CN207367391U - Monitoring system for low-latitude flying - Google Patents
Monitoring system for low-latitude flying Download PDFInfo
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- CN207367391U CN207367391U CN201721010435.XU CN201721010435U CN207367391U CN 207367391 U CN207367391 U CN 207367391U CN 201721010435 U CN201721010435 U CN 201721010435U CN 207367391 U CN207367391 U CN 207367391U
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Abstract
The utility model discloses a kind of monitoring system for low-latitude flying, wherein, which includes：Multi-beam phased array radar detection subsystem, ADS B subsystems, remote data communication subsystem and comprehensive situation display subsystem, wherein, remote data communication subsystem is connected with multi-beam phased array radar detection subsystem and ADS B subsystems, data process subsystem is connected with remote data communication subsystem, and comprehensive situation display subsystem is connected with data process subsystem.The system can obtain the relevant information of low flyer in real time, and merged with ADS B flying qualities, formation is precisely controlled information, in a manner of active probe and passive data are combined, achieve the purpose that to monitor low altitude airspace in real time, supported for the open basic technology that provides in low latitude day, provide service for General Aviation navigation, provide safeguard safely for important goal low altitude airspace.
Description
Technical field
It the utility model is related to space communication technical field, more particularly to a kind of monitoring system for low-latitude flying.
Background technology
At present, unmanned plane not manned is flown as a kind of using what wireless remote control device and the control device of itself were controlled
Row device, is widely used in civil and military field.
But since unmanned plane has the characteristics that flexibility height, mobility strong, hiding are good, thus, to the pipe of unmanned plane
Reason, especially monitors and manages in low altitude airspace, be global challenge, the water that the low latitude of the unmanned plane that it is seriously restricted opens
The development of gentle General Aviation.
Therefore, in order to adapt to the rise of unmanned plane business, how effectively efficiently to monitor the unmanned plane of low altitude airspace into
To need.
Utility model content
The purpose of this utility model is intended to solve one of above-mentioned technical problem at least to a certain extent.
For this reason, a purpose of the utility model is to propose a kind of monitoring system for low-latitude flying, can obtain in real time
Low flyer relevant information, and merge with ADS-B flying qualities, formation is precisely controlled information, with active probe with
The mode that passive data are combined, achievees the purpose that to monitor low altitude airspace in real time, is supported for the open basic technology that provides in low latitude day,
Service is provided for General Aviation navigation, is provided safeguard safely for important goal low altitude airspace.
The monitoring system for low-latitude flying of the utility model, including：Multi-beam phased array radar detection subsystem,
ADS-B subsystems, remote data communication subsystem, data process subsystem and comprehensive situation display subsystem, wherein, it is described remote
Journey data communication subsystem is connected with the multi-beam phased array radar detection subsystem and the ADS-B subsystems, the number
It is connected according to processing subsystem with the remote data communication subsystem, the comprehensive situation display subsystem and the data processing
Subsystem is connected, wherein, the multi-beam phased array radar detection subsystem, in default low altitude airspace survey mission mesh
Mark, and the detection data of the airbound target is obtained, wherein, the detection data includes three coordinate informations of the airbound target
And flying speed；The ADS-B subsystems, in the default low altitude airspace, obtaining and being based on ADS-B airborne equipments, and/
Or, the ADS-B flying qualities of the airbound target of airborne integrated data communication gateway transmitting；The remote data communication subsystem
System, for obtaining and transmitting the detection data and the ADS-B flying qualities；The data process subsystem, for receiving
And the detection data and the ADS-B flying qualities are merged, to calculate the positional information of the airbound target；The synthesis
Battle state display subsystem, for the situation map of the low altitude airspace to be formed and shown according to the positional information.
The monitoring system for low-latitude flying of the utility model, can obtain the low-latitude flying in radar zone of control in real time
Target information, and be precisely controlled information with airborne ADS-B data fusions, formation, be combined with active probe and passive data
Mode, achievees the purpose that to monitor low altitude airspace in real time, supports for the open basic technology that provides in low latitude day, is carried for General Aviation navigation
For service, provide safeguard safely for important goal low altitude airspace.
In addition, the monitoring system for low-latitude flying of the utility model, also has technical characterstic additional as follows：
In one embodiment of the utility model, the positional information of the airbound target includes：The airbound target
At least one of coordinate information, range information, elevation information.
In one embodiment of the utility model, the comprehensive situation display subsystem, is additionally operable to obtaining less than institute
When stating the ADS-B flying qualities of airbound target, non-controllable airbound target warning is carried out.
In one embodiment of the utility model, the multi-beam phased array radar detection subsystem includes, antenna array
Row module, ripple control computer module, data processing module and driver module, wherein, the ripple control computer and the antenna
Array is connected, and the data processing module is connected with the antenna array module, wherein, the ripple control computer module, is used for
The aerial array launching beam is controlled to scan the default low altitude airspace, obtains the flight signal of the airbound target；Institute
Data processing module is stated, for being calculated according to the flight signal to obtain the detection data；The driver module, is used for
The flight signal is compensated.
In one embodiment of the utility model, the ADS-B subsystems are additionally operable to receive the data processing subsystem
The instruction that system is sent, to send data according to described instruction.
In one embodiment of the utility model, the remote data communication subsystem by cable data module, or
Person, wireless data module transmit the detection data and the ADS-B flying qualities.
In one embodiment of the utility model, the data process subsystem includes：Data processing core module and
GIS map laminating module, wherein, the Data processing core module is connected with the GIS map laminating module, wherein, it is described
Data processing core module, for being merged to the detection data and the ADS-B flying qualities and obtaining the flight
The positional information of target；The GIS map laminating module, for airbound target described in the Overlapping display in the GIS map
Positional information.
In one embodiment of the utility model, the Data processing core module, is additionally operable to confirm flight parameter letter
Breath.
In one embodiment of the utility model, the flight parameter information includes flight-path angle information, course line flex point is believed
Breath, collision alert information, pilot's input control information, wind speed information, wind direction information, aircraft ambient temperature information, aircraft are known
One or more in other information and classification information.
In one embodiment of the utility model, the Data processing core module, is additionally operable to the record-setting flight date, flies
One or more in row temporal information, flight position information.
The aspect and advantage that the utility model adds will be set forth in part in the description, partly by from following description
In become obvious, or recognized by the practice of the utility model.
Brief description of the drawings
The above-mentioned and/or additional aspect of the utility model and advantage from the following description of the accompanying drawings of embodiments will
Become obvious and be readily appreciated that, wherein：
Fig. 1 is the structure diagram according to the monitoring system for low-latitude flying of the utility model one embodiment；
Fig. 2 is the structure diagram according to the multi-beam phased array radar detection subsystem of the utility model one embodiment；
Fig. 3 is the structure diagram according to the data process subsystem of the utility model one embodiment；And
Fig. 4 is the structure diagram according to the monitoring system for low-latitude flying of one specific embodiment of the utility model.
Embodiment
The embodiment of the utility model is described below in detail, the example of the embodiment is shown in the drawings, wherein from beginning
Same or similar element is represented to same or similar label eventually or there is same or like element.Below by ginseng
The embodiment for examining attached drawing description is exemplary, and is only used for explaining the utility model, and it is not intended that to the utility model
Limitation.On the contrary, the embodiment of the utility model includes falling into owning in the range of the spirit and intension of attached claims
Change, modification and equivalent.
In the description of the utility model, it is to be understood that term " first ", " second " etc. are only used for description purpose,
And it is not intended that instruction or hint relative importance., it is necessary to illustrate, unless otherwise bright in the description of the utility model
True regulation and restriction, term " connected ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or removable
Connection is unloaded, or is integrally connected；Can mechanically connect or be electrically connected；It can be directly connected, can also be in
Between medium be indirectly connected.For the ordinary skill in the art, with concrete condition above-mentioned term can be understood in this practicality
Concrete meaning in new.In addition, in the description of the utility model, unless otherwise indicated, " multiple " be meant that two or
Two or more.
Below with reference to the accompanying drawings the monitoring system for low-latitude flying of the utility model embodiment is described.
Fig. 1 is the structure diagram of the monitoring system for low-latitude flying of the utility model one embodiment.Such as Fig. 1 institutes
Show, which includes：Multi-beam phased array radar detection subsystem 100, ADS-B subsystems 200,
Remote data communication subsystem 300, data process subsystem 400 and comprehensive situation display subsystem 500.
Wherein, with reference to Fig. 1, remote data communication subsystem 300 and multi-beam phased array radar detection subsystem 100 and
ADS-B subsystems 200 are connected, and data process subsystem 400 is connected with remote data communication subsystem 300, and comprehensive situation is shown
Subsystem 500 is connected with data process subsystem 400.
Specifically, multi-beam phased array radar detection subsystem 100, in default low altitude airspace survey mission mesh
Mark, and the detection data of airbound target is obtained, wherein, detection data includes three coordinate informations and flying speed of airbound target.
Wherein, default low altitude airspace can be the universe low altitude airspace in airport or empty corridor or radar power range
Deng and in multi-beam phased array radar detection subsystem 100, the performance of multiple-beam radar is related, and the performance of multiple-beam radar is got over
Good detection accuracy is higher, then the identification range of low altitude airspace is bigger, for example, when the detection of separate unit multi-beam phased-array radar
Precision is in the range of 45Km, it is possible to find RCS<The low target of 0.5 ㎡, can find RCS in the range of 10km<0.1 ㎡'s
Airbound target, thus, performance based on multiple-beam radar set low altitude airspace, ensure that recognition efficiency, and improve identification can
By property.
In one embodiment of the utility model, multi-beam phased array radar detection subsystem 100 is based on multi-beam phase
Control the operating mode of battle array radar, according to the matched angle of multi-beam phased-array radar and speed to default low altitude airspace into
360 ° of radar scanning detections of row.
Further, multi-beam phased array radar detection subsystem 100 works as spy in default low altitude airspace survey mission target
After measuring doubtful airbound target, the detection data of airbound target is obtained, wherein, three coordinates that detection data includes airbound target are believed
Cease (distance, angle, scheduling) and flying speed.
Certainly, in practical applications, when low altitude airspace is wider, in order to detection more comprehensively, a multi-beam is phased
It can include the multi-beam phased-array radar of multiple detections in battle array radar detection subsystem, so that the multi-beam of multiple detections is phased
Battle array radar can carry out multi-platform combined, formation low latitude day net.
It should be appreciated that in order to further improve the recognition performance of multi-beam phased array radar detection subsystem 100, also
It can effectively eliminate ambient noise and noise jamming using first code algorithm is superintended and directed, target information extracted, alternatively, using CXI power is put
Big technology, effectively reduces product general power, minimizes multi-beam phased-array radar, or using IC2Antenna processing technology, has
Effect reduces antenna size.
It should be noted that according to the difference of concrete application scene, multi-beam phased array radar detection subsystem 100 can be with
It is made of different modules to realize its function, as a kind of possible implementation, as shown in Fig. 2, the multi-beam phased array
Radar detection subsystem 100 includes antenna array module 110, ripple control computer module 120, data processing module 130 and excitation
Device module 140.
Wherein, it is connected with reference to Fig. 2, ripple control computer 120 with aerial array 110, data processing module 130 and aerial array
Module 110 is connected, wherein,
Ripple control computer module 120, for controlling aerial array launching beam to scan default low altitude airspace, obtains flight
The flight signal of target.
Data processing module 130, for being calculated according to flight signal to obtain detection data.
Driver module 140, for being compensated to flight signal.
In one embodiment of the utility model, if airbound target is the airbound target of known identities, and it is directed to and is somebody's turn to do
Airbound target has set prebriefed pattern, then can carry out airbound target based on the beam phased array radar detection subsystem 100
Pipe
Reason, i.e., in low altitude airspace monitors detection process, when according to detection data identification airbound target deviation predefined paths
When, send suggestion voice and navigation indicates, in order to as early as possible lead the airbound target into correct path.
ADS-B subsystems 200, in default low altitude airspace, acquisition to be based on ADS-B (Automatic Dependent
Surveillance-Broadcast, Automatic dependent surveillance broadcast) airborne equipment, and/or, airborne integrated data communication gateway
The ADS-B flying qualities of the airbound target of transmitting.
It should be appreciated that ADS-B subsystems from its functionally for belong to one kind of aerial surveillance systems, but slave device
Working method on for but closer to data communication system.ADS-B subsystems, which do not have itself, determines airbound target
The ability of position, the positioning to airbound target is completed by other equipment, and ADS-B subsystems are merely responsible for an airborne equipment and are adopted
The flying quality collected, such as the information such as azel are transmitted to related system, to realize the monitoring similar to radar interface
Function.
In one embodiment of the utility model, ADS-B subsystems 200, are additionally operable to receive airborne integrated data network pass
The ADS-B flying qualities of transmission, wherein, which can be the data gateway based on 3G/4G nets, can also
Be its in the ADS-B terminals in general data radio station, this is not restricted.
In one embodiment of the use of the new type, in order to adapt to speed of data processing etc., form good processing and follow
Ring, ADS-B subsystems 200 are additionally operable to receive the instruction that data process subsystem 400 is sent, to send data according to instruction,
Remote data communication subsystem 300, for obtaining and transmitting detection data and ADS-B flying qualities.
Specifically, remote data communication subsystem 300 is by cable data module, alternatively, wireless data module transmission is visited
Survey data and ADS-B flying qualities.Wherein, the form of expression of wireless data module can be wireless data radio station module, the mould
Block can be that the optional module of whole monitoring system uses.
Data process subsystem 400, for receiving simultaneously fusion detection data and ADS-B flying qualities, to calculate flight
The positional information of target.
Wherein, in coordinate information of the positional information of airbound target including airbound target, range information, elevation information extremely
Few one kind.
It is appreciated that in practical implementation, data process subsystem 400 is mainly used for what correlation radar was detected
Detection data and ADS-B data are merged, according to accurate three coordinate (angle, distance, height) of airbound target and flight speed
The information such as degree, and other flight parameters, including (collision alert information, pilot input information, boat to other possible additional informations
The information such as mark angle, course line flex point) and aircraft identification information and classification information.Furthermore it is possible to include course, air speed, wind
The additional informations such as speed, wind direction and aircraft ambient temperature, calculate the positional information of airbound target.
In one embodiment of the utility model, as shown in figure 3, the data process subsystem 400 includes data processing
Center module 410 and GIS map laminating module 420, wherein, Data processing core module 410, for detection data and ADS-
B flying qualities are merged and obtain the positional information of airbound target, GIS map laminating module 420, in GIS map
The positional information of Overlapping display airbound target.
Wherein, Data processing core module 410, is additionally operable to confirm flight parameter information, which includes boat
Mark angle information, course line flex point information, collision alert information, pilot's input control information, wind speed information, wind direction information, aircraft
One or more in ambient temperature information, aircraft identification information and classification information.
In one embodiment of the utility model, Data processing core module 410, is additionally operable to the record-setting flight date, flies
One or more in row temporal information, flight position information, in order to which related personnel carries out follow-up according to the information of record
The analysis of unsafe incidents, wherein, in order to further be easy to related personnel to analyze more comprehensive, data processing centre's mould
Block 410, is additionally operable to store the data of acquisition in the form of word, and is stored according to preset time, wherein, preset time can
To need to be configured according to concrete application, for example it can be 10 years.
In one embodiment of the utility model, it can also be realized based on data process subsystem 400 to relevant device
Remote management etc..
Comprehensive situation display subsystem 500, for the situation map of low altitude airspace to be formed and shown according to positional information.
Specifically, comprehensive situation display subsystem 500 is mainly used for showing the position of airbound target, distance, image information,
So that operating personnel commander, control and operation.
In one embodiment of the utility model, comprehensive situation shows subsystem 500, above-mentioned data investigation can be existed
In the GIS map of region, forming region low altitude airspace situation map.
Certainly, in practical applications, in order to further be easy to implement visual analyzing, above-mentioned each subsystem will can be based on
The correlation detection process of the acquisition of system shown, such as, in multi-beam phased array radar detection subsystem 100 to according to default speed
When degree carries out moving detection to predeterminable area, in display platform, for example detecting area is shown in comprehensive situation shows subsystem 500
Domain electronic map, the coordinate position of radar and the real time position of airbound target and speed, in the real time position of search coverage, display
Region etc. is detected.
It is emphasized that it should be appreciated that under application scenes, same flight may can not be got
The detection data and ADS-B flying qualities of target, think that airbound target is uncontrollable at this time, then show subsystem in comprehensive situation
Airbound target warning alert is provided in 500, to prompt to enter clueless airbound target in related personnel low latitude, helps to add
By force to the safety management of low altitude airspace.
Based on above example, it should be appreciated that multiple subsystems of the utility model, according to its application scenarios not
Together, its function can be realized with different modules, for more clearly description, be exemplified below：
As shown in figure 4, this is used in the monitoring system of low-latitude flying, multi-beam phased array radar detection subsystem 100 wraps
Antenna array module 110 is included, transmitting receiving array module 150, driver module 140, data processing module 130, ripple control calculate
Machine module 120, ADS-B subsystems 200 include ADS-B data reception antennas module 210 and ADS-B data reception modules 220, far
Journey data communication subsystem 300 includes remote data communication module 310 and data dual-mode antenna module 320, data processing subsystem
System 400 includes Data processing core module 410 and GIS map laminating module 420.
In the present embodiment, the transmitting receiving array module 150 in antenna array module 110 is according to default speed and angle
Degree implements target area 360 ° of radar scanning detections, after doubtful airbound target is detected, obtains corresponding airbound target three and sits
The data such as data (distance, angle, height) and movement velocity are marked, wherein, in scanning probe, driver module 140 is to detection
The signal arrived carries out signal compensation, and ripple control computer module 120 controls antenna array module 110 to send associated beam and visited
Survey, data processing module 130 is used to obtaining and handling the detection data detected.
Meanwhile ADS-B subsystems 200 are scanned and detected including ADS-B data reception antennas module 210 and first close data, with
After the ADS-B flying qualities of airbound target are detected, the ADS-B of airbound target is received via ADS-B data reception modules 220
Flying quality.
And then after remote data communication module 310 receives the communication data and ADS-B flying qualities of airbound target, warp
Being sent by data transmit-receive Anneta module 320 to data process subsystem 400, certain data transmit-receive Anneta module 320 can also receive
Data and instruction from data process subsystem 400, after Data processing core module 410 receives related data, will detect
Data and ADS-B data are merged, and calculate the accurate coordinate of airbound target, and directly perceived in GIS map laminating module 420
Show, comprehensive situation display subsystem 500 can also show the position of airbound target by means of the GIS map laminating module 420
Put, essential information and other additional informations such as distance, height, and form monitor area low altitude airspace situation map.
Thus, in the monitoring system for low-latitude flying of the utility model, realize and low altitude airspace is implemented to monitor, find
Airbound target, obtains three coordinate informations of airbound target in real time, and synchronously receive the integrated data gateway of the airbound target
ADS-B data, form the accurate target and flying quality of airbound target, and the synchronous comprehensive situation at the center of charge shows subsystem
Position, height and the aircraft parameter of upper display airbound target, form the low altitude airspace situation map of monitor area, are not obtaining at the same time
During two item datas, there is provided non-controllable airbound target warning, improves the surveillance coverage of low altitude airspace, ensure movement area low altitude airspace peace
Entirely, can low latitude opening and General Aviation operation offer technical support and service.
More specifically, it is possible to find and the information such as the distance of the monitored airbound target of display, angle, height, translational speed, connect
Receive ADS-B ADS-B positional informations (longitude, latitude, height and time) and other possible additional informations (collision alert information,
Pilot inputs information, flight-path angle, the information such as course line flex point) and airbound target identification information and classification information.In addition, also
It may include additional information, the above- mentioned informations such as course, air speed, wind speed, wind direction and aircraft ambient temperature and synchronously pass through teledata
Communication subsystem is transferred to data process subsystem, and then carries out data fusion, forms accurate target information, is shown in comprehensive state
Gesture shown in subsystem, for monitoring, commanding, operating personnel's analysis such as control, judging, wherein, the synchronous note of data process subsystem
Record and preserve above- mentioned information, easy to be analyzed problem and prevented.
In conclusion the monitoring system for low-latitude flying of the utility model, can obtain in radar zone of control in real time
Low flyer information, and information is precisely controlled with airborne ADS-B data fusions, formation, with active probe and passive number
According to the mode being combined, achieve the purpose that to monitor low altitude airspace in real time, supported for the open basic technology that provides in low latitude day, be general
Aerial navigation provides service, provides safeguard safely for important goal low altitude airspace.
It should be appreciated that each several part of the utility model can be realized with hardware, software, firmware or combinations thereof.
In the above embodiment, what multiple steps or method can be performed in memory and by suitable instruction execution system with storage
Software or firmware are realized.If, and in another embodiment, can be with known in this field for example, realized with hardware
Any one of following technology or their combination realize：With the logic gate for realizing logic function to data-signal
The discrete logic of circuit, the application-specific integrated circuit with suitable combinational logic gate circuit, programmable gate array (PGA),
Field programmable gate array (FPGA) etc..
In the description of this specification, reference term " one embodiment ", " some embodiments ", " example ", " specifically show
The description of example " or " some examples " etc. means specific features, structure, material or the spy for combining the embodiment or example description
Point is contained at least one embodiment or example of the utility model.In the present specification, to the schematic table of above-mentioned term
State and may not refer to the same embodiment or example.Moreover, particular features, structures, materials, or characteristics described can be
Combined in an appropriate manner in any one or more embodiments or example.
While there has been shown and described that the embodiment of the utility model, it will be understood by those skilled in the art that：
These embodiments can be carried out with a variety of changes, modification in the case where not departing from the principle and objective of the utility model, replaced
And modification, the scope of the utility model are limited by claim and its equivalent.
Claims (10)
- A kind of 1. monitoring system for low-latitude flying, it is characterised in that including：Multi-beam phased array radar detection subsystem, ADS-B subsystems, remote data communication subsystem, data process subsystem and comprehensive situation display subsystem, wherein, it is described remote Journey data communication subsystem is connected with the multi-beam phased array radar detection subsystem and the ADS-B subsystems, the number It is connected according to processing subsystem with the remote data communication subsystem, the comprehensive situation display subsystem and the data processing Subsystem is connected, wherein,The multi-beam phased array radar detection subsystem, in default low altitude airspace survey mission target, and described in obtaining The detection data of airbound target, wherein, the detection data includes three coordinate informations and flying speed of the airbound target；The ADS-B subsystems, in the default low altitude airspace, obtaining and being based on ADS-B airborne equipments, and/or, it is airborne The ADS-B flying qualities of the airbound target of integrated data communication gateway transmitting；The remote data communication subsystem, for obtaining and transmitting the detection data and the ADS-B flying qualities；The data process subsystem, for receiving and merging the detection data and the ADS-B flying qualities, to calculate The positional information of the airbound target；The comprehensive situation display subsystem, for the situation of the low altitude airspace to be formed and shown according to the positional information Figure.
- 2. the system as claimed in claim 1, it is characterised in that the positional information of the airbound target includes：At least one of the coordinate information of the airbound target, range information, elevation information.
- 3. the system as claimed in claim 1, it is characterised in thatThe comprehensive situation display subsystem, is additionally operable to, when obtaining the ADS-B flying qualities less than the airbound target, carry out Non-controllable airbound target warning.
- 4. the system as claimed in claim 1, it is characterised in that the multi-beam phased array radar detection subsystem includes, day Linear array module, ripple control computer module, data processing module and driver module, wherein, the ripple control computer with it is described Aerial array is connected, and the data processing module is connected with the antenna array module, wherein,The ripple control computer module, for controlling the aerial array launching beam to be obtained to scan the default low altitude airspace Take the flight signal of the airbound target；The data processing module, for being calculated according to the flight signal to obtain the detection data；The driver module, for being compensated to the flight signal.
- 5. the system as claimed in claim 1, it is characterised in that the ADS-B subsystems are additionally operable to receive the data processing The instruction that subsystem is sent, to send data according to described instruction.
- 6. the system as claimed in claim 1, it is characterised in thatThe remote data communication subsystem is by cable data module, alternatively, wireless data module transmits the detection data With the ADS-B flying qualities.
- 7. the system as claimed in claim 1, it is characterised in that the data process subsystem includes：Data processing centre's mould Block and GIS map laminating module, wherein, the Data processing core module is connected with the GIS map laminating module, wherein,The Data processing core module, for the detection data and the ADS-B flying qualities to be merged and obtained The positional information of the airbound target；The GIS map laminating module, the positional information for airbound target described in the Overlapping display in the GIS map.
- 8. system as claimed in claim 7, it is characterised in thatThe Data processing core module, is additionally operable to confirm flight parameter information.
- 9. system as claimed in claim 8, it is characterised in thatThe flight parameter information includes flight-path angle information, course line flex point information, collision alert information, pilot's input control letter One or more in breath, wind speed information, wind direction information, aircraft ambient temperature information, aircraft identification information and classification information.
- 10. system as claimed in claim 7, it is characterised in thatThe Data processing core module, the one kind being additionally operable in record-setting flight date, flight-time information, flight position information It is or a variety of.
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| CN201721010435.XU CN207367391U (en) | 2017-08-11 | 2017-08-11 | Monitoring system for low-latitude flying |
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| CN201721010435.XU CN207367391U (en) | 2017-08-11 | 2017-08-11 | Monitoring system for low-latitude flying |
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| CN109814105A (en) * | 2019-03-06 | 2019-05-28 | 安徽瞭望科技有限公司 | A kind of control system for aircraft obstruction lamps and its method based on Radar Technology |
| CN110660274A (en) * | 2019-09-30 | 2020-01-07 | 中国电子科技集团公司第二十八研究所 | Airport capacity demand balance prediction method |
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| CN111951613A (en) * | 2020-07-24 | 2020-11-17 | 北京航空航天大学 | Air-ground cooperative wide-area airspace security situation assessment method |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109814105A (en) * | 2019-03-06 | 2019-05-28 | 安徽瞭望科技有限公司 | A kind of control system for aircraft obstruction lamps and its method based on Radar Technology |
| CN110660274A (en) * | 2019-09-30 | 2020-01-07 | 中国电子科技集团公司第二十八研究所 | Airport capacity demand balance prediction method |
| CN110660274B (en) * | 2019-09-30 | 2020-09-25 | 中国电子科技集团公司第二十八研究所 | Airport capacity demand balance prediction method |
| CN111899376A (en) * | 2020-07-06 | 2020-11-06 | 上海桥枫航空科技有限公司 | Fire balloon flight monitoring system |
| CN111951613A (en) * | 2020-07-24 | 2020-11-17 | 北京航空航天大学 | Air-ground cooperative wide-area airspace security situation assessment method |
| CN114120712A (en) * | 2021-11-22 | 2022-03-01 | 四川九洲电器集团有限责任公司 | Aerospace ball-borne AIS early warning method and device |
| CN114120712B (en) * | 2021-11-22 | 2022-11-29 | 四川九洲电器集团有限责任公司 | Aerospace ball-borne AIS early warning method and device |
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