehicle Real-time and Dynamic and setting, by man-machine interaction unit import control license data [sensor control signal] to data processing server, the alarm suppression or the alarm that control each sensor in sensor network activate；
According to the sensor detection signal of alarm state of activation, data processing server controls whether acousto-optic warning unit is reminded or alert.
Described alarm controls logic:
(1) according to the airborne vehicle real-time dynamic data on control tower operation management system (TOMS), if airborne vehicle is the state of landing on this runway, then control the 4th sensor [sensor 6,7 such as No. 36 runways corresponding in Fig. 5 with G, F road junction, and the sensor 8,9 at corresponding No. 18 runways and E, D road junction] alarm activates, 3rd sensor [such as the sensor 5 of No. 18 runways corresponding in Fig. 5, and the sensor 10 of corresponding No. 36 runways] alarm suppression；4th sensor detects when airborne vehicle passes through, then trigger the prompting message that airborne vehicle does not departs from from corresponding road junction；When airborne vehicle the 5th and the 6th sensor [sensor 11,12,13,14,15,16 as in Fig. 6] successively detects that airborne vehicle passes through, then trigger airborne vehicle and departed from prompting message from this road junction；When airborne vehicle without departing from time [the 5th and the 6th sensor does not monitors airborne vehicle and departs from from each road junction], now issue departure from port aircraft takeoff instruction, i.e. control tower operation management system (TOMS) operation aircraft takeoff state, then trigger warning information；
Airborne vehicle real-time dynamic data according to control tower operation management system (TOMS), if airborne vehicle is takeoff condition on this runway, then control the 3rd sensor [sensor 5 such as No. 18 runways corresponding in Fig. 5, and the sensor 10 of No. 36 runways of correspondence] alarm activation, 4th sensor alarms suppression [such as the sensor 6,7 of No. 36 runways corresponding in Fig. 5 with G, F road junction, and the sensor 8,9 at corresponding No. 18 runways and E, D road junction]；3rd sensor detects when airborne vehicle passes through, and triggers aircraft takeoff sliding race prompting message；
(2) if the light path of the second sensor and first sensor successively [；Sensor 2 or 1 in i.e. Fig. 6 is from inside to outside] it is blocked, trigger prompting message；If the light path priority of first sensor and the second sensor [；Sensor 2 or 1 in i.e. Fig. 6 is from outside to inside] it is blocked, illustrate that object enters runway, triggered acousto-optic warning unit and produce warning information；First sensor is blocked before the second sensor is blocked and does not alerts, and the second sensor is blocked before first sensor is blocked and does not alerts, and the most single being blocked does not alerts；
If the light path of the 5th sensor and the 6th sensor successively [such as the sensor 11,12,13,14,15 or 16 in Fig. 6 from inside to outside] is blocked, trigger the prompting message that airborne vehicle departs from from corresponding road junction；The light path of the 6th sensor and the 5th sensor [；Successively it is blocked such as the sensor 11,12,13,14,15 or 16 in Fig. 6 from outside to inside], triggers warning information；5th sensor is blocked before the 6th sensor is blocked and does not alerts, and the 6th sensor is blocked before the 5th sensor is blocked and does not alerts, and the most single being blocked does not alerts；
In 7th sensor to the second sensor any one group, just triggers warning information as long as being then blocked；
(3) if controller enters runway license to airborne vehicle, vehicle or personnel [on this runway, airborne vehicle is " LINEUP " state], then control the second sensor and first sensor alarm suppression, the alarm suppression time is 1 minute, and after 1 minute, the second sensor and first sensor alarm activate；
(4) if this runway is in the lock state, then all the sensors alarm suppression, after runway unlocks, alarm activates.
Data processing server communicates to connect with blank pipe many radars automated system；Obtain in real time from blank pipe many radars automated system and land flight elevation information, land flight when 10 kilometers of runway head of distance, the air position of highly 610 meters, corresponding runway holding fix forbids that flight or exotic invade runway, regardless of whether obtain control license, first sensor and the second sensor detect when airborne vehicle, vehicle or personnel enter runway, all can trigger warning information；
When 4 unidirectional emission probe arranged at runway two sense land flight fly over time, trigger audible and visual alarm unit and produce prompting message, informing that controller lands airborne vehicle will ground connection.
The control tower operation management system (TOMS), data processing server and the Choice of Sensors that relate to this utility model below illustrate.
(1) control tower operation management system (TOMS)
Control tower operation management system is the tower control system of future generation based on electrical steps list, by integrated air traffic control automation system, scene surveillance radar system, Flight Information processing system, aeronautical meteorology information service system data, based on electrical steps list management and running platform, use brand new digital regulatory model, it is achieved airport scope flight is flown to, from application clearance, ground taxi, runway, the dynamic Whole Course Management of schedule flight that control is transferred.
(2) data processing server
The information that sensor network nodes collects the most all will be sent to data processing server, data processing server mainly realizes the management to whole network and provides reliable runway status information for staff, facilitate it accurately to understand the situation that runway invades, thus make rapidly correct decision-making.Data processing server functional block diagram is as shown in Figure 8.
Data processing server, based on PC, provides the user the interactive interface of close friend.This interface can show that situation is monitored in the sensor node networking of runway each protection zone in real time, thus realize management personnel and to the monitoring in real time of network and manage.Data processing server can also select the node transmitting control commands to specific region according to the actually used situation of runway, be monitored this region.
Data processing server mainly includes user management module, database management module, monitoring and inquiry display module, network management module and audible and visual alarm control module, and population structure is as shown above.
(3) sensor type
Sensor can select ABH tetra-light beam infrared opposite-type detector and laser correlative detector；
1, ABH tetra-light beam infrared opposite-type detector
ABH tetra-light beam infrared opposite-type detector is made up of active infrared transmitter and passive infrared receiver, infrared beam between transmitter and receiver can produce alarm condition when being interdicted completely or interdict by given percentage ratio, ABH tetra-light beam infrared opposite-type detector has the following characteristics that adjustable beam breaking time；Multiple application c-type relay, integrated form breaking-proof switch；Open when shell is removed；Optional beam frequency, is suitable to distance and stacking application；Numeral method received signal strength, easy debugging；Width funtion and energy-saving design；"AND" OR technique designs；Digital communication function；High-accuracy Fresnel Lenses technology；High-seal is waterproof: IP65；Wide angle optical correcting range: level ± 90 ° is vertical ± 10 °；Digital filtering, environment self-adaption function, rate of false alarm is preferably minimized；Beam interference minimumization, is applicable to various complex environment.
The specifications parameter of ABH tetra-light beam infrared opposite-type detector is:
2, laser correlative detector
Laser correlative detector is made up of laser transmitter, laser receiver, with the laser beam of a branch of or multi beam independence as warning line.It is arranged on runway anti-intrusion protection zone periphery, constitutes distance warning line or tight light wall.Compared with similar active detector, having the following advantages (1) laser characteristics excellence, quality is higher, is obviously enhanced the adaptability of extreme climate environment；(2) laser monochromaticity is strong, and good directionality, each other without crosstalk, can meet the security protection requirement of higher level；(3) set up defences flexible configuration, take precautions against precision high；(5) strong interference immunity, noiseless to miscellaneous equipment；(6) easy construction, cost performance is high.
The technical specification of laser correlative detector is:
Beneficial effect:
Current runway invasion is problem the most in the urgent need to address in the middle of airport security is run, existing miscoordination monitors that means (such as scene surveillance radar) structure is complicated, quantities is great and involves great expense, and collaborative supervision means (such as automatic dependent surveillance) need airborne secondary radar answering machine could obtain aircraft identification, and scene vehicle cannot obtain mark, therefore aircraft can only be monitored, and other exotics can not be monitored and invade, this utility model can overcome the problems referred to above, invade for runway and provide a kind of economical and practical, safe and reliable technical solution, and have the advantage that
1, the sensor node distribution in each region of airfield runway and radio sensing network form: each group of sensor includes that receives device and a discharger; many group sensor ordered distribution are at airport ground protection zone plane geometry end points, it is achieved radio sensing network covers whole airport ground protection zone.By selecting suitable latticed form to carry out data transmission, when runway invades event generation, pass to tower controller with warning information.
2, in order to ensure that runway invades the reliability of detection, use multisensor a target multifrequency nature to be detected simultaneously, can have with the sensor detection form used: infrared, the specific region target acquisition etc. of millimetre-wave radar, laser intrusion-detector.
Multisensor is used to obtain target multi-faceted detection information, realize the Real-time Collection of wireless data, transmission, processed by multi-sensor information fusion, the runway being likely to occur is invaded event and automatically detects, judge and alert, runway can be improved and invade the accuracy of detection.
4, data processing server passes through Network Isolation fire wall, obtains in real time the sliding state information of all aircrafts being in airfield runway land protection region from control tower operation management system (TOMS), including: slide, wait, skid off, go-cart etc.；The alarm suppression or the alarm that arrange corresponding region sensor accordingly enable.Realize the personal settings of sensor alarms logic control function.
6, system components module has low cost, reliability height, the advantage of good stability.
This utility model is the monitoring to airport ground protection zone, therefore, is equally applicable to the pattern in the case of many runways and bisecting runway.System can be configured neatly by different airports according to own situation, is actually needed to meet, and this is that other monitoring systems current cannot complete to improve, with this, level that China prevents runway from invading.
Accompanying drawing explanation
Fig. 1 is land protection section model；
Fig. 2 is this utility model runway anti-intrusion protection zone model；
Fig. 3 is system hardware structure figure of the present utility model；
Fig. 4 is the transducer arrangements of pattern one in embodiment；
Fig. 5 is the transducer arrangements of pattern two in embodiment；
Fig. 6 is the transducer arrangements of pattern three in embodiment；
Fig. 7 is this utility model aerial reconnaissance module principle figure；
Fig. 8 is this utility model data processing server functional block diagram；
Description of reference numerals:
In figure, numbering 1 to 30 is sensor.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, this utility model is described in more detail.
Below as a example by certain airfield runway domestic, airfield runway safety pre-warning system of the present utility model and method are illustrated.
(1) runway anti-intrusion protection zone model is set:
According to the definition of International Civil Aviation Organization, runway invades any airborne vehicle, vehicle or the personnel referring to occur on airport and is strayed into and specifies for aircraft lands and the situation in land protection district taken off.Land protection district includes Tu Mianqu, ILS sensitizing range, ILS critical zone and the runway end safety area in the range of airfield runway and the taxiway part between applicable runway holding fix and actual runway, each 75m in runway center line marking both sides, as shown in Figure 1.
This utility model is according to airfield runway form and is actually needed, and sets runway anti-intrusion protection zone model, and i.e. detected land protection district is as shown in Figure 2；In figure, a, b, c, d, e, f, g, h, i, j, k, l are the border of runway anti-intrusion protection zone model；As in figure 2 it is shown, sensor can be arranged in region a, b, c, d, e, f, g, h, i, j, k, l, form radio sensing network, cover the whole runway with airfield runway as core anti-intrusion protection zone.Wherein region e, i is runway holding fix.
System hardware structure figure of the present utility model is as it is shown on figure 3, the sensor network of a-l of runway anti-intrusion protection zone forms sensor network, and its detection signal accesses after data interface module through Date Conversion Unit, enters data processing server.The Database Lists stored on data processing server, the alarm preserving the different airborne vehicle on corresponding control tower operation management system (TOMS) set in advance in Database Lists the most different controls logic；
Tower controller issues control order, and dynamic by control tower operation management system (TOMS) operation airborne vehicle；Data processing server obtains the real-time operation airborne vehicle dynamic data on control tower operation management system (TOMS) by network through fire wall, control logic according to the alarm in the Database Lists on data processing server, control the alarm of each sensor in sensor network by man-machine interaction unit and suppress or alarm enable.
Meanwhile, the Sensor monitoring that the alarm of each region enables invades to illegal object, will immediately provide warning position to data processing server, and trigger and provide audible and visual alarm information, the relevant information that prompting tower controller generation runway invades or exotic invades in time.
(2) transducer arrangements pattern and corresponding alarm control logic
Often group sensor includes emitter and the receptor being mutually matched a pair；When airborne vehicle wheel is through sensor, block sensor signal transmission, cause warning information or prompting message.In order to this utility model is more fully described, the present embodiment provides three kinds of transducer arrangements patterns to illustrate.Airfield runway in embodiment, according to two towards, numbering be respectively No. 18 runways and No. 36 runways.
Pattern one:
Being respectively provided with first sensor outside 36, No. 18 runway holding fixs, i.e. sensor 1 and 2, sensor 1 is parallel with 2 equal runway centerlines, is arranged on the outer both sides of runway holding fix.Controller permits that, when airborne vehicle, vehicle, personnel pass in and out runway, system does not alerts；Otherwise, alarm.
Pattern two:
Pattern two is with the difference of pattern one, increases and arranges sensor 3,4,5,6,7,8,9,10,11,12,13,14,15,16；
Wherein sensor 5,6,7,8,9,10 respectively includes one group of sensor；Sensor 11,12,13,14,15,16 respectively includes adjacent and parallel two sensors；Sensor 1,2 also includes adjacent and parallel two sensors；Wherein a group in two sensors is on the border of runway anti-intrusion protection zone, and another set is outside runway anti-intrusion protection zone.
The position description of each sensor:
Sensor 3,4 is by the unidirectional emission probe composition of 4 layouts that assume diamond in shape, and device is at the runway head of 36, No. 18 runways.
Sensor 11,12,13,14,15,16, is arranged on the position that land protection district is tangent with each road junction, a length of each road junction width.Parallel with runway centerline, inner sensors is arranged on runway anti-intrusion protection zone boundary, and outer sensors is adjacent with the sensor of inner side.
Sensor 10,5: vertical with runway centerline, it is arranged on runway both sides, the respectively distance 150 meters of distance 36,18 runway head.
Sensor 9,8,7,6: vertical with runway centerline, is arranged on runway both sides；9,8 respectively on the right side of D, E road junction, i.e. road junction and the outside of runway junction；7,6 respectively on the left of F, G road junction, i.e. road junction and the outside of runway junction.
Alarm controls logic: (1) sensor 1,3,6,7,10 is monitoring sensor during No. 36 runways of use；Monitoring sensor when sensor 2,4,5,8,9 is to use No. 18 runways.When using No. 36 runways, related sensor alarm or the prompting message of No. 18 are suppressed.When using No. 18 runways, related sensor alarm or the prompting message of No. 36 are suppressed.And sensor 11,12,13,14,15,16, no matter when using any bar runway, when signal is blocked, all can trigger warning information.
Illustrating as a example by during to use No. 36 runways, sensor 6,7 is that on No. 36 runways, airborne vehicle lands monitoring, and sensor 10 is that aircraft states of taking off on No. 36 runways monitors；According to control tower operation management system (TOMS) data, if airborne vehicle is " LANDING " landing state, sensor 6 and 7 state of activation；If airborne vehicle is " TAKEOFF " takeoff condition, sensor 10 is state of activation, and No. 18 runways are the most as the same.On No. 36 runways airborne vehicle for land state time: airborne vehicle pass through 7, then trigger airborne vehicle not from F road junction depart from prompting message；Airborne vehicle passes through 6, then trigger airborne vehicle not from the prompting message at G road junction；Airborne vehicle passes through 14, then trigger airborne vehicle and departed from prompting message from F road junction, and airborne vehicle is as the same by 15,16.When airborne vehicle is departure from port state on No. 36 runways: when airborne vehicle is by 10, trigger the sliding race prompting message of airborne vehicle.
If 1. airborne vehicle departs from from F road junction, then trigger and remind prompting message, such as: " F departing from "；
2. if airborne vehicle departs from from G road junction, trigger prompting message the most successively, such as: " F without departing from ", " G departing from "；
3. if airborne vehicle departs from from H road junction, trigger prompting message successively, such as: " F without departing from ", " G without departing from ", wait airborne vehicle after H road junction departs from, then trigger " H departing from ".
When airborne vehicle without departing from time (native system does not monitors airborne vehicle and departs from from each road junction), now issue departure from port aircraft takeoff instruction, i.e. control tower operation management system (TOMS) operation TAKEOFF takeoff condition, then trigger warning information.
5,8,9 functions on No. 18 runways are as the same, 8,9 when 18 airborne vehicle landing devices break through E, D road junction trigger prompting message, 5 No. 18 aircraft takeoff by time trigger prompting message.
(2) 1,2,11,12,13,14,15,16 respectively include two sensors.Wherein, 11,12,13,14,15 or 16 are successively blocked from inside to outside, trigger prompting message；Successively it is blocked from outside to inside, triggers warning information.Sensor 1 or 2 is when controller permits that airborne vehicle, vehicle or personnel enter runway, and alarm suppresses；Otherwise, alarm activates.Inner sensors is blocked before outer sensors is blocked and does not alerts, and outer sensors is blocked before inner side is blocked and does not alerts, and the most single being blocked does not alerts；And 5,6,7,8,9,10 respectively include one group of sensor, just trigger alarm as long as being blocked.
(3) 2 and 1 is each two sensors being located at 18 and No. 36 holding points respectively.When using 36 runway, in TOMS, airborne vehicle is " LINEUP " state [i.e. control license], and sensor alarms is suppressed, and the suppression time is 1 minute, and after 1 minute, alarm activates.No. 18 runways are the most as the same.
(4) when runway is in the lock state, all alarms are suppressed.
(5) non-full Runway operation, as runway is entered at the H road junction of No. 18 runways of airborne vehicle, the C road junction of No. 36 runways.As a example by No. 36 runways: when performing non-full Runway operation, controller is set to C road junction by control tower operation management system (TOMS) the holding point position of taxi circuit, data processing server introduces data from control tower operation management system (TOMS), thus updates and alert logic accordingly.
(6) invade if there is runway or exotic invades, ALM time 60s.In particular cases, controller command airborne vehicle from be rapidly separated be redirected back into runway time, it may appear that ALM, simultaneously eject a dialog box " acknowledge？", after controller confirms, alarm disappears.That is any one runway can trigger dialog box " acknowledge while invading and triggering alarm？" appearance.
(7) aerial reconnaissance module: 3,4 are respectively used to monitor 36, No. 18 runways and land the dynamic of airborne vehicle, trigger the airborne vehicle prompting message by runway head.As shown in Figure 7, obtain in real time from blank pipe many radars automated system land flight (judgement land homeplate flight first can from transit telegram machine obtain airport of destination be the flight of homeplate, then obtain from homeplate secondary radar targetpath analysis) elevation information, 10 kilometers of runway head of distance, highly 610 meters (flight that lands intercept and capture 3 degree of elevations angle of blind landing glide path signal) air position time, corresponding runway holding fix forbids that flight or exotic invade runway, the sensor of runway holding fix detect.4 unidirectional emission probes are set at runway two, the upwards Vertical Launch detectable signal from ground, ground location point was leaped when landing flight, sensed by 4 unidirectional emission probes, and trigger tower control room audible and visual alarm unit immediately and produce acoustic and light information prompting, inform that controller lands airborne vehicle by runway head.
Because main runway invades event and occurs mainly in each road junction, this pattern, in each road junction placement sensor, effectively can invade event to runway and be monitored and alert.
It is noted that the height of each sensor have to meet " civil airport movement area technical standard ".
Pattern three:
Pattern three is with the difference of pattern two, increases placement sensor 17,18,19,20,21,22,23,24,25,26,27,28,29,30,31,32；With many group sensors, anti-for runway intrusion protection zone being enclosed, monitoring runway anti-intrusion protection zone, prevents runway from invading in all directions.
Sensor 17,18,19,20,21,22,23,24,25,26,27,28,29,30,31,32 is respectively made up of one group of sensor, just triggers runway intrusion alarm as long as being blocked；Special instruction is 24 to be realized by multiple sensor segments.
The position description of each sensor:
Sensor 32,31 300 meters of distance 18,36 runway head respectively is vertical with runway centerline.
Sensor 24 is parallel with runway centerline, and the distance between emitter and receptor is landing airdrome length+600 meters.
Sensor 29,30 is parallel with runway centerline, and distance is 300 meters.
Sensor 25,26,27,28: vertical with runway centerline, the distance between emitter and receptor is holding point to the distance of runway centerline subtracts the distance of L rice.
Sensor 17,18,19,20,21,22,23: parallel with runway centerline.
Special instruction: this utility model is the monitoring to airport ground protection zone, therefore, is equally applicable to the pattern in the case of many runways and bisecting runway.
Claims (9)
1. an airfield runway safety pre-warning system, it is characterised in that include sensor network, Date Conversion Unit, data interface unit, switch, data processing server, man-machine interaction unit and acousto-optic warning unit；
Sensor network is connected with switch with data interface unit through Date Conversion Unit successively；Switch and data processing server connect；The detection signal of sensor network is sent to data processing server through Date Conversion Unit, data interface unit and switch successively；
Man-machine interaction unit is all connected with data processing server with acousto-optic warning unit；
Described sensor network includes one or more groups sensor being arranged on runway anti-intrusion protection zone circumference; often group sensor includes emitter and the receptor being mutually matched a pair; emitter and receptor are attached separately to the both sides in detected path; when object is by detected path; signal between emitter and receptor is blocked, and receiver actions one control signal of output is to data processing server；Runway anti-intrusion protection zone; i.e. detected land protection district includes the part between Tu Mianqu, runway holding fix and actual runway in the range of each L rice of runway center line marking both sides and runway end safety area; runway end safety area is that runway two ends respectively stretch out a length of 300 meters; width is the region of L rice, and runway end safety area is symmetrical in runway center line marking extended line；L value is 75, and when movement area index is F level, L value is 107.5；
Described sensor network includes being arranged on the first sensor outside runway holding fix, and the receptor of first sensor and emitter are attached separately to the outer both sides of runway holding fix, and receptor is parallel with runway centerline with the line of emitter；For detecting whether there is object to pass in and out runway；Data processing server obtains control license data by man-machine interaction unit, when not obtaining control license, detects that object passes in and out runway, then triggers acousto-optic warning unit and produce warning information.
Airfield runway safety pre-warning system the most according to claim 1, it is characterized in that, described sensor network also includes the second sensor being arranged on runway holding fix border, the receptor of the second sensor and emitter include being attached separately to runway holding fix boundaries on either side, and receptor is parallel with runway centerline with the line of emitter；
If the light path of the second sensor and first sensor is successively blocked, object is described from runway out, has then triggered prompting message；If the light path of first sensor and the second sensor is successively blocked, illustrate that object enters runway, if not obtaining control license, then triggered acousto-optic warning unit and produce warning information.
Airfield runway safety pre-warning system the most according to claim 1, it is characterized in that, described sensor network also includes the 3rd sensor being arranged on the runway boundary at distance runway head L1 rice, the receptor of the 3rd sensor and emitter are attached separately on border, runway both sides, and receptor is vertical with runway centerline with the line of emitter；For monitoring the aircraft takeoff state on this runway, if the light path of the 3rd sensor is blocked, triggers sliding race of aircraft takeoff and remind；The span of described L1 is 100--300；
Described sensor network also includes being arranged on runway with front end, junction, road junction (according to direction of advance when aircraft takeoff or landing, after airborne vehicle through position be front end) runway boundary on the 4th sensor, the receptor of the 4th sensor and emitter include being attached separately on border, runway both sides, and receptor is vertical with runway centerline with the line of emitter；Land state for monitoring the airborne vehicle on this runway, if the light path of the 4th sensor is blocked, illustrates that this road junction broken through by airborne vehicle, do not depart from from this road junction, trigger airborne vehicle and do not depart from from this road junction and remind；
Described sensor network also includes two groups of the 5th adjacent sensors and the 6th sensor being arranged on other road junction connected with runway in addition to road junction, runway holding fix place, and the emitter in the 5th sensor and the 6th sensor is all parallel with runway centerline with the line of receptor；In 5th sensor and the 6th sensor, the sensor nearer with runway centerline is the 5th sensor, the 5th sensor distance runway centerline L rice；If the light path of the 5th sensor and the 6th sensor is successively blocked, trigger the prompting message that airborne vehicle departs from from this road junction；The light path of the 6th sensor and the 5th sensor is successively blocked, and triggers warning information.
Airfield runway safety pre-warning system the most according to claim 3, it is characterized in that, described sensor network also includes being arranged on 4 unidirectional emission probes of the assuming diamond in shape arrangement outside runway head, lands airborne vehicle for monitoring dynamic, triggers airborne vehicle and lands prompting.
Airfield runway safety pre-warning system the most according to claim 4, it is characterised in that described sensor network also includes the 7th sensor being arranged on the border, runway anti-intrusion protection zone at distance runway 300 meters of boundary in front；The emitter of the 7th sensor is vertical with runway centerline with receptor line, and the distance of emitter and receptor is 2L rice；
Described sensor network also includes the 8th sensor being arranged on the border, runway anti-intrusion protection zone in landing airdrome length direction；8th sensor is made up of the sensor of multiple segmentations；The detection path of the sensor of multiple segmentations is continuous, and the line in detection path is parallel with runway centerline, and the wire length in detection path is that landing airdrome length adds 600 meters；
Described sensor network also includes borderline 9th sensor in part both sides and the tenth sensor being separately positioned between runway holding fix and actual runway；The emitter of the 9th sensor and the tenth sensor is all vertical with runway centerline with the line of receptor, emitter and receptor one of both are arranged on runway holding fix, and the distance between emitter and receptor subtracts L rice equal to the distance of runway holding fix to runway centerline；
Described sensor network also includes the 11st sensor of the portion outboard being arranged between runway holding fix and actual runway; parallel with the extension line of runway centerline with the line of receptor and distance runway centerline the distance of the emitter of the 11st sensor is L rice; distance between emitter and receptor is 300 meters, and emitter and receptor are arranged on border, runway anti-intrusion protection zone；
Being provided with the 12nd sensor between road junction adjacent on border, runway anti-intrusion protection zone, the emitter of the 12nd sensor is parallel with runway centerline with the line of receptor；
If the light path of one of above-mentioned 7th sensor, the 8th sensor, the 9th sensor, the tenth sensor, the 11st sensor and the 12nd sensor is blocked, trigger warning information.
6. according to the airfield runway safety pre-warning system according to any one of Claims 1 to 5, it is characterised in that also include control tower operation management system TOMS；Data processing server communicates to connect with control tower operation management system TOMS through switch and fire wall；Air station flight flight is dynamically sent to data processing server by control tower operation management system TOMS.
Airfield runway safety pre-warning system the most according to claim 6, it is characterised in that also include blank pipe many radars automated system；Data processing server communicates to connect with blank pipe many radars automated system；Blank pipe many radars automated system obtains airport in real time and lands the elevation information of flight, and sends data processing server to.
Airfield runway safety pre-warning system the most according to claim 6, it is characterised in that described sensor uses ABH tetra-light beam infrared opposite-type detector.
Airfield runway safety pre-warning system the most according to claim 6, it is characterised in that described sensor uses laser correlative detector.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620154677.5U CN205451355U (en) | 2016-03-01 | 2016-03-01 | Airport runway safety precaution system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620154677.5U CN205451355U (en) | 2016-03-01 | 2016-03-01 | Airport runway safety precaution system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205451355U true CN205451355U (en) | 2016-08-10 |
Family
ID=56605713
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620154677.5U Expired - Fee Related CN205451355U (en) | 2016-03-01 | 2016-03-01 | Airport runway safety precaution system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205451355U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105575021A (en) * | 2016-03-01 | 2016-05-11 | 杨兴文 | Airport runway safety early warning system and airport runway safety early warning method |
| CN106952506A (en) * | 2017-05-03 | 2017-07-14 | 中国民航大学 | A kind of low coverage parallel runways risk of collision and personal distance computing system and method |
| CN108918423A (en) * | 2018-06-25 | 2018-11-30 | 江苏双良低碳产业技术研究院有限公司 | A kind of safety system for the detection of open laser gas |
| CN109118829A (en) * | 2018-09-10 | 2019-01-01 | 北京航空航天大学东营研究院 | A kind of airport personnel dynamic monitoring and controlling method and system |
| CN114913716A (en) * | 2022-05-12 | 2022-08-16 | 智航信息服务(深圳)有限公司 | Flight scheduling integrated management method and system |
-
2016
- 2016-03-01 CN CN201620154677.5U patent/CN205451355U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105575021A (en) * | 2016-03-01 | 2016-05-11 | 杨兴文 | Airport runway safety early warning system and airport runway safety early warning method |
| CN106952506A (en) * | 2017-05-03 | 2017-07-14 | 中国民航大学 | A kind of low coverage parallel runways risk of collision and personal distance computing system and method |
| CN108918423A (en) * | 2018-06-25 | 2018-11-30 | 江苏双良低碳产业技术研究院有限公司 | A kind of safety system for the detection of open laser gas |
| CN109118829A (en) * | 2018-09-10 | 2019-01-01 | 北京航空航天大学东营研究院 | A kind of airport personnel dynamic monitoring and controlling method and system |
| CN114913716A (en) * | 2022-05-12 | 2022-08-16 | 智航信息服务(深圳)有限公司 | Flight scheduling integrated management method and system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105575021B (en) | A kind of airfield runway safety pre-warning system and method | |
| CN205451355U (en) | Airport runway safety precaution system | |
| CN110491179B (en) | Airport scene monitoring system with dynamic virtual electronic fence | |
| RU2634502C2 (en) | Method and device for traffic control at aerodrome | |
| US7868812B2 (en) | Surveillance and warning system | |
| US6606035B2 (en) | System and method for airport runway monitoring | |
| WO2021190212A1 (en) | Multi-source sensing and detection system for airport surface operation element | |
| AU2009230765B2 (en) | System and method for detecting and preventing runway incursion, excursion and confusion | |
| US5724040A (en) | Aircraft wake vortex hazard warning apparatus | |
| CN103592948B (en) | Unmanned plane flight collision avoidance method | |
| CN111968409B (en) | Aircraft takeoff stopping identification method and system based on real-time ADS-B data | |
| CN102332214A (en) | Enhanced airport scene monitoring system | |
| CN103413466A (en) | Airborne visible ground guide and warning device and guide and warning method thereof | |
| CN104380363A (en) | Systems and methods for enhanced awareness of obstacle proximity during taxi operations | |
| CN103325193A (en) | Airfield runway incursion prevention system and method based on wireless sensor network | |
| CN102034368A (en) | System and method for enhanced awareness of clearance from conflict for surface traffic operations | |
| CN111445727A (en) | System and method for monitoring airport runway incursion | |
| AU2022220403A1 (en) | Systems and methods for monitoring activities in an aviation environment | |
| CN206271197U (en) | A kind of airport ground runs CAS | |
| Zhang et al. | Empirical study of airport geofencing for unmanned aircraft operation based on flight track distribution | |
| US20080158041A1 (en) | Airport Surface Detector and Control System | |
| CN104898121A (en) | Runway collision avoidance system based on ranging mode and method thereof | |
| KR101119887B1 (en) | Intelligent system for controlling aerial lamp | |
| KR101277285B1 (en) | System and method for data fusion | |
| CN113129620A (en) | Vehicle signal lamp system at intersection of aircraft taxiway and service lane based on radar |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160810 Termination date: 20180301 |