CN105489068B - A kind of control order error correction method - Google Patents
A kind of control order error correction method Download PDFInfo
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- CN105489068B CN105489068B CN201510932804.XA CN201510932804A CN105489068B CN 105489068 B CN105489068 B CN 105489068B CN 201510932804 A CN201510932804 A CN 201510932804A CN 105489068 B CN105489068 B CN 105489068B
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- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/04—Anti-collision systems
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Abstract
The present invention provides a kind of control order error correction system and control order error correction method, including data integrated processing module, synthetic display module, system-level real-time monitoring module, the system also includes real-time command error correction alarm module and history alarm comprehensive analysis module.The present invention is by receiving data and carrying out data integrated treatment, conflict modeling is carried out to the current aircraft for changing command altitude, conflict calculating is carried out again, identify whether current control order can cause the generation of control unsafe incidents, so as to play the function of conflict anticipation, the security of job of air traffic control is improved；Present invention alarm accuracy is high, false alarm rate is low, data are accurate, applied widely in real time；In addition, region of the present invention is portable high, customization is good, and flexibility is high, and each control zone can have been used for instructing daily control to run work according to actual conditions customization of individual character warning information, parameter etc., alerts accuracy and false alarm rate reaches advanced international level.
Description
Technical field
The present invention relates to a kind of air traffic control system, and in particular to a kind of control order error correction system and its control refer to
Make error correction method.
Background technology
Control order is the directional beacon that aircraft flies in the air, and effective control order ensure that passenger, crew
Life security, in recent years, due to control commander it is improper caused by aircraft accident occur repeatedly, only 2014 the whole nation just occur
More cause control orders assign unsafe incidents caused by mistake, therefore the validity of stringent monitoring control order is present
Air traffic control focus of attention.
In the research of control order monitoring, general medium-term and long-term collision alert, short term collision alert can not both at home and abroad
Effectively solve the problems, such as this.Studies in China mechanism put forth effort on the alarm of research mid-term conflict probe to solve control order punching in recent years
The generation of the problems such as prominent, but the theoretical level stage is only rested on, it can not be applied in actual control work, such as Zou Binbin《It is empty
Pipe automated system mid-term conflict probe is studied》Deng.
In Chinese patent literature, publication number CN102542848A, title are a kind of air target short-term conflict warning methods
(referring to this application specification specific embodiment part), discloses a kind of air target short-term conflict warning method, including：If
Determine that the current track points of two aerial target are located at sustained height layer, then determine whether flying for described two aerial targets
Line direction, the height layer are the different height layer divided in advance according to the height of aerial target flight domain；If judge institute
It is relative flight to state two aerial targets, then the current track points for choosing described two aerial targets judge as pending alarm
Current track points pair；If judging described two aerial targets for flight in the same direction, and it is more than in the speed of rear aerial target
The speed of preceding aerial target, then choose the current boat that the current track points of described two aerial targets judge as pending alarm
Mark point pair；The distance between the current track points of current track points centering judged according to the pending alarm decide whether into
Row collision alert.The prior art is not examined simply by the height and course progress collision alert that judge two targets
Consider the situation that two targets are lateral or intersect, conflict model is also relatively simple, so as to cause target acquisition precision low, false alarm rate is high
The shortcomings of, in addition, the prior art also can not carry out analysis playback to history alarm information, so that can not be right in practical applications
Effective guidance is played in control work.
Therefore, in order to solve the problems in the existing technology, study that a kind of detection accuracy is high, false alarm rate is low and can be real
Now conflict the control order error correction system and control order error correction method of anticipation, and domestic flight is had far-reaching significance safely.
The content of the invention
The technical problem to be solved by the present invention is to provide a kind of control order error correction system, it is therefore an objective to is referred to by receiving control
Order, carries out data integrated processing with merging the information such as radar, flight dynamic, gps clock, the current command altitude that changes is flown
Row device carries out conflict modeling, and conflict model is calculated again after the completion of modeling, identifies whether current control order can cause pipe
The generation of unsafe incidents processed, so as to play the function of conflict anticipation, and then corrects the false command of controlling officer, effectively in time
The operating pressure for alleviating controlling officer, reduce control conflict generation probability, auxiliary improve air traffic control work
The security of work.
The technical scheme is that：
In order to solve the above technical problem, the present invention provides a kind of control order error correction system, including it is data integrated
Processing module, synthetic display module, system-level real-time monitoring module, the system also includes real-time command error correction alarm module with
And history alarm comprehensive analysis module；
The data integrated processing module, for receiving, handling data and data are carried out storage transmission；
The real-time command error correction alarm module, conflicts for receiving the data that data integrated processing module is sent
Modeling and conflict calculate, and conflict of qualification simultaneously carries out Real-time Alarm for conflicting information；
The history alarm comprehensive analysis module, for record flight data and warning information, and by the history number of record
According to carrying out analysis playback；
The synthetic display module, carries out for showing the flying quality and warning information that receive, and to warning information
False alarm rejection；
The system-level real-time monitoring module, for each server of monitoring system and the operating status of application software, and
The operating status of each work seat and application software can be monitored.
Control order error correction system is comprehensive information integrated processing system, has merged the number of multiclass blank pipe production system
According to data class includes control order, fusion radar, flight dynamic, gps clock information etc., in data integrated processing also
The data check functions such as the positive normal manner identification of aircraft, height error correction, radar saltus step suppression are added, effectively raise model
Precision, reduces false alarm rate, and fusion radar includes the data such as height, speed, position and the course of aircraft, automation is managed
System instruction with merge radar, flight dynamic, gps clock information integral processing after, then by conflict model to forward, inversely,
Lateral and four kinds of models of intersection are modeled, and model and conflict rule are carried out matching primitives after the completion of modeling, and judge to manage
Whether system instruction can cause the generation of aircraft conflict, and wrong control order is then corrected in the event of conflict, so as to pacify to control
Effective guaranteeing role is played entirely；In addition, the conflict model of the system using space as research object, establishes space 3-dimensional conflict
Model, changes with aerial vehicle trajectory and constantly corrects conflict model, which covers all conflicts that can occur in flight course
Model, the detection based on the model can effectively improve detection accuracy, and false alarm rate is reduced to the acceptable model of controlling officer
Within enclosing, effective supervisory role can be played to control order in actual work.
The data integrated processing module draws to connect submodule and with data draw including data connects the number that submodule is connected
According to processing submodule, the data draw connect submodule draw the data that connect include fusion radar, control order, flight dynamic and
Gps clock information, fusion radar, control order and the flight multidate information pass through automated system used in control department
Draw connecing, the gps clock information, which is drawn, connects standard gps clock information, and the data processing submodule is used to carry out abnormal number
According to processing, Data Fusion and data broadcast transmission；Data integrated processing module be used for carry out data draw connect, abnormal data
Processing, Data Fusion and data broadcasting such as send at the function, and data, which are drawn, to be connect submodule and be used to draw to connect data, data processing
Module first carries out dissection process to drawing the data connect, provides basic data for Data Fusion after data parsing, then leads to again
Data Fusion is crossed to obtain fusion radar data, according to fusion radar in aircraft flying quality traversal flight dynamic and
Control order data, judge whether that traversal is completed by searching for data, the data after traversal then are carried out fusion treatment, then right
Fused data after fusion carries out data check, will finally verify the accurate data output completed；Fused data is aerial all
Aircraft data, fused data include fusion radar, control order and flight dynamic, fused data in system with broadcast
Form be transmitted, all terminal seats receive the fused data of broadcast in system；For fused data, data check meeting
Checking treatment is carried out to fused data, in checking procedure, for error numbers such as Height Anomalies, position hopping, mistake control orders
According to error checking and correction processing is carried out, for non-civil aviaton's aircraft, its answering machine coding is filtered in data integrated processing, prevents
Its calculating to civil aviaton's aircraft impacts；Control order is controller according to control space-time condition at that time, including process
Visually fly on single, flight dynamic telegram and related data, current meteorological data, adjacent and alternate airport data and radar screen
The information such as the state of flight of machine, after being processed combination with reference to oneself existing knowledge experience, the order that is sent to unit, control
Instruct the influence in Modeling Calculation to model maximum, therefore the appearance of abnormal control order can cause model accuracy huge shadow
Ring, the appearance of abnormal control order, sets up interference range, interference range is centered on certain coordinate points, with setpoint distance in order to prevent
For radius, cylinder or cone with altitude range, the control order data of aircraft are in failure state in interference range,
The aircraft that control order is carried in all interference ranges is operated according to no control order, which can not only be used as and visit
Target acquisition surrounding aircraft is surveyed, but detection calculating can be carried out as detected target；Setting up for interference range improves model
Precision, to improve result of calculation accuracy play an important roll.
The real-time command error correction alarm module includes conflict modeling submodule and instruction error correction submodule；
The conflict modeling submodule, for according to the data relationship between different target aircraft and detected aircraft
Information establishes conflict model；Conflict modeling is to be directed to data relationship between different target aircrafts and detected aircraft to establish
Forward, inversely, laterally and the conflict model that intersects, which includes the spacing of different target aircraft and detected aircraft
From, angle, speed difference, difference in height and history flight path etc., the model established is constantly promoted with target aircraft,
Exception Model identification is carried out by adding model errors analysis mechanisms, correct model is determined whether and it is constantly repaiied
Just；
Described instruction error correction submodule, is rushed for the conflict model combination control order and conflict rule according to foundation
It is prominent to calculate, and conflicting information is subjected to multicast and is sent so that controller carries out instruction error correction in time；Instruction error correction, which is directed to, have been modeled
Into relation aircraft, predict aircraft between flight trend, the track that calculating aircraft constantly promotes in flight course,
After promoting track to judge whether current control order can cause the generation of aircraft conflict, conflict to calculate, in the event of punching
It is prominent, conflicting information is subjected to multicast transmission, and carry out conflict to controlling officer in time and remind so as to carry out instruction error correction.
The conflicting information is including between flight number, conflict model type and target aircraft and detected aircraft
Distance, angle, speed difference, difference in height and history flight path, conflict model include forward, inversely, laterally and intersection four species
Type.
The history alarm comprehensive analysis module includes historical record submodule and analysis playback submodule；
The historical record submodule, flying quality and warning information before being alerted for record-setting flight device；Go through
Records of the Historian record disposably remembers flying quality of two aircraft in alarm first five cycle at moment for the aircraft alerted
Record in hard disk, and by the identification information recording of alarm in the database；In alarm moment start recording aircraft flying subsequently
Row data, untill conflict terminates；The field information of historical record includes flight path number, flight number, secondary code, current height
Degree, the latitude residing for aircraft, longitude, coordinate X, coordinate Y, direction, state of flight, command altitude, affiliated flight range and
The field informations such as renewal time；The secondary code is the unique sign that each aircraft distributes in the air；
The analysis playback submodule, for the data of historical record to be loaded into again and play back output, reduction punching again
The raw scene that happens suddenly and the reason for analyze conflict or false-alarm；
The colliding data of record is loaded into and plays back output by analysis playback again, the scene that reduction conflict occurs again,
The reason for the reason for conflict is analyzed on the basis of the scene or false-alarm, provide to instruct control to work or improving collisions parameter setting
Effective instrument and means；Conflict playback includes the functions such as conflict query, data loading, data playback, playback pause, analysis
Function is that the position data relation of each minute airline is analyzed, and obtains the reason for conflict occurs, is risen in real work
To directive function；For false-alarm, analytic function can summarize false-alarm Producing reason, by means such as adjustment parameters, reduce empty
The alert probability produced, makes software significantly more efficient and provides service for control trouble free service.
The synthetic display module includes warning information display sub-module and false alarm rejection submodule；
The warning information display sub-module, for receiving data integrated processing module and real-time command error correction alarm mould
The data message of block multicast transmission simultaneously carries out synthesis display；Warning information display sub-module will receive rushing for system broadcasts transmission
Prominent information carries out synthesis display, is shown alarm aircraft in the form of highlighted line on radar graphic interface, and will
Alarm details are shown in a manner of window pop-up, with sound alarm, prevent controlling officer's mistake from forgetting to leak, and ignore alarm letter
Breath；
The false alarm rejection submodule, the warning information for real-time command error correction alarm module to be sent are identified as false-alarm
And the interference of false-alarm is discharged by manual type；False alarm rejection will appear from warning information and be identified as false-alarm, arrange in a manual manner
Except the interference of false-alarm, the accuracy rate of flight is improved, reduces false alarm rate.
Present invention also offers a kind of method that control order error correction is carried out using control order error correction system, control order
Error correction system receiving control instructs, and carries out data integrated processing with merging radar, flight dynamic, gps clock information, for
Data after integrated treatment carry out conflict modeling to the current aircraft for changing command altitude and conflict calculates, and judge current
Whether control order can cause aircraft conflict, and then error correction is carried out to control order in time for conflicting information in the event of conflict
Alarm.
It the described method comprises the following steps：
Step 1, receive current control order, fusion thunder by the data integrated processing module of control order error correction system
Reach, fly dynamic and gps clock information, dealing of abnormal data and Data Fusion are carried out to the data of reception, and then will melt
Data after conjunction carry out data check processing, and will verify the accurate data output completed；In addition, data integrated treated
Interference range is additionally provided with journey, by judging whether aircraft in interference range prevents the appearance of abnormal control order；
Step 2, the real-time command error correction alarm module of control order error correction system receive data integrated processing module hair
The data sent, the data relationship between different target aircrafts and detected aircraft for the current control order of reception,
By conflict modeling establish forward, inversely, laterally and intersect conflict model, with target aircraft constantly propulsion, pass through
Model errors analysis mechanisms constantly correct conflict model；
Step 3, the relation aircraft completed for conflict modeling, predict the flight trend between aircraft, simulated flight
The track that device constantly promotes in flight course, carries out matching primitives by conflict model and conflict rule, judges that current control refers to
Whether order can cause the generation of aircraft conflict, in the event of conflicting, then be sent into by conflicting information multicast so as to be instructed
Error correction alerts, if do not clashed, conflict calculating finishes；
Step 4, the synthetic display module of control order error correction system receive what real-time command error correction alarm module was sent
Warning information, will alert aircraft in graphic software platform area and is shown in the form of highlighted line, and will alert details
Shown in a manner of window pop-up, alerted at the same time in the form of two kinds of figure and sound, prevent controlling officer's careless omission warning information；Control
The synthetic display module of instruction error correction system is additionally operable to receive control order, the fusion thunder that data integrated processing module is sent
Reach, fly dynamic and gps clock information, so that the data received are patterned display；Further, it is also possible to by comprehensive
Close the warning information that display module will appear from and be identified as false-alarm, so as to exclude the interference of false-alarm in a manual manner.
The method is further comprising the steps of：
After control order error correction alarm is completed, control order error correction system can also pass through history alarm comprehensive analysis mould
Block carries out data record to flying quality and warning information and analysis plays back, after the colliding data of historical record is loaded into again
The scene that conflict occurs can be reduced, is carried out at the same time playback output, and then analysis conflict or false-alarm produce on the basis of the scene
The reason for, and export analysis report.
The method is further comprising the steps of：
Control order error correction system passes through each server of system-level real-time monitoring module real-time monitoring system and application software
Operating status, the state quality of each server and application software is marked by color, represents that operating status is normal using green,
Represent that server or application software are abnormal using red；It can also monitor each work seat in real time by system-level real-time monitoring module
Position and the operating status of application software, the state quality of each work seat and application software are marked by color, using green table
Show that operating status is normal, represent that the seat or application software are abnormal using red；Control order error correction system supports two services
Device is run at the same time, each other Hot Spare, when host is abnormal, automatically switches to backup machine operation；On system monitoring seat
Also system-level real-time monitoring module manual switching active/standby server can be passed through.
Conflict modeling in the step 2 specifically includes following steps：
A1, identification are given the aircraft of control order, judge whether the instruction of target aircraft is completed, if instructed
Cheng Ze re-recognizes the aircraft for being given control order；If instruction does not complete, it is identified as target aircraft and goes to step
Rapid a2；
A2, judge whether target aircraft is in interference range, and the target aircraft is excluded if being in interference range；
Step a3 is gone to if being not located in interference range；By judging whether aircraft in interference range prevents abnormal control order
Appearance；
A3, the 3D search coverages for establishing target aircraft；
A4, detect whether there is detected aircraft in target aircraft search coverage, if there is detected flight
Device then establishes conflict model according to distance, angle, speed difference, difference in height and history flight path relation data；
A5, the conflict model to foundation carry out Exception Model identification by model errors analysis mechanisms, determine whether just
True model；
Conflict in the step 3, which calculates, specifically includes following steps：
B1, judge to be detected the conflict sector that aircraft is presently in conflict model；
Relative distance trend and angle trend between b2, prediction aircraft；
B3, matched according to the distance between aircraft, angle and length velocity relation with conflict rule, predicts target flight
Whether device can produce the trend for breaking through alarm parameter during following Level Change between detected aircraft, judge whether
Conflict can be produced, when judging to clash, then carries out control order error correction alarm；When not clashing, conflict has been calculated
Finish.
The data record specifically includes following steps：
C1, judge whether to conflict；Each real-time command error correction alarm module is completed after conflict calculates, can will be all
In conflict deposit conflict buffering area, if conflict buffering area has conflict, it can determine whether to there is currently conflict, you can conflict
Record；
In the presence of c2, conflict, the flying quality in first five cycle that conflicts is recorded, and the identification information of conflict is remembered
Record is in the database；
C3, judge whether information updating, and if being recorded in the presence of if, there is no the detection information renewal for carrying out a new round
Judgement, until information updating or conflict terminate；
The analysis playback specifically includes following steps：
D1, by the schema modification of control order error correction system be recovering and analysis pattern；
D2, whether there is according to time or conflict mark information inquiry conflict；
If d3, conflict exist, colliding data is loaded into, colliding data is subjected to playback multicast after loading；
D4, in playback window, receive playback of data, and by the position data relation of each minute airline of calculating with chart
Form be presented to analysis personnel and analyzed, occur or false-alarm Producing reason so as to obtain conflict, and export analysis report；
It in playing process, can also suspend data playback, make a concrete analysis of the conflict reason at a certain moment；
D5, be normal mode by the schema modification of control order error correction system after playing.
The present invention technique effect be：
The present invention provides a kind of control order error correction system and its control order error correction method, referred to by receiving control
Order, carries out data integrated processing with merging the information such as radar, flight dynamic, gps clock, the current command altitude that changes is flown
Row device carries out conflict modeling, and conflict model is calculated again after the completion of modeling, identifies whether current control order can cause pipe
The generation of unsafe incidents processed, so as to play the function of conflict anticipation, and then corrects the false command of controlling officer, effectively in time
The operating pressure for alleviating controlling officer, reduce control conflict generation probability, auxiliary improve air traffic control work
The security of work.Present invention alarm accuracy is high, can identify all warning information under different situations；False alarm rate is low, passes through
Manually and automatic two kinds of means shield false-alarm, exclusive PCR；Data are accurate in real time, and the system data is accurate, time delay is low, and mistake refers to
Order can be recognized by the system immediately, and enough make-up times are provided for controlling officer；It is applied widely, in normal condition, pipe
Excess load processed commander, thunderstorm are diversion etc. and can effectively play the role of security control, especially in unreasonable air route, large area thunderstorm
Etc. under rough sledding, more effective guarantee can be provided safely for control；In addition, region of the present invention is portable high, customization is good, spirit
Active high, each control zone can have been used for instructing daily control according to actual conditions customization of individual character warning information, parameter etc.
Work is run, accuracy is alerted and false alarm rate reaches advanced international level.
Brief description of the drawings
Fig. 1 is control order error correction system structure diagram of the present invention.
Fig. 2 is control order error correction method flow chart of the present invention.
Fig. 3 is the data integrated process chart of the present invention.
Embodiment
Illustrate the embodiment of the present invention below in conjunction with the accompanying drawings：
As shown in Figure 1-Figure 3, the present invention provides a kind of control order error correction system, including data integrated processing mould
Block, synthetic display module, system-level real-time monitoring module, the system also includes real-time command error correction alarm module and history
Alarm integration analysis module；
The data integrated processing module, for receiving, handling data and data are carried out storage transmission；The data
Integrated treatment module draws to connect submodule and with data draw including data connects the data processing submodule that submodule is connected, described
Data, which draw to connect submodule and draw the data that connect, includes fusion radar, control order, flight dynamic and gps clock information, described to melt
Close radar, control order and flight multidate information draw connecing by automated system used in control department, during the GPS
Clock information, which is drawn, connects standard gps clock information, and the data processing submodule is used to carry out dealing of abnormal data, Data Fusion
With data broadcast transmission；
The real-time command error correction alarm module, conflicts for receiving the data that data integrated processing module is sent
Modeling and conflict calculate, and conflict of qualification simultaneously carries out Real-time Alarm for conflicting information；Real-time command error correction alarm module includes
Conflict modeling submodule and instruction error correction submodule；Conflict modeling submodule, for according to different target aircraft and detected
Data relationship information between aircraft establishes conflict model；Error correction submodule is instructed, for the conflict model knot according to foundation
Close control order and conflict rule carries out conflict calculating, and conflicting information is subjected to multicast and is sent so that controller is referred in time
Make error correction；The conflicting information is including between flight number, conflict model type and target aircraft and detected aircraft
Distance, angle, speed difference, difference in height and history flight path, conflict model include forward, inversely, laterally and intersection four species
Type；
The history alarm comprehensive analysis module, for record flight data and warning information, and by the history number of record
According to carrying out analysis playback；History alarm comprehensive analysis module includes historical record submodule and analysis playback submodule；History is remembered
Record submodule, flying quality and warning information before being alerted for record-setting flight device；Analysis playback submodule, for inciting somebody to action
The data of historical record are loaded into and play back output again, and the scene that reduction conflict occurs again simultaneously analyzes the original of conflict or false-alarm
Cause；
The synthetic display module, carries out for showing the flying quality and warning information that receive, and to warning information
False alarm rejection；Synthetic display module includes warning information display sub-module and false alarm rejection submodule；Warning information shows submodule
Block, for receiving the data message of data integrated processing module and real-time command error correction alarm module multicast transmission and carrying out comprehensive
Close display；False alarm rejection submodule, the warning information for real-time command error correction alarm module to be sent are identified as false-alarm and lead to
Cross the interference of manual type discharge false-alarm；
The system-level real-time monitoring module, for each server of monitoring system and the operating status of application software, and
The operating status of each work seat and application software can be monitored.
Present invention also offers a kind of method that control order error correction is carried out using control order error correction system, control order
Error correction system receiving control instructs, and carries out data integrated processing with merging radar, flight dynamic, gps clock information, for
Data after integrated treatment carry out conflict modeling to the current aircraft for changing command altitude and conflict calculates, and judge current
Whether control order can cause aircraft conflict, and then error correction is carried out to control order in time for conflicting information in the event of conflict
Alarm.
It the described method comprises the following steps：
Step 1, receive current control order, fusion thunder by the data integrated processing module of control order error correction system
Reach, fly dynamic and gps clock information, dealing of abnormal data and Data Fusion are carried out to the data of reception, and then will melt
Data after conjunction carry out data check processing, and will verify the accurate data output completed；
Step 2, the real-time command error correction alarm module of control order error correction system receive data integrated processing module hair
The data sent, the data relationship between different target aircrafts and detected aircraft for the current control order of reception,
By conflict modeling establish forward, inversely, laterally and intersect conflict model, with target aircraft constantly propulsion, pass through
Model errors analysis mechanisms constantly correct conflict model；
The conflict modeling specifically includes following steps：
A1, identification are given the aircraft of control order, judge whether the instruction of target aircraft is completed, if instructed
Cheng Ze re-recognizes the aircraft for being given control order；If instruction does not complete, it is identified as target aircraft and goes to step
Rapid a2；
A2, judge whether target aircraft is in interference range, and the target aircraft is excluded if being in interference range；
Step a3 is gone to if being not located in interference range；By judging whether aircraft in interference range prevents abnormal control order
Appearance；
A3, the 3D search coverages for establishing target aircraft；
A4, detect whether there is detected aircraft in target aircraft search coverage, if there is detected flight
Device then establishes conflict model according to distance, angle, speed difference, difference in height and history flight path relation data；
A5, the conflict model to foundation carry out Exception Model identification by model errors analysis mechanisms, determine whether just
True model；
Step 3, the relation aircraft completed for conflict modeling, predict the flight trend between aircraft, simulated flight
The track that device constantly promotes in flight course, carries out matching primitives by conflict model and conflict rule, judges that current control refers to
Whether order can cause the generation of aircraft conflict, in the event of conflicting, then be sent into by conflicting information multicast so as to be instructed
Error correction alerts, if do not clashed, conflict calculating finishes；
The conflict calculating specifically includes following steps：
B1, judge to be detected the conflict sector that aircraft is presently in conflict model；
Relative distance trend and angle trend between b2, prediction aircraft；
B3, matched according to the distance between aircraft, angle and length velocity relation with conflict rule, predicts target flight
Whether device can produce the trend for breaking through alarm parameter during following Level Change between detected aircraft, judge whether
Conflict can be produced, when judging to clash, then carries out control order error correction alarm；When not clashing, conflict has been calculated
Finish.
Step 4, the synthetic display module of control order error correction system receive what real-time command error correction alarm module was sent
Warning information, will alert aircraft in graphic software platform area and is shown in the form of highlighted line, and will alert details
Shown in a manner of window pop-up, alerted at the same time in the form of two kinds of figure and sound, prevent controlling officer's careless omission warning information；Control
The synthetic display module of instruction error correction system is additionally operable to receive control order, the fusion thunder that data integrated processing module is sent
Reach, fly dynamic and gps clock information, so that the data received are patterned display；Further, it is also possible to by comprehensive
Close the warning information that display module will appear from and be identified as false-alarm, so as to exclude the interference of false-alarm in a manual manner；
Step 5, when complete control order error correction alarm after, control order error correction system can also be integrated by history alarm
Analysis module carries out data record to flying quality and warning information and analysis plays back, by the colliding data of historical record again
The scene that conflict occurs can be reduced after loading, is carried out at the same time playback output, and then the analysis conflict or empty on the basis of the scene
Alert Producing reason, and export analysis report；
The data record specifically includes following steps：
C1, judge whether to conflict；Each real-time command error correction alarm module is completed after conflict calculates, can will be all
In conflict deposit conflict buffering area, if conflict buffering area has conflict, it can determine whether to there is currently conflict, you can conflict
Record；
In the presence of c2, conflict, the flying quality in first five cycle that conflicts is recorded, and the identification information of conflict is remembered
Record is in the database；
C3, judge whether information updating, and if being recorded in the presence of if, there is no the detection information renewal for carrying out a new round
Judgement, until information updating or conflict terminate；
The analysis playback specifically includes following steps：
D1, by the schema modification of control order error correction system be recovering and analysis pattern；
D2, whether there is according to time or conflict mark information inquiry conflict；
If d3, conflict exist, colliding data is loaded into, colliding data is subjected to playback multicast after loading；
D4, in playback window, receive playback of data, and by the position data relation of each minute airline of calculating with chart
Form be presented to analysis personnel and analyzed, occur or false-alarm Producing reason so as to obtain conflict, and export analysis report；
It in playing process, can also suspend data playback, make a concrete analysis of the conflict reason at a certain moment；
D5, be normal mode by the schema modification of control order error correction system after playing；
Step 6, control order error correction system by each server of system-level real-time monitoring module real-time monitoring system and are answered
With the operating status of software, the state quality of each server and application software is marked by color, represents to run shape using green
State is normal, represents that server or application software are abnormal using red；It can also be monitored in real time by system-level real-time monitoring module
Each work seat and the operating status of application software, the state quality of each work seat and application software is marked by color, is adopted
Represent that operating status is normal with green, represent that the seat or application software are abnormal using red.
Claims (11)
1. a kind of control order error correction method, control order error correction is carried out using control order error correction system, it is characterised in that：Pipe
System instruction error correction system receiving control instruction, and carry out data integrated place with merging radar, flight dynamic, gps clock information
Reason, carries out conflict modeling to the current aircraft for changing command altitude for the data after integrated treatment and conflict calculates,
Judge whether current control order can cause aircraft conflict, in the event of conflict then for conflicting information in time to control order
Carry out error correction alarm；
It the described method comprises the following steps：
Step 1, received by the data integrated processing module of control order error correction system current control order, fusion radar,
The data of reception are carried out dealing of abnormal data and Data Fusion by flight dynamic and gps clock information, and then by after fusion
Data carry out data check processing, and will verify complete accurate data output；In addition, in data integrated processing procedure
Interference range is additionally provided with, by judging whether aircraft in interference range prevents the appearance of abnormal control order；
Step 2, the real-time command error correction alarm module of control order error correction system receive what data integrated processing module was sent
Data, for the data relationship between the different target aircrafts and detected aircraft for receiving current control order, pass through
Conflict modeling establish forward, inversely, laterally and intersect conflict model, with target aircraft constantly propulsion, pass through model
Error analysis facility constantly corrects conflict model；
Step 3, the relation aircraft completed for conflict modeling, predict the flight trend between aircraft, simulated flight device exists
The track constantly promoted in flight course, carries out matching primitives by conflict model and conflict rule, judges that current control order is
The no generation that can cause aircraft conflict, in the event of conflicting, then sends so as to carry out instruction error correction into by conflicting information multicast
Alarm, if do not clashed, conflict calculating finishes；
Step 4, the synthetic display module of control order error correction system receive the alarm that real-time command error correction alarm module is sent
Information, will alert aircraft in graphic software platform area and be shown in the form of highlighted line, and will alert details with window
Mouth pop-up mode is shown, is alerted at the same time in the form of two kinds of figure and sound, prevents controlling officer's careless omission warning information；Control order
The synthetic display module of error correction system is additionally operable to receive the control order of data integrated processing module transmission, fusion radar, flies
Mobile state and gps clock information, so that the data received are patterned display；Further, it is also possible to by comprehensive aobvious
Show that the warning information that module will appear from is identified as false-alarm, so as to exclude the interference of false-alarm in a manual manner.
2. control order error correction method as claimed in claim 1, it is characterised in that：The control order error correction system includes number
According to integrated treatment module, synthetic display module, system-level real-time monitoring module, the system also includes real-time command error correction announcement
Alert module and history alarm comprehensive analysis module；
The data integrated processing module, for receiving, handling data and data are carried out storage transmission；
The real-time command error correction alarm module, conflict modeling is carried out for receiving the data that data integrated processing module is sent
And conflict calculates, conflict of qualification simultaneously carries out Real-time Alarm for conflicting information；
The history alarm comprehensive analysis module, for record flight data and warning information, and by the historical data of record into
Row analysis playback；
The synthetic display module, false-alarm is carried out for showing the flying quality and warning information that receive, and to warning information
Suppress；
The system-level real-time monitoring module, for each server of monitoring system and the operating status of application software, and can
Monitor the operating status of each work seat and application software.
3. control order error correction method as claimed in claim 2, it is characterised in that：The data integrated processing module includes
Data, which draw to connect submodule and with data draw, connects the data processing submodule that submodule is connected, and the data, which draw to connect submodule and draw, to be connect
Data include fusion radar, control order, flight dynamic and gps clock information, it is described fusion radar, control order and fly
Mobile state information draw connecing by automated system used in control department, and the gps clock information is drawn when meeting standard GPS
Clock information, the data processing submodule are used to carry out dealing of abnormal data, Data Fusion and data broadcast transmission.
4. control order error correction method as claimed in claim 2, it is characterised in that：The real-time command error correction alarm module bag
Include conflict modeling submodule and instruction error correction submodule；
The conflict modeling submodule, for according to the data relationship information between different target aircraft and detected aircraft
Establish conflict model；
Described instruction error correction submodule, based on carrying out conflict according to the conflict model combination control order and conflict rule of foundation
Calculate, and conflicting information is subjected to multicast and is sent so that controller carries out instruction error correction in time.
5. control order error correction method as claimed in claim 4, it is characterised in that：The conflicting information includes flight number, punching
Prominent types of models and the distance between target aircraft and detected aircraft, angle, speed difference, difference in height and history flight
Track, conflict model include forward, inversely, laterally and intersection four types.
6. control order error correction method as claimed in claim 2, it is characterised in that：The history alarm comprehensive analysis module bag
Include historical record submodule and analysis playback submodule；
The historical record submodule, flying quality and warning information before being alerted for record-setting flight device；
The analysis playback submodule, for being loaded into the data of historical record again and playing back output, reduction conflict again is sent out
Raw scene and the reason for analyze conflict or false-alarm.
7. control order error correction method as claimed in claim 2, it is characterised in that：The synthetic display module, which includes alarm, to be believed
Cease display sub-module and false alarm rejection submodule；
The warning information display sub-module, for receiving data integrated processing module and real-time command error correction alarm module group
Broadcast the data message sent and carry out synthesis display；
The false alarm rejection submodule, the warning information for real-time command error correction alarm module to be sent are identified as false-alarm and lead to
Cross the interference of manual type discharge false-alarm.
8. control order error correction method as claimed in claim 1, it is characterised in that：The method is further comprising the steps of：
After control order error correction alarm is completed, control order error correction system can also pass through history alarm comprehensive analysis module pair
Flying quality and warning information carry out data record and analysis plays back, can be also after the colliding data of historical record is loaded into again
The scene that original conflict occurs, is carried out at the same time playback output, and then the original that analysis conflict or false-alarm produce on the basis of the scene
Cause, and export analysis report.
9. the control order error correction method as described in claim 1 or 8, it is characterised in that：The method is further comprising the steps of：
Control order error correction system passes through each server of system-level real-time monitoring module real-time monitoring system and the fortune of application software
Row state, the state quality of each server and application software is marked by color, is represented that operating status is normal using green, is used
Red represents that server or application software are abnormal；Can also be monitored in real time by system-level real-time monitoring module each work seat and
The operating status of application software, the state quality of each work seat and application software is marked by color, represents to transport using green
Row state is normal, represents that the seat or application software are abnormal using red.
10. control order error correction method as claimed in claim 1, it is characterised in that：Conflict modeling in the step 2 is specific
Comprise the following steps：
A1, identification are given the aircraft of control order, judge whether the instruction of target aircraft is completed, if instructing and completing
Re-recognize the aircraft for being given control order；If instruction does not complete, it is identified as target aircraft and goes to step a2；
A2, judge whether target aircraft is in interference range, and the target aircraft is excluded if being in interference range；If
It is not located in interference range and then goes to step a3；
A3, the 3D search coverages for establishing target aircraft；
A4, detect whether there is detected aircraft in target aircraft search coverage, if there is detected aircraft then
Conflict model is established according to distance, angle, speed difference, difference in height and history flight path relation data；
A5, the conflict model to foundation carry out Exception Model identification by model errors analysis mechanisms, determine whether correct mould
Type；
Conflict in the step 3, which calculates, specifically includes following steps：
B1, judge to be detected the conflict sector that aircraft is presently in conflict model；
Relative distance trend and angle trend between b2, prediction aircraft；
B3, matched according to the distance between aircraft, angle and length velocity relation with conflict rule, and prediction target aircraft exists
The trend for breaking through alarm parameter whether can be produced during following Level Change between detected aircraft, judges whether to produce
Raw conflict, when judging to clash, then carries out control order error correction alarm；When not clashing, conflict calculating finishes.
11. control order error correction method as claimed in claim 8, it is characterised in that：The data record specifically includes following
Step：
C1, judge whether to conflict；
In the presence of c2, conflict, the flying quality in first five cycle that conflicts is recorded, and the identification information recording of conflict is existed
In database；
C3, judge whether information updating, and if being recorded in the presence of if, there is no sentencing for the detection information renewal for carrying out a new round
It is disconnected, until information updating or conflict terminate；
The analysis playback specifically includes following steps：
D1, by the schema modification of control order error correction system be recovering and analysis pattern；
D2, whether there is according to time or conflict mark information inquiry conflict；
If d3, conflict exist, colliding data is loaded into, colliding data is subjected to playback multicast after loading；
D4, in playback window, receive playback of data, and by the position data relation of each minute airline of calculating with the shape of chart
Formula is presented to analysis personnel and is analyzed, so as to obtain conflict generation or false-alarm Producing reason, and exports analysis report；Play
During, it can also suspend data playback, make a concrete analysis of the conflict reason at a certain moment；
D5, be normal mode by the schema modification of control order error correction system after playing.
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