CN204832505U - Vehicular aviation management primary radar - Google Patents
Vehicular aviation management primary radar Download PDFInfo
- Publication number
- CN204832505U CN204832505U CN201520542140.1U CN201520542140U CN204832505U CN 204832505 U CN204832505 U CN 204832505U CN 201520542140 U CN201520542140 U CN 201520542140U CN 204832505 U CN204832505 U CN 204832505U
- Authority
- CN
- China
- Prior art keywords
- primary radar
- vehicular
- processing module
- radar
- antenna
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Radar Systems Or Details Thereof (AREA)
- Traffic Control Systems (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The utility model relates to a vehicular aviation management primary radar, including on -vehicle platform, on -vehicle platform is large -scale special truck platform, installs the primary radar electron shelter that leg, built -in primary radar electronic equipment were propped in the leveling on its truck frame respectively to and make up by the antenna that antenna, revolving stage and horizon sensor form, the cabin of the primary radar electron shelter body go up GPS position sensor that fixed mounting is used for gathering GPS location information with be used for with the communication interface module of external communication. The utility model discloses an all radar equipments have all been installed on the radar carries the car platform, after only needing to carry a car and transporting appointed jobsite, just can carry out auto leveling to the radar antenna level, carry out automation to north to the antenna bearing, can quick travel to appointed jobsite, be applicable to emergent calamity fully or other provisional application scenarios, be connected to the central monitored control system of air traffic control through its communication interface module, shoulder airport air traffic control's task rapidly.
Description
Technical field
The utility model relates to Radar Technology field, especially a kind of vehicular aviation management primary radar.
Background technology
Existing aviation management primary radar is generally fixed station design, and such radar is generally made up of antenna combination and electronic equipment subsystem; All radar equipments are all arranged in fixing buildings, and antenna combination is arranged on the top of buildings, for transceiving electromagnetic ripple; Electronic equipment subsystem is arranged on other positions of buildings, and these equipment, for detecting the original echo information received from radar antenna, carry out to original echo the point mark flight path information that check processing can obtain airbound target and show.Visible, fixed aviation management primary radar does not have removable feature.
Standby in emergent calamity, as earthquake causes airport to be destroyed, or some other interim applicable cases, when annual overhaul as fixed station radar necessity cannot normally be executed the task during safeguarding, need a kind of airport that can move to needs easily to bear the responsibility interim task on duty, the vehicular aviation management primary radar of other desired airport work after finishing the work, can be moved to again easily.
Utility model content
The purpose of this utility model is that providing a kind of is arranged on Radar Carrier platform by all radar equipments, can move quickly into the work place of specifying, and is applicable to vehicular aviation management primary radar that is standby in emergent calamity or other provisional application scenarios.
For achieving the above object, the utility model have employed following technical scheme: a kind of vehicular aviation management primary radar, comprise vehicular platform, described vehicular platform is large-scale specialized truck platform, its truck frame is installed respectively the primary radar electronic shelter of leveling support leg, built-in primary radar electronic equipment, and the antenna combination to be made up of antenna, turntable and horizon sensor, the cabin body of described primary radar electronic shelter fixedly mounts GPS location sensor for gathering GPS position information and for the communication interface module with extraneous communication.
The built-in transmitter of described primary radar electronic shelter, receiver, signal processing module, data processing module, servo control module and leveling controller, the output terminal of described receiver is connected with the input end of transmitter, receiver and signal processing module both-way communication, the output terminal of signal processing module is connected with the input end of data processing module, and the output terminal of data processing module is by communication interface module and supervisory system communication; The output terminal of described servo control module is connected with the signal input part of turntable, and the input end of leveling controller is connected with the output terminal of horizon sensor, and the signal input part that leg is supportted in output terminal and the leveling of leveling controller is connected.
The number of described leveling support leg is four, and be arranged on four edges of truck frame respectively, described horizon sensor, antenna are all installed on turntable, and turntable is installed in truck frame.
The side of described primary radar electronic shelter sets firmly the air-conditioning for regulating temperature in its cabin.
Described transmitter, receiver, signal processing module, data processing module and servo control module composition LAN (Local Area Network).
As shown from the above technical solution, advantage of the present utility model is as follows: first, all radar equipments have been arranged on Radar Carrier platform all, only need carry after car is transported to the work place of specifying, just can carry out automatic leveling to radar antenna level, carry out automatically to north to antenna bearingt, visible, the utility model can move quickly into the work place of specifying, and is applicable to or other provisional application scenarios standby in emergent calamity; The second, the utility model is connected to the supervisory system at air traffic control center by its communication interface module, promptly can shoulder the task of air-traffic control; 3rd, the utility model has various communication interfaces, as network, optical fiber, microwave etc., to the some track data of supervisory system transmission monitoring target at air traffic control center and the work state information of radar equipment, and can accept the remote control of remote terminal during work.
Accompanying drawing explanation
Fig. 1 is the block diagram of system of the present utility model;
Fig. 2 is topology layout schematic diagram of the present utility model.
Embodiment
A kind of vehicular aviation management primary radar, comprise vehicular platform 1, described vehicular platform 1 is large-scale specialized truck platform, this vehicular platform 1 has truck cabin 9 and wheel 10, the truck frame 2 of this vehicular platform 1 is installed respectively leveling support leg 3, the primary radar electronic shelter 4 of built-in primary radar electronic equipment, and by antenna 5a, the antenna combination 5 that turntable 5b and horizon sensor 5c forms, the cabin body of described primary radar electronic shelter 4 fixedly mounts GPS location sensor 6 for gathering GPS position information and for the communication interface module 7 with extraneous communication, as shown in Figure 2.Vehicular platform 1 is a large-scale specialized truck platform through repacking; The hydraulic auxiliary support system that leveling support leg 3 uses when being radar system erections, antenna combination 5 is fixed on the middle part of vehicular platform 1, can carry out the automatic leveling of antenna level and the automatic to north of antenna bearingt before radar enters duty.
As shown in Figure 1, the built-in transmitter 4a of described primary radar electronic shelter 4, receiver 4b, signal processing module 4c, data processing module 4d, servo control module 4e and leveling controller 4f, the output terminal of described receiver 4b is connected with the input end of transmitter 4a, receiver 4b and signal processing module 4c both-way communication, the output terminal of signal processing module 4c is connected with the input end of data processing module 4d, and the output terminal of data processing module 4d is by communication interface module 7 and supervisory system communication; The output terminal of described servo control module 4e is connected with the signal input part of turntable 5b, and the input end of leveling controller 4f is connected with the output terminal of horizon sensor 5c, and the signal input part that leg 3 is supportted in output terminal and the leveling of leveling controller 4f is connected.Described transmitter 4a, receiver 4b, signal processing module 4c, data processing module 4d and servo control module 4e form LAN (Local Area Network).
As shown in Figure 2, the number of described leveling support leg 3 is four, and be arranged on four edges of truck frame 2 respectively, described horizon sensor 5c, antenna 5a are all installed on turntable 5b, and turntable 5b is installed in truck frame 2; The side of described primary radar electronic shelter 4 sets firmly the air-conditioning 8 for regulating temperature in its cabin.Communication interface module 7 has the multiple interfaces such as network, optical fiber, microwave, to the some track data of supervisory system transmission monitoring target at air traffic control center and the work state information of radar equipment, and can accept the remote control of remote terminal during work.
Be further described below in conjunction with Fig. 1,2 pairs of the utility model.
After radar transport arrives assigned work position, first energising and the horizontal information measured by leveling controller 4f perception horizon sensor 5c go control leveling support leg 3, the surfaces of revolution of antenna 5a is made automatically to be adjusted to level, the GPS location sensor 6 being arranged on primary radar electronic shelter 4 top for a pair is parked directional information and is fed to by LAN (Local Area Network) the initial positive north value that data processing module 4d is used for revising antenna 5a by carrying car, namely automatic to north.During work, antenna 5a rotates with turntable 5b, and turntable 5b rotates and controlled by the servo control module 4e in primary radar electronic shelter 4, and supervisory system reaches the object of control antenna 5a by LAN (Local Area Network) monitoring servo control module 4e.
The course of work of radar system is: receiver 4b produces clock signal of system and send signal processing module 4c, signal processing module 4c produces system triggers signal, receiver 4b is under the control of system clock and trigger pip, produce and launch pumping signal and be sent to transmitter 4a and carry out power amplification, high-power transmitting is gone out to space radiation finally by antenna 5a.Electromagnetic wave encounters airbound target by reflection electromagnetic wave in space, reflection echo signal is intercepted and captured through antenna 5a and is imported receiver 4b into, the process such as radio frequency amplification in receiver 4b, down coversion, intermediate frequency amplification, orthogonal transformation provides orthogonal i/q signal and send signal processing module 4c, signal processing module 4c detects that the some mark signal of airbound target send data processing module 4d to form the Track In Track information of airbound target, and these information are finally sent into the supervisory system that communication interface module 7 is connected to the air traffic control center of far-end and shown.In primary radar electronic shelter 4, each electronic device works state is also connected with supervisory system by LAN (Local Area Network), air traffic control center reaches running parameter and the failure message of communication interface module 7 dynamic surveillance radar equipment each several part by supervisory system, and remote control also can be carried out to radar equipment mode of operation and switching on and shutting down in air traffic control center simultaneously.
In sum, all radar equipments of the present utility model have been arranged on Radar Carrier platform 1 all, only need carry after car is transported to the work place of specifying, just can carry out automatic leveling to radar antenna level, antenna bearingt is carried out automatically north, the utility model can move quickly into the work place of specifying, and is applicable to or other provisional application scenarios standby in emergent calamity.
Claims (5)
1. a vehicular aviation management primary radar, it is characterized in that: comprise vehicular platform (1), described vehicular platform (1) is large-scale specialized truck platform, its truck frame (2) is installed respectively leveling support leg (3), the primary radar electronic shelter (4) of built-in primary radar electronic equipment, and by antenna (5a), the antenna combination (5) that turntable (5b) and horizon sensor (5c) form, the cabin body of described primary radar electronic shelter (4) fixedly mounts GPS location sensor (6) for gathering GPS position information and for the communication interface module (7) with extraneous communication.
2. vehicular aviation management primary radar according to claim 1, it is characterized in that: the built-in transmitter of described primary radar electronic shelter (4) (4a), receiver (4b), signal processing module (4c), data processing module (4d), servo control module (4e) and leveling controller (4f), the output terminal of described receiver (4b) is connected with the input end of transmitter (4a), receiver (4b) and signal processing module (4c) both-way communication, the output terminal of signal processing module (4c) is connected with the input end of data processing module (4d), the output terminal of data processing module (4d) is by communication interface module (7) and supervisory system communication, the output terminal of described servo control module (4e) is connected with the signal input part of turntable (5b), the input end of leveling controller (4f) is connected with the output terminal of horizon sensor (5c), and the signal input part that leg (3) is supportted in output terminal and the leveling of leveling controller (4f) is connected.
3. vehicular aviation management primary radar according to claim 1, it is characterized in that: the number of described leveling support leg (3) is four, be arranged on four edges of truck frame (2) respectively, described horizon sensor (5c), antenna (5a) are all installed on turntable (5b), and turntable (5b) is installed in truck frame (2).
4. vehicular aviation management primary radar according to claim 1, is characterized in that: the side of described primary radar electronic shelter (4) sets firmly the air-conditioning (8) for regulating temperature in its cabin.
5. vehicular aviation management primary radar according to claim 2, is characterized in that: described transmitter (4a), receiver (4b), signal processing module (4c), data processing module (4d) and servo control module (4e) form LAN (Local Area Network).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520542140.1U CN204832505U (en) | 2015-07-24 | 2015-07-24 | Vehicular aviation management primary radar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520542140.1U CN204832505U (en) | 2015-07-24 | 2015-07-24 | Vehicular aviation management primary radar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204832505U true CN204832505U (en) | 2015-12-02 |
Family
ID=54690090
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520542140.1U Active CN204832505U (en) | 2015-07-24 | 2015-07-24 | Vehicular aviation management primary radar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204832505U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105044708A (en) * | 2015-07-24 | 2015-11-11 | 安徽四创电子股份有限公司 | Vehicle-mounted air traffic control primary radar |
-
2015
- 2015-07-24 CN CN201520542140.1U patent/CN204832505U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105044708A (en) * | 2015-07-24 | 2015-11-11 | 安徽四创电子股份有限公司 | Vehicle-mounted air traffic control primary radar |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105044708A (en) | Vehicle-mounted air traffic control primary radar | |
| CN204316545U (en) | Based on the Unmanned Aerial Vehicle Data link system of mobile communications network | |
| CN103873133B (en) | A kind of communication and navigation monitoring system based on multimode data link | |
| CN100517413C (en) | ADS-B control workstation data processing system | |
| EP1849260B1 (en) | Method and system for subterranean wireless data transmission between at least one mobile station and a fixed network by means of a radio network | |
| CN108011659A (en) | A kind of UAV Communication method, apparatus and unmanned plane | |
| US20100265848A1 (en) | System for automatic configuration of a mobile communication system | |
| CN106325298A (en) | Unmanned plane range extension control system and unmanned plane range extension control method | |
| CN107121987A (en) | A kind of unmanned plane multiterminal remotely continue the chain-circuit system of control | |
| CN103369671A (en) | Close-range positioning system and method based on WIFI | |
| CN204013537U (en) | A kind of communication and navigation surveillance based on multimode data link | |
| CN105282698A (en) | Method of acquiring GPS signal and system thereof | |
| CN204331799U (en) | Real-time vehicle-mounted cold chain transportation information monitoring system | |
| US11978350B2 (en) | Data acquisition system and method for airborne navigation devices based on unmanned aerial vehicle | |
| CN204832505U (en) | Vehicular aviation management primary radar | |
| CN111698639B (en) | Control method, system, equipment and storage medium for signal coverage of air route | |
| WO2012062008A1 (en) | Intelligent radar detection device and method thereof | |
| CN104820209A (en) | Multilaser-action surveillance inquiry transmitter for civil aviation and inquiry method thereof | |
| KR20180064271A (en) | Surveillance method for unmanned aerial vehicle, and surveillance apparatus for the same | |
| CN108123749A (en) | A kind of communication relay backs up unmanned mobile device, topological system and construction method | |
| CN202158845U (en) | Airplane crack real-time monitoring system based on Beidou navigation satellites | |
| CN204575845U (en) | The interrogator transmitter of a kind of civil aviaton multipoint positioning | |
| CN105109661A (en) | Monitoring method and network based on aerostats and aerostat | |
| CN112835382A (en) | 5G base station test system based on unmanned aerial vehicle | |
| CN206431837U (en) | A kind of real-time measurement and management system of high-precision unmanned vehicle satellite link in full spatial domain |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |