CN110364032A - Aircraft enters protection zone method and system, management aircraft methods and system - Google Patents
Aircraft enters protection zone method and system, management aircraft methods and system Download PDFInfo
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- CN110364032A CN110364032A CN201910655913.XA CN201910655913A CN110364032A CN 110364032 A CN110364032 A CN 110364032A CN 201910655913 A CN201910655913 A CN 201910655913A CN 110364032 A CN110364032 A CN 110364032A
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- aircraft
- protection zone
- request
- module
- entry condition
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0047—Navigation or guidance aids for a single aircraft
- G08G5/006—Navigation or guidance aids for a single aircraft in accordance with predefined flight zones, e.g. to avoid prohibited zones
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/04—Anti-collision systems
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- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Computer Networks & Wireless Communication (AREA)
- Traffic Control Systems (AREA)
Abstract
Whether the invention discloses a kind of aircraft to enter protection zone method, comprising: judge aircraft within the scope of regulatory area using global position system；When the aircraft is within the scope of the regulatory area and needs to enter protection zone, Xiang Tatai is transmitted into request；When getting access order, the aircraft is controlled into the protection zone.The present invention enters the program of protection zone by optimizing aircraft; to judge whether in regulatory area range more accurate quick by using global position system; and traditional work being accomplished manually can be made by automatically completing; reducing leads to protection zone intrusion event odds due to making mistakes in chaos, and improves the safety of aircraft Runway operation.
Description
Technical field
The present invention relates to air traffic control fields more particularly to a kind of aircraft to enter protection zone method and system, pipe
Manage aircraft methods and system.
Background technique
Currently, runway invasion is to cause one of principal element of civil aviation accident, counted according in terms of civil aviaton, the U.S., from 2004 years
By 2006, there is 30% to be caused in aircraft safety accident by runway invasion, and from 2013 to 2016 year, runway intrusion event occurs
Quantity with every year about 10% speed rise.In China, runway intrusion event occurs for Hongqiao in Shanghai on October 11 within 2016, only
2 years are spent, on November 13rd, 2018, runway intrusion event occurred again for Pudong International Airport.
According to existing airdrome control mode, aircraft enters runway protection zone to be responsible for by tower controller, i.e. control tower pipe
Member processed listens to and monitors the request that aircraft enters runway, and range estimation judges the occupancy situation of runway protection zone, comprehensive runway protection
Area's occupancy situation and situation schedule aircraft is accepted into request sequentially enter and clear the runway protection zone, to guarantee aircraft
Orderly function.
Under current tower control mode, with the increase of airport popularization and aerodrome traffic amount, aircraft, vehicle and personnel
Request into runway largely concurrently generates regularly, so that controller is in always under the working condition of high load capacity, in addition
Often the adverse weather that occurs, bird hit the factors such as event and air traffic control, and controller makes mistakes in chaos unavoidable, Hongqiao in Shanghai's machine
" 10.11 " runway intrusion event of field is forgotten aircraft dynamic by controller and is caused.
Summary of the invention
(1) goal of the invention
Enter protection zone method and system, management aircraft methods the object of the present invention is to provide a kind of aircraft and is
System, to prevent the generation of runway intrusion event.
(2) technical solution
To solve the above problems, the first aspect of the present invention, which provides a kind of aircraft, enters protection zone method, comprising: benefit
Judge aircraft whether within the scope of regulatory area with global position system；When the aircraft within the scope of the regulatory area and needs
When entering protection zone, Xiang Tatai is transmitted into request；When getting access order, the aircraft is controlled into the guarantor
Protect area.
Further, further includes: when get wait instruction when, control the aircraft and go around and spiral access is waited to refer to
It enables.
Further, further includes: when the aircraft is not within the scope of the regulatory area or do not need to enter protection zone,
The aircraft is controlled to continue to fly.
Further, further includes: after the aircraft leaves the protection zone, report is sailed out of in the transmission of Xiang Suoshu control tower.
According to another aspect of the present invention, a kind of control tower management aircraft is provided and enters protection zone method, comprising: is obtained
What aircraft was sent, which enter, requests and is stored in into request queue end, and described into request is judged using global position system
Aircraft is within the scope of regulatory area, and the aircraft needs to send when entering protection zone；Judge whether the aircraft accords with
Close protection zone entry condition；When the aircraft meets the protection zone entry condition, Xiang Suoshu aircraft sends access and refers to
It enables.
It is further, described that judge whether the aircraft meets protection zone entry condition step include: to check the guarantor
Whether shield area's occupied state and the protection zone are in locking states；Check flight device enters whether request is located at request queue head
Position.
Further, further includes: when the aircraft does not meet the protection zone entry condition, not to the aircraft
Send instruction.
Further, further includes: when the aircraft meets the protection zone entry condition, sent out to the aircraft
The protection zone is set to locking states before sending access to instruct.
Further, the protection zone entry condition includes: protection zone locking situation and the priority for entering request.
Further, the priority includes: low priority and high priority；The low priority is activly request entrance
What the aircraft of the protection zone issued enters request；The high priority is the aircraft for communication failure occur or needing to force-land
Sending enters request.
According to another aspect of the invention, a kind of aircraft is provided and enters protection sound zone system, comprising: locating module is used for
Judge aircraft whether within the scope of regulatory area using global position system；Information sending module, for existing when the aircraft
Within the scope of the regulatory area and when needing to enter protection zone, Xiang Tatai is transmitted into request；Control module gets standard for working as
When entering order, the aircraft is controlled into the protection zone.
Further, the control module be also used to when get wait instruction when, control the aircraft and go around and disk
Rotation waits access instruction.
Further, the control module be also used to when the aircraft not within the scope of the regulatory area or do not need into
When entering protection zone, controls the aircraft and continue to fly.
Further, the information sending module is also used to after the aircraft leaves the protection zone, Xiang Suoshu tower
Report is sailed out of in platform transmission.
According to another aspect of the invention, a kind of control tower management aircraft is provided and enters protection sound zone system, comprising: information is adopted
Collect module, request and be stored in for obtaining entering for aircraft transmission into request queue end, described into request is to utilize
Global position system judges aircraft within the scope of regulatory area, and the aircraft needs to send when entering protection zone；Judgement
Module, for judging whether the aircraft meets protection zone entry condition；Information sending module, for being accorded with when the aircraft
When closing the protection zone entry condition, Xiang Suoshu aircraft sends access instruction.
Further, the judgment module includes: protection zone detection module, for checking that detecting the protection zone occupies shape
Whether state and the protection zone are in locking states；Whether list detection module enters to request to be located at for sense aircraft and ask
Ask queue the first.
Further, information sending module is also used to when the aircraft does not meet the protection zone entry condition, no
It sends and instructs to the aircraft.
Further, further includes: locking module, for when the aircraft meets the protection zone entry condition,
The protection zone is set to locking states before sending access instruction to the aircraft.
Further, the protection zone entry condition includes: protection zone locking situation and the priority for entering request.
Further, the priority includes: low priority and high priority；The low priority is activly request entrance
What the aircraft of the protection zone issued enters request；The high priority is the aircraft for communication failure occur or needing to force-land
Sending enters request.
(3) beneficial effect
Above-mentioned technical proposal of the invention has following beneficial technical effect:
The present invention enters the program of protection zone by optimizing aircraft, to judge whether by using global position system
In regulatory area range more accurate quick, and traditional work being accomplished manually can be made by automatically completing, reduced
Due to making mistakes in chaos lead to protection zone intrusion event odds, protection zone is prevented not to be connected to access when being in locking states
The aircraft of license enters protection zone, avoids collision accident in protection zone from occurring, improves the safety of aircraft Runway operation.
Detailed description of the invention
Fig. 1 is that the aircraft of first embodiment according to the present invention enters protection zone method flow diagram；
Fig. 2 is that the control tower management aircraft of the another aspect of first embodiment according to the present invention enters protection zone method stream
Cheng Tu；
Fig. 3 is the aircraft runway intrusion prevention method application schematic diagram of an optional embodiment according to the present invention；
Fig. 4 is that the aircraft of an optional embodiment according to the present invention enters the process flow diagram of runway protection zone；
Fig. 5 is the aircraft occupancy of runway protection zone and the locking shape at various locations of an optional embodiment according to the present invention
State schematic diagram；
Fig. 6 is the automation tower control system architecture schematic diagram of an optional embodiment according to the present invention.
Specific embodiment
In order to make the objectives, technical solutions and advantages of the present invention clearer, With reference to embodiment and join
According to attached drawing, the present invention is described in more detail.It should be understood that these descriptions are merely illustrative, and it is not intended to limit this hair
Bright range.In addition, in the following description, descriptions of well-known structures and technologies are omitted, to avoid this is unnecessarily obscured
The concept of invention.
Obviously, described embodiments are some of the embodiments of the present invention, instead of all the embodiments.Based on the present invention
In embodiment, every other implementation obtained by those of ordinary skill in the art without making creative efforts
Example, shall fall within the protection scope of the present invention.
As long as in addition, the non-structure each other of technical characteristic involved in invention described below different embodiments
It can be combined with each other at conflict.
As shown in Figure 1, wrapping in the embodiment of the present invention in a first aspect, providing a kind of aircraft enters protection zone method
It includes:
S1: judge aircraft whether within the scope of regulatory area using global position system；
S2: when aircraft is within the scope of regulatory area and needs to enter protection zone, Xiang Tatai is transmitted into request；It is optional
, further includes: when aircraft is not within the scope of regulatory area or do not need to enter protection zone, control aircraft continues to fly.
S3: when getting access order, control aircraft enters protection zone.
Optionally, further includes: when getting waiting instruction, control aircraft, which goes around and spirals, waits access to instruct.
Optionally, further includes: after aircraft leaves protection zone, sail out of report to control tower transmission.Wherein, it sails out of in report
Location information including aircraft.
The above method makes to judge whether to be in regulatory area range more accurate quick by using global position system, and
And traditional work being accomplished manually can be made by automatically completing, reduce causes protection zone to invade thing due to making mistakes in chaos
Part odds, the aircraft for preventing protection zone not to be connected to access license when being in locking states enter protection zone, avoid protecting
It protects collision accident in area to occur, improves the safety that aircraft enters protection zone Runway operation.
As shown in Fig. 2, in the other side of the embodiment of the present invention, a kind of control tower management aircraft is provided and enters protection zone
Method, comprising:
T1: what acquisition aircraft was sent enters request and is stored in into request queue end, and entrance request is to utilize to defend
Star positioning system judges aircraft within the scope of regulatory area, and aircraft needs to send when entering protection zone；
T2: judge whether aircraft meets protection zone entry condition；Optionally, which includes: to check the protection zone
Whether occupied state and the protection zone are in locking states；Check flight device enters whether request is located at request queue first place.
The title that can be aircraft that request queue is added in the step is also possible to the number of aircraft, can uniquely refer to this in a word
Aircraft.Optionally, protection zone entry condition includes: protection zone locking situation and the priority for entering request.Optionally,
Priority includes: low priority and high priority；Low priority is the entrance that activly request enters that the aircraft of protection zone issues
Request；High priority is the entrance request for communication failure or the aircraft for needing to force-land occur and issuing.
T3: when aircraft meets protection zone entry condition, access instruction is sent to aircraft.Optionally, further includes: when
When aircraft does not meet protection zone entry condition, does not send and instruct to aircraft.When i.e. aircraft does not receive access instruction, running
The inverted position turn of pipe protection area waits.
Optionally, further includes: when aircraft meets protection zone entry condition, before sending access instruction to aircraft
Protection zone is set to locking states.
At the another aspect of the embodiment of the present invention, a kind of aircraft is provided and enters protection sound zone system, comprising: locating module,
For judging aircraft whether within the scope of regulatory area using global position system；Information sending module, for existing when aircraft
Within the scope of regulatory area and when needing to enter protection zone, Xiang Tatai is transmitted into request；Control module gets access life for working as
When enabling, control aircraft enters protection zone.
Optionally, control module is also used to when instruction has not been obtained, and control aircraft, which goes around and spirals, waits access to refer to
It enables.
Optionally, control module is also used to control when aircraft not within the scope of regulatory area or when not needing to enter protection zone
Aircraft processed continues to fly.
Optionally, information sending module is also used to after aircraft leaves protection zone, sails out of report to control tower transmission.
At the another aspect of the embodiment of the present invention, a kind of control tower management aircraft is provided and enters protection sound zone system, comprising: letter
Acquisition module is ceased, requests and is stored in for obtaining entering for aircraft transmission into request queue end, be to utilize into request
Global position system judges aircraft within the scope of regulatory area, and aircraft needs to send when entering protection zone；Judgment module,
For judging whether aircraft meets protection zone entry condition；Information sending module, for entering when aircraft meets protection zone
When condition, access instruction is sent to aircraft.
Optionally, judgment module includes: protection zone detection module, for detecting the protection zone occupied state and the guarantor
Whether shield area is in locking states；List detection module, for request queue to be added in aircraft.
Optionally, information sending module is also used to when aircraft does not meet protection zone entry condition, is sent to aircraft
Wait instruction.
Optionally, further includes: locking module, for being sent out to aircraft when aircraft meets protection zone entry condition
Protection zone is set to locking states before sending access to instruct.
Optionally, protection zone entry condition includes: protection zone locking situation and the priority for entering request.
Optionally, priority includes: low priority and high priority；Low priority is that activly request enters flying for protection zone
What row device issued enters request；High priority is the entrance request for communication failure or the aircraft for needing to force-land occur and issuing.
In an alternative embodiment, a kind of aircraft runway intrusion prevention method is provided, specifically by taking aircraft as an example, by fixed
Position satellite automatically determines aircraft self-position, and protects to control tower reported position if you need to enter runway at approaching runway protection zone
Qu Zexiang control tower is protected to initiate to enter request；Control tower accepts the entrance request of aircraft, according to runway locking situation and enters request
Priority ranking sends access instruction to aircraft or waits instruction；Control tower first sets runway protection zone before issuing access instruction
For locking states, until aircraft clears the runway completely, protection zone can release locking, guarantee that runway protection zone is in locking states
When, at most there is an aircraft to enter runway.As shown in figure 3, control tower processing ground plane and when entering request of airborne aircraft
Workflow is slightly different, and control tower, which is sent to it outside runway, when ground plane is unsatisfactory for entry condition waits instruction, airflight
Control tower is sent to it waiting instruction of going around and spiral when device is unsatisfactory for entry condition.
As shown in figure 4, aircraft side process requirements aircraft is protected by satellite positioning real-time monitoring self-position in approaching runway
Active to control tower reported position and is transmitted into request for the first time when protecting area, and runway of being allowed for access after receiving control tower access admittance is protected
Protect area, periodically to control tower reported position when being run in runway protection zone, when clear the runway protection zone after last time to tower
Platform reported position and send sail out of report.
Control tower effluent journey is divided into three sub threads: intercepting thread, runway control thread, state of emergency force interrupt thread.
After system electrification initialization, current runway occupied state is identified first, and anti-locking system starts preceding runway occupied state
It is lower to send access license to aircraft.
Intercepting thread holding is communicated with aircraft, is managed the occupied state of runway protection zone and is safeguarded occupancy list, will
The aircraft ID deposit for issuing legal entrance request enters request queue.
Guarantee that the access request issued before system starting is finished by controller first after the starting of runway control thread, so
System, which is accepted into request queue, afterwards enters request, it is ensured that aircraft safety enters runway protection zone and in system monitoring downlink
Into with leave, as shown in figure 5, by taking aircraft landing as an example, the occupancy and locking states of aircraft runway protection zone at various locations.Just
The request that enters that all activly requests enter the aircraft of runway protection zone in normal situation is low priority, the entrance of high priority
Request is only used for the aircraft for needing to land in an emergency.
State of emergency artificial treatment interrupt thread is used to dispose the aircraft that lands in an emergency that needs under abnormality, such as
Aircraft communication equipment fault cannot receive message or aircraft occurs catastrophe failure and needs to force-land, at this point, controller has the right manually
Other threads are interrupted, the aircraft ID for needing to land in an emergency directly is entered into request queue with high priority deposit, runway is waited to protect
Runway is preferentially supplied to the aircraft for needing to land in an emergency after shield unlock.
This embodiment scheme be establish with " based on the self-locking intrusion prevention mechanism of satellite positioning and protection zone " core from
Dynamicization tower control system, the system include following equipment: core processing system, communication system, display system, input system,
And warning system, the framework of system are as shown in Figure 6.
Each system function and workflow are as follows:
(1) communication system is responsible for receiving forwarding into request, access license and position report.
(2) core processing subsystem, the sub thread comprising three operations simultaneously listen to sub thread and are responsible for receiving into request
It is reported with position, the correct aircraft ID for entering and requesting that issues is put into request queue tail portion with low priority；Go to management sub-line
Journey successively provides access license according to the priority and sequencing for entering request in queue；Force interrupt emergency processing sub-line
Journey is responsible for controller being stored in queue tail by interrupting the aircraft ID of input with high priority.Three threads run detailed
Process is referring to Fig. 3
(3) display system is responsible for showing the operating status of entire automation tower control system and the operation shape of aircraft
State.
(4) warning system is responsible for receiving core processing subsystem sending unexpected message and be alerted to tower controller.
(5) input system is responsible for the control command of tower controller being sent to core processing system.
Moving objects location is automatically performed by pre-set programs, runway occupies detection, entry criteria judgement, access queue row
A series of tasks, the tower controllers such as sequence, access license transmission only need to be confirmed in key link.The present invention is by a large amount of towers
The task of platform controller transfers to automated procedures to complete, and reduces runway intrusion event probability caused by human factor, improves
The efficiency of tower control work.
The present invention is directed to protect a kind of aircraft to enter protection zone method, comprising: utilize global position system judgement flight
Whether device is within the scope of regulatory area；When the aircraft is within the scope of the regulatory area and needs to enter protection zone, Xiang Tatai
It is transmitted into request；When getting access order, the aircraft is controlled into the protection zone.The present invention is flown by optimization
Row device enters the program of protection zone, to judge whether by using global position system more accurate fast in regulatory area range
Victory, and traditional work being accomplished manually can be made by automatically completing, reducing leads to protection zone due to making mistakes in chaos
Intrusion event odds improves the safety of aircraft Runway operation.
It should be understood that above-mentioned specific embodiment of the invention is used only for exemplary illustration or explains of the invention
Principle, but not to limit the present invention.Therefore, that is done without departing from the spirit and scope of the present invention is any
Modification, equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.In addition, appended claims purport of the present invention
Covering the whole variations fallen into attached claim scope and boundary or this range and the equivalent form on boundary and is repairing
Change example.
Claims (20)
1. a kind of aircraft enters protection zone method characterized by comprising
Judge aircraft whether within the scope of regulatory area using global position system；
When the aircraft is within the scope of the regulatory area and needs to enter protection zone, Xiang Tatai is transmitted into request；
When getting access order, the aircraft is controlled into the protection zone.
2. the method according to claim 1, wherein further include:
When get wait instruction when, control the aircraft and go around and spiral access is waited to instruct.
3. the method according to claim 1, wherein further include:
When the aircraft is not within the scope of the regulatory area or do not need to enter protection zone, controls the aircraft and continue to fly
Row.
4. the method according to claim 1, wherein further include:
After the aircraft leaves the protection zone, report is sailed out of in the transmission of Xiang Suoshu control tower.
5. a kind of control tower management aircraft enters protection zone method characterized by comprising
Entering of obtaining that aircraft sends is requested and is stored in into request queue end, and described into request is to utilize satellite positioning
System judges aircraft within the scope of regulatory area, and the aircraft needs to send when entering protection zone；
Judge whether the aircraft meets protection zone entry condition；
When the aircraft meets the protection zone entry condition, Xiang Suoshu aircraft sends access instruction.
6. according to the method described in claim 5, it is characterized in that, described judge whether the aircraft meets protection zone entrance
Condition step includes:
Check whether the protection zone occupied state and the protection zone are in locking states；
Check flight device enters whether request is located at request queue first place.
7. according to the method described in claim 5, it is characterized by further comprising:
When the aircraft does not meet the protection zone entry condition, does not send and instruct to the aircraft.
8. according to the method described in claim 5, it is characterized by further comprising:
It, will be described before sending access instruction to the aircraft when the aircraft meets the protection zone entry condition
Protection zone is set to locking states.
9. according to method described in claim 5-8, which is characterized in that the protection zone entry condition includes: protection zone locking
Situation and the priority for entering request.
10. according to the method described in claim 9, it is characterized in that, the priority includes: low priority and high priority；
The low priority is to request the entering for aircraft sending of activly request into the protection zone；
The high priority is the entrance request for communication failure or the aircraft for needing to force-land occur and issuing.
11. a kind of aircraft enters protection sound zone system characterized by comprising
Locating module, for judging aircraft whether within the scope of regulatory area using global position system；
Information sending module, for when the aircraft within the scope of the regulatory area and need enter protection zone when, Xiang Tatai
It is transmitted into request；
Control module, for when getting access order, controlling the aircraft into the protection zone.
12. system according to claim 11, which is characterized in that the control module, which is also used to work as, gets waiting instruction
When, it controls the aircraft and goes around and spiral access is waited to instruct.
13. system according to claim 11, which is characterized in that the control module is also used to not exist when the aircraft
Within the scope of the regulatory area or when not needing to enter protection zone, controls the aircraft and continue to fly.
14. system according to claim 11, which is characterized in that the information sending module is also used to when the aircraft
After leaving the protection zone, report is sailed out of in the transmission of Xiang Suoshu control tower.
15. a kind of control tower management aircraft enters protection sound zone system characterized by comprising
Information acquisition module is requested and is stored in into request queue end, the entrance for obtaining entering for aircraft transmission
Request be judge using global position system aircraft within the scope of regulatory area, and hair when the aircraft is needed into protection zone
It send；
Judgment module, for judging whether the aircraft meets protection zone entry condition；
Information sending module, for when the aircraft meets the protection zone entry condition, Xiang Suoshu aircraft to send quasi-
Enter instruction.
16. system according to claim 15, which is characterized in that the judgment module includes:
Protection zone detection module, for detecting whether the protection zone occupied state and the protection zone are in locking states；
List detection module enters whether request is located at request queue first place for sense aircraft.
17. system according to claim 15, which is characterized in that information sending module is also used to not be inconsistent when the aircraft
When closing the protection zone entry condition, does not send and instruct to the aircraft.
18. system according to claim 15, which is characterized in that further include:
Locking module, for sending access to the aircraft when the aircraft meets the protection zone entry condition
The protection zone is set to locking states before instruction.
19. system described in 5-18 according to claim 1, which is characterized in that the protection zone entry condition includes: protection zone lock
It closes situation and enters the priority of request.
20. system according to claim 19, which is characterized in that the priority includes: low priority and high priority；
The low priority is to request the entering for aircraft sending of activly request into the protection zone；
The high priority is the entrance request for communication failure or the aircraft for needing to force-land occur and issuing.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201910655913.XA CN110364032B (en) | 2019-07-19 | 2019-07-19 | Method and system for aircraft to enter protected area and method and system for managing aircraft |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201910655913.XA CN110364032B (en) | 2019-07-19 | 2019-07-19 | Method and system for aircraft to enter protected area and method and system for managing aircraft |
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| CN110364032B CN110364032B (en) | 2021-07-20 |
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| CN107092008A (en) * | 2017-04-26 | 2017-08-25 | 毕雪松 | Pinpoint system and method are carried out to traffic pattern Inner aircraft |
| CN109583627A (en) * | 2018-10-31 | 2019-04-05 | 北京航空航天大学 | Aircraft landing is lined up optimization method and device |
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