CN209103548U - The empty integrated traffic service system in road - Google Patents
The empty integrated traffic service system in road Download PDFInfo
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- CN209103548U CN209103548U CN201821678055.8U CN201821678055U CN209103548U CN 209103548 U CN209103548 U CN 209103548U CN 201821678055 U CN201821678055 U CN 201821678055U CN 209103548 U CN209103548 U CN 209103548U
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Abstract
The utility model proposes a kind of empty integrated traffic service systems in road, low-latitude flying corridor including highway and highway overhead, and Air Traffic Control Subsystem, wherein, the side of highway has service area, service area includes aircraft landing-strip, and aircraft landing-strip is used for parked aircraft；Air Traffic Control Subsystem, for carrying out traffic control to the aircraft to fly on low-latitude flying corridor, wherein, Air Traffic Control Subsystem includes flying quality acquisition equipment, data fusion gateway and remotely manages maneuvering platform, wherein, data acquisition equipment and the communication connection of data Convergence gateway, data fusion gateway and long-range management maneuvering platform communication connection.It relies on freeway net to establish the transport hub of normalization road sky service as a result, realizes resource consolidation and share, extend transport services new model.
Description
Technical field
The utility model relates to the empty integrated traffic service systems of transportation facilities technology more particularly to a kind of road.
Background technique
It will be pursued with the development of the times as every field with the progress of technology, the service mode of high-efficiency and low-cost
Target, wherein in field of traffic, land parking service and aerial shut down service can be combined, become main
Direction is pursued, realizes that the transport services of the empty one in road either still send out tourism and logistics the civil-military inosculation of military field
Exhibition all has important positive effect.
Utility model content
The utility model is intended to solve at least some of the technical problems in related technologies.
For this purpose, the purpose of this utility model is that a kind of empty integrated traffic service system in road is proposed, to realize resource consolidation
It is shared, extend transport services new model.
In order to achieve the above object, the empty integrated traffic service system in the road of the utility model embodiment, comprising: highway and institute
State low-latitude flying corridor and the Air Traffic Control Subsystem in highway overhead, wherein the side of the highway has
There is service area, the service area includes aircraft landing-strip, and the aircraft landing-strip is used for parked aircraft；The aerial friendship
Siphunculus subsystem, for carrying out traffic control to the aircraft to fly on the low-latitude flying corridor, wherein described aerial
Traffic control subsystem includes flying quality acquisition equipment, data fusion gateway and remotely manages maneuvering platform, wherein described to fly
Row data acquisition equipment is connected with the data fusion gateway communication, and the data fusion gateway and the long-range management commander are flat
Platform communication connection.
The empty integrated traffic service system in the road of the utility model embodiment, relies on freeway net to establish normalization road sky clothes
The transport hub of business realizes resource consolidation and shares, extends transport services new model, has broken the open bottleneck in low latitude, has been
Emergency management and rescue, unmanned plane logistics and fortune trip the business such as combine and provide support.
In addition, the empty integrated traffic service system in the road of the utility model embodiment, also has following additional technology two special
Sign:
In one embodiment of the utility model, the aircraft landing-strip includes: airplane parking area.
In one embodiment of the utility model, the aircraft landing-strip includes: takeoff runway section and race of landing
Road segment segment.
In one embodiment of the utility model, the flying quality acquisition equipment includes that multi-beam phased-array radar is visited
Measurement equipment and ADS-B detecting devices based on Beidou,
Wherein, the multi-beam phased array radar detection equipment, for the flight in default low altitude airspace explorer vehicle
Data, wherein the flying quality includes three coordinate informations and flying speed of the aircraft；The ADS- based on Beidou
B detecting devices is used in the default low altitude airspace, obtains the ADS-B airborne equipment based on Beidou, and/or, airborne synthesis
The ADS-B flying quality based on Beidou of the aircraft of data communication gateway transmitting.
In one embodiment of the utility model, the multi-beam phased array radar detection equipment, comprising: aerial array
Module, wave control computer module, data processing module and driver module, wherein the wave control computer and the antenna array
Column are connected, and the data processing module is connected with the antenna array module, wherein the wave control computer module, for controlling
The aerial array launching beam is made to scan the default low altitude airspace, obtains the flying quality of the aircraft；The number
According to processing module, for being calculated according to the flying quality to obtain the flight position of the aircraft；The driver module,
For exciting power needed for explorer vehicle.
In one embodiment of the utility model, the ADS-B detecting devices based on Beidou, comprising: Beidou navigation
Positioning chip, the flight position for the aircraft according to Beidou location Calculation.
In one embodiment of the utility model, the flying quality Convergence gateway includes input circuit, comparison circuit
And output circuit, wherein the input circuit is connected with the comparison circuit, the phase of the output circuit and the comparison circuit
Even, the output circuit includes first input end and the second input terminal, and the input circuit is adopted for receiving the flying quality
Collect the first coordinate voltage value and the second coordinate voltage value of equipment acquisition；The comparison circuit, for according to first coordinate
Voltage value and the second coordinate voltage value and preset voltage value export first control signal or second control signal；
The output circuit exports first coordinate voltage for the first input end to be connected according to the first control signal
Value exports the second coordinate voltage value alternatively, second input terminal is connected according to the second control signal.
In one embodiment of the utility model, the service area further includes aircraft service area, wherein the flight
Device service area is adjacent with the aircraft landing-strip.
In one embodiment of the utility model, when the service area is adjacent with river, the service area further include:
Ship stops harbour, wherein it is adjacent with the river that the ship stops harbour.
In one embodiment of the utility model, the aircraft includes: baby plane, heavy unmanned plane, flight vapour
One of vehicle, flight container are a variety of.
The additional aspect of the utility model and advantage will be set forth in part in the description, partially will be from following description
In become obvious, or recognized by the practice of the utility model.
Detailed description of the invention
The utility model is above-mentioned and/or additional aspect and advantage from the following description of the accompanying drawings of embodiments will
Become obvious and be readily appreciated that, in which:
Fig. 1-1 is the structural schematic diagram according to the empty integrated traffic service system in road of the utility model one embodiment；
Fig. 1-2 is shown according to the transport hub of the empty integrated traffic service system in road of one specific embodiment of the utility model
It is intended to；
Fig. 2-1 is the structural schematic diagram according to the aircraft landing-strip of the utility model one embodiment；
Fig. 2-2 is the structural schematic diagram according to the aircraft landing-strip of one specific embodiment of the utility model；
Fig. 3 is the structural schematic diagram according to the multi-beam phased array radar detection equipment of the utility model one embodiment；
Fig. 4 is the structural schematic diagram according to the flying quality Convergence gateway of the utility model one embodiment；
Fig. 5 is the structural schematic diagram according to the empty integrated traffic service system in road of the utility model another embodiment.
Specific embodiment
The embodiments of the present invention are described below in detail, examples of the embodiments are shown in the accompanying drawings, wherein from beginning
Same or similar element or element with the same or similar functions are indicated to same or similar label eventually.Below by ginseng
The embodiment for examining attached drawing description is exemplary, it is intended to for explaining the utility model, and should not be understood as to the utility model
Limitation.
Below with reference to the accompanying drawings the empty integrated traffic service system in road of the utility model embodiment is described.
Fig. 1-1 is according to the structural schematic diagram of the empty integrated traffic service system in road of the utility model one embodiment, figure
1-2 is the transport hub schematic diagram according to the empty integrated traffic service system in road of one specific embodiment of the utility model.Such as figure
Shown in 1-1 and Fig. 1-2, the empty integrated traffic service system 1000 in the road includes: the low latitude of highway 100 and highway overhead
Flight corridor 200 and Air Traffic Control Subsystem 300, wherein
The side of highway 100 has service area 400, and service area 400 includes aircraft landing-strip 410, and aircraft rises
410 are settled in an area for parked aircraft.
To which service area 400 is also flight in the service area other than having vehicle service function in the prior art
Special parking area is arranged in device, thus, aircraft can be taken off and be parked based on the aircraft landing-strip 410, be broken
Existing aircraft region of rising and falling is found difficult universal to yoke Air Service mode, will add in service area 400
For the function of aircraft service, will combine together to sky service with service over the ground, resource-sharing is road sky Integrated Service Mode
Provide support.
Wherein, above-mentioned aircraft may include one of baby plane, heavy unmanned plane, hovercar, flight container
It is or a variety of, wherein the difference of aircraft type, the hardware device that corresponding aircraft landing-strip 410 includes is different, and example is such as
Under:
The first example:
In this example, aircraft include heavy unmanned plane etc. can directly standing start equipment.
In this example, such as Fig. 2-1, aircraft landing-strip 410 includes airplane parking area 411, wherein the airplane parking area 411 can be with
It is identified including airplane parking area, in order to which Aerial vehicle position goes out its region, the area and shape of airplane parking area 411 are according to service area
400 and aircraft type setting, this is not restricted.Wherein, for the ease of airplane parking area 411 and service area other equipment
Isolation, airplane parking area 411 may include support rod, and airplane parking area 411 is supported the setting that is above the ground level by support rod.
Example two:
In this example, aircraft includes that baby plane etc. needs starting runway and slides the equipment for shutting down runway.
In this example, as shown in Fig. 2-2, aircraft landing-strip 410 includes takeoff runway section 412 and landing runway road
Section 413, wherein for the flight of assisting in flying device 410, can be set between takeoff runway section 412 and landing runway section 413
It is set to the buffering section to rise and fall.For example, it is upward to be provided with inclination angle as shown in Fig. 2-2, on connection takeoff runway section 412
Buffering section, in connection 413 Department formation of the landing runway section buffering section that has inclination angle downward.
Air Traffic Control Subsystem 300, for carrying out traffic control to the aircraft to fly on low-latitude flying corridor,
Wherein, Air Traffic Control Subsystem 300 includes that flying quality acquisition equipment 310, data fusion gateway 320 and long-range management refer to
Wave platform 330, wherein flying quality acquires equipment 310 and data Convergence gateway 320 communicates to connect, 320 He of data fusion gateway
Long-range management maneuvering platform 330 communicates to connect.
In one embodiment of the utility model, flying quality acquires equipment 310 and visits including multi-beam phased-array radar
Measurement equipment and ADS-B detecting devices based on Beidou, wherein multi-beam phased array radar detection equipment, in default low latitude
The flying quality of airspace explorer vehicle, wherein flying quality includes three coordinate informations and flying speed of aircraft, based on north
The ADS-B detecting devices of bucket is used in default low altitude airspace, obtains the ADS-B airborne equipment based on Beidou, and/or, it is airborne
The ADS-B flying quality based on Beidou of the aircraft of integrated data communication gateway transmitting.
In the present embodiment, as shown in figure 3, multi-beam phased array radar detection equipment, comprising: antenna array module, wave
Control computer module, data processing module and driver module, wherein wave control computer is connected with aerial array, data processing
Module is connected with antenna array module, wherein wave control computer module, it is default to scan for controlling aerial array launching beam
Low altitude airspace obtains the flying quality of aircraft；Data processing module, for being calculated according to flying quality to obtain aircraft
Flight position；Driver module, for exciting power needed for explorer vehicle.
Specifically, the transmitting receiving array module in antenna array module is according to preset speed and angle to target area
360 ° of radar scanning detections are implemented in domain, after detecting doubtful airbound target, corresponding three coordinate data of airbound target of acquisition (away from
From, angle, height) and data such as movement velocity, wherein in scanning probe, it is required that driver module is used to generate detection
Exciting power, wave control computer module control antenna array module issue associated beam and are detected, and data processing module is used for
It obtains and handles the detection data detected.
Meanwhile the ADS-B equipment 200 based on Beidou include the ADS-B data reception antenna module scans based on Beidou simultaneously
Related flying quality is detected, with after detecting the ADS-B flying quality based on Beidou of aircraft, via based on Beidou
The ADS-B flying quality based on Beidou of ADS-B data reception module reception aircraft.
In turn, after receiving the communication data of airbound target and the ADS-B flying quality based on Beidou, via data transmit-receive
Anneta module is sent to data fusion gateway 320, and certain data transmit-receive Anneta module also can receive and come from data fusion gateway 320
Data and instruction, after data fusion gateway 320 receives related flying quality, by detection data and based on the ADS-B of Beidou
Data are merged, and the accurate coordinate of aircraft is calculated.
In one embodiment of the utility model, the ADS-B detecting devices based on Beidou, comprising: Beidou navigation positioning
Chip, for the flight position according to Beidou location Calculation institute aircraft.
It should be understood that the ADS-B detecting devices based on Beidou from its functionally for belong to aerial surveillance systems
One kind, but from the working method of equipment for closer to data communication system.ADS-B detecting devices based on Beidou itself
The ability positioned to aircraft is not had, the positioning to aircraft is completed by other equipment, and based on Beidou
ADS-B detecting devices is merely responsible for the collected flying quality of airborne equipment institute, for example, the information such as azel are transmitted to phase
Relationship system, to realize the function for monitoring for being similar to radar interface.
It should be understood that flying quality Convergence gateway 320 is mainly used for receiving and fly in the embodiments of the present invention
The flying quality that row data acquisition equipment 310 acquires is merged, for example, the detection data and base that will detect to correlation radar
It is merged in the ADS-B data of Beidou, according to accurate three coordinate (angle, distance, height) and flying speed of airbound target
Etc. information and other flight parameters, including (collision alert information, pilot input information, track to other possible additional informations
Angle, the information such as course line inflection point) and aircraft identification information and classification information.Furthermore it is possible to include course, air speed, wind speed,
The additional informations such as wind direction and aircraft ambient temperature, calculate the location information of aircraft.
As a kind of possible implementation, as shown in figure 4, flying quality Convergence gateway 320 include input circuit 321,
Comparison circuit 322 and output circuit 323.
Wherein, input circuit 321 is connected with comparison circuit 322, and output circuit 323 is connected with comparison circuit 322, output
Circuit 323 includes first input end 3231 and the second input terminal 3232.Input circuit 321 is for receiving flying quality acquisition equipment
310 the first coordinate voltage value A acquired in real time, the first coordinate voltage value can be used to indicate that dipper system to low flyer
The representative voltage of the corresponding flight position of the flying quality of acquisition, input circuit 321 is for receiving flying quality acquisition equipment 310
The the second coordinate voltage value B acquired in real time, wherein the second coordinate voltage value B can indicate radar system 300 to low flyer
Representative the second coordinate voltage value of the corresponding flight position of the flying quality of the aircraft acquired in real time.Comparison circuit 322 is used for
According to the first coordinate voltage value A and the second coordinate voltage value B and preset voltage value, first control signal or second is exported
Signal is controlled, for example, first control signal and second control signal can be low and high level signal.Output circuit 323 is used for root
The first coordinate voltage value A is exported according to first control signal conducting first input end 3231, alternatively, being connected according to second control signal
Second input terminal 3232 exports the second coordinate voltage value B.Wherein, preset voltage value can be configured according to the actual situation.
Wherein, one embodiment according to the present utility model, the first coordinate voltage value A, comprising: the first longitude voltage value
X1, the first latitude voltage value y1, the first height voltage value z1, that is, the first coordinate voltage value A is represented by (x1, y1, z1)；The
Two coordinate voltage value B, comprising: the second longitude voltage value x2, the second latitude voltage value y2, the second height voltage value z2, that is, second
Coordinate voltage value B is represented by (x2, y2, z2).
The flying quality in a variety of sources that flying quality Convergence gateway 320 acquires flying quality acquisition equipment 310 as a result,
Carry out error correction, the higher one group of flying quality of output prograin.
Further, as shown in figure 5, above-mentioned long-range management maneuvering platform 330 may include and in GIS map laminating module
331, the coordinate of aircraft is intuitively shown, long-range management maneuvering platform 330 can also be by means of the GIS map superposition mould
Block 331 shows essential informations and other additional informations such as position, distance, the height of airbound target, and forms monitor area low latitude
Airspace situation map.
Wherein, remotely management maneuvering platform 330 is also based on flying quality and sends flight control instruction etc. to aircraft,
For example send aircraft decline instruction at once etc..
In order to further increase the service function of the empty integrated service mode in above-mentioned road, in an implementation of the utility model
Example in, with continued reference to Fig. 1-2, may also include aircraft service area 430 in the service area 400, the aircraft service area 430 and fly
Row device landing-strip 410 is adjacent, which is used to provide oil plant for aircraft, maintain a breakdown maintenance etc..
Certainly, the service mode of the empty one of sea route also may be implemented in the service area 400 of the utility model embodiment, for example,
As shown in figure 5, server 400 may also include ship and stop harbour 420, wherein ship stops when server 400 is adjacent with river
It is adjacent with river by harbour 420, for providing service relevant to harbour.
To sum up, the empty integrated traffic service system in the road of the utility model embodiment, relies on freeway net to establish normalization
The transport hub of road sky service realizes resource consolidation and shares, extends transport services new model, has broken the open bottle in low latitude
Neck the business such as combines and provides support for emergency management and rescue, unmanned plane logistics and fortune trip.
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 spy described in conjunction with this embodiment or example
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
It states and is necessarily directed to identical embodiment or example.Moreover, particular features, structures, materials, or characteristics described can be with
It can be combined in any suitable manner in any one or more of the embodiments or examples.In addition, without conflicting with each other, this field
Technical staff can by the feature of different embodiments or examples described in this specification and different embodiments or examples into
Row combination and combination.
In addition, term " first ", " second " are used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance
Or implicitly indicate the quantity of indicated technical characteristic.Define " first " as a result, the feature of " second " can be expressed or
Implicitly include at least one this feature.The meaning of " plurality " is at least two, such as two in the description of the present invention,
It is a, three etc., unless otherwise specifically defined.
Any process described otherwise above or method description are construed as in flow chart or herein, and expression includes
It is one or more for realizing custom logic function or process the step of executable instruction code module, segment or portion
Point, and the range of preferred embodiments of the present invention includes other realization, wherein can not be by shown or discussion
Sequence, including according to related function by it is basic simultaneously in the way of or in the opposite order, Lai Zhihang function, this should be by this
The embodiment person of ordinary skill in the field of utility model is understood.
Expression or logic and/or step described otherwise above herein in flow charts, for example, being considered use
In the order list for the executable instruction for realizing logic function, may be embodied in any computer-readable medium, for
Instruction execution system, device or equipment (such as computer based system, including the system of processor or other can be held from instruction
The instruction fetch of row system, device or equipment and the system executed instruction) it uses, or combine these instruction execution systems, device or set
It is standby and use.For the purpose of this specification, " computer-readable medium ", which can be, any may include, stores, communicates, propagates or pass
Defeated program is for instruction execution system, device or equipment or the dress used in conjunction with these instruction execution systems, device or equipment
It sets.The more specific example (non-exhaustive list) of computer-readable medium include the following: there is the electricity of one or more wirings
Interconnecting piece (electronic device), portable computer diskette box (magnetic device), random access memory (RAM), read-only memory
(ROM), erasable edit read-only storage (EPROM or flash memory), fiber device and portable optic disk is read-only deposits
Reservoir (CDROM).In addition, computer-readable medium can even is that the paper that can print described program on it or other are suitable
Medium, because can then be edited, be interpreted or when necessary with it for example by carrying out optical scanner to paper or other media
His suitable method is handled electronically to obtain described program, is then stored in computer storage.
It should be appreciated that each section of the utility model can be realized with hardware, software, firmware or their combination.?
In above embodiment, what multiple steps or method can be executed in memory and by suitable instruction execution system with storage
Software or firmware are realized.Such as, if realized with hardware in another embodiment, can be under well known in the art
Any one of column technology or their combination are realized: having a logic gates for realizing logic function to data-signal
Discrete logic, with suitable combinational logic gate circuit specific integrated circuit, programmable gate array (PGA), scene
Programmable gate array (FPGA) etc..
Those skilled in the art are understood that realize all or part of step that above-described embodiment method carries
It suddenly is that relevant hardware can be instructed to complete by program, the program can store in a kind of computer-readable storage medium
In matter, which when being executed, includes the steps that one or a combination set of embodiment of the method.
In addition, can integrate in a processing module in each functional unit in each embodiment of the utility model,
It can be each unit to physically exist alone, can also be integrated in two or more units in a module.It is above-mentioned integrated
Module both can take the form of hardware realization, can also be realized in the form of software function module.The integrated mould
If block is realized and when sold or used as an independent product in the form of software function module, it also can store and counted at one
In calculation machine read/write memory medium.
Storage medium mentioned above can be read-only memory, disk or CD etc..Although having been shown and retouching above
The embodiments of the present invention are stated, it is to be understood that above-described embodiment is exemplary, and should not be understood as practical new to this
The limitation of type, those skilled in the art can be changed above-described embodiment in the scope of the utility model, repair
Change, replacement and variant.
Claims (10)
1. a kind of empty integrated traffic service system in road, which is characterized in that low including highway and the highway overhead
Empty flight corridor and Air Traffic Control Subsystem, wherein
The side of the highway has service area, and the service area includes aircraft landing-strip, the aircraft landing-strip
For parked aircraft；
The Air Traffic Control Subsystem, for carrying out traffic pipe to the aircraft to fly on the low-latitude flying corridor
System, wherein
The Air Traffic Control Subsystem includes that flying quality acquisition equipment, data fusion gateway and long-range management commander are flat
Platform, wherein flying quality acquisition equipment is connected with the data fusion gateway communication, the data fusion gateway and described
Long-range management maneuvering platform communication connection.
2. the system as claimed in claim 1, which is characterized in that the aircraft landing-strip includes: airplane parking area.
3. the system as claimed in claim 1, which is characterized in that the aircraft landing-strip include: takeoff runway section and
Run road segment segment in land.
4. the system as claimed in claim 1, which is characterized in that
The flying quality acquisition equipment includes that multi-beam phased array radar detection equipment and the ADS-B detection based on Beidou are set
It is standby,
Wherein, the multi-beam phased array radar detection equipment, for the flying quality in default low altitude airspace explorer vehicle,
Wherein, the flying quality includes three coordinate informations and flying speed of the aircraft；
The ADS-B detecting devices based on Beidou, for obtaining the ADS-B based on Beidou in the default low altitude airspace
Airborne equipment, and/or, the ADS-B flying quality based on Beidou of the aircraft of airborne integrated data communication gateway transmitting.
5. system as claimed in claim 4, which is characterized in that the multi-beam phased array radar detection equipment, comprising: antenna
Array module, wave control computer module, data processing module and driver module, wherein the wave control computer and the day
Linear array is connected, and the data processing module is connected with the antenna array module, wherein
The wave control computer module is obtained for controlling the aerial array launching beam to scan the default low altitude airspace
Take the flying quality of the aircraft；
The data processing module, for being calculated according to the flying quality to obtain the flight position of the aircraft；
The driver module, for exciting power needed for explorer vehicle.
6. the system as claimed in claim 1, which is characterized in that the ADS-B detecting devices based on Beidou, comprising:
Beidou navigation positioning chip, the flight position for the aircraft according to Beidou location Calculation.
7. the system as claimed in claim 1, which is characterized in that the flying quality Convergence gateway includes input circuit, is compared
Circuit and output circuit, wherein the input circuit is connected with the comparison circuit, the output circuit and the comparison circuit
Be connected, the output circuit includes first input end and the second input terminal,
The input circuit, for receiving the first coordinate voltage value and the second coordinate electricity of the flying quality acquisition equipment acquisition
Pressure value；
The comparison circuit, for according to the first coordinate voltage value and the second coordinate voltage value and preset voltage
Value exports first control signal or second control signal；
The output circuit exports first coordinate for the first input end to be connected according to the first control signal
Voltage value exports the second coordinate voltage value alternatively, second input terminal is connected according to the second control signal.
8. the system as claimed in claim 1, which is characterized in that
The service area further includes aircraft service area, wherein the aircraft service area is adjacent with the aircraft landing-strip.
9. the system as claimed in claim 1, which is characterized in that when the service area is adjacent with river, the service area is also
It include: that ship stops harbour, wherein it is adjacent with the river that the ship stops harbour.
10. the system as claimed in claim 1, which is characterized in that the aircraft includes:
One of baby plane, heavy unmanned plane, hovercar, flight container are a variety of.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821678055.8U CN209103548U (en) | 2018-10-16 | 2018-10-16 | The empty integrated traffic service system in road |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821678055.8U CN209103548U (en) | 2018-10-16 | 2018-10-16 | The empty integrated traffic service system in road |
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| CN209103548U true CN209103548U (en) | 2019-07-12 |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110940983A (en) * | 2019-12-10 | 2020-03-31 | 湖南纳雷科技有限公司 | Multi-beam radar for ground-imitating flight control of unmanned aerial vehicle and data fusion method |
| CN112906842A (en) * | 2021-01-18 | 2021-06-04 | 清华大学 | Information processing method and guidance system based on dynamic traffic information code |
| US20210343155A1 (en) * | 2020-04-29 | 2021-11-04 | Rohde & Schwarz Gmbh & Co. Kg | Communication system and method of controlling air traffic of an airspace |
| US12027054B2 (en) * | 2020-04-29 | 2024-07-02 | Rohde & Schwarz Gmbh & Co. Kg | Communication system and method of controlling air traffic of an airspace |
-
2018
- 2018-10-16 CN CN201821678055.8U patent/CN209103548U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110940983A (en) * | 2019-12-10 | 2020-03-31 | 湖南纳雷科技有限公司 | Multi-beam radar for ground-imitating flight control of unmanned aerial vehicle and data fusion method |
| US20210343155A1 (en) * | 2020-04-29 | 2021-11-04 | Rohde & Schwarz Gmbh & Co. Kg | Communication system and method of controlling air traffic of an airspace |
| US12027054B2 (en) * | 2020-04-29 | 2024-07-02 | Rohde & Schwarz Gmbh & Co. Kg | Communication system and method of controlling air traffic of an airspace |
| CN112906842A (en) * | 2021-01-18 | 2021-06-04 | 清华大学 | Information processing method and guidance system based on dynamic traffic information code |
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