CN203165241U - Maneuvering control system based on broadcast type automatic dependent surveillance - Google Patents
Maneuvering control system based on broadcast type automatic dependent surveillance Download PDFInfo
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- CN203165241U CN203165241U CN 201320115849 CN201320115849U CN203165241U CN 203165241 U CN203165241 U CN 203165241U CN 201320115849 CN201320115849 CN 201320115849 CN 201320115849 U CN201320115849 U CN 201320115849U CN 203165241 U CN203165241 U CN 203165241U
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Abstract
The utility model provides a maneuvering control system based on broadcast type automatic dependent surveillance. The system comprises a voice communication device, a satellite single receiving station, a 1090ES data link ground station, a position management system, an information and business processing system, and further comprises a mobile apparatus, wherein the above-mentioned systems are integrated and disposed on the mobile apparatus so as to satisfy mobile control of the whole system. The maneuvering ADS-B control system has the advantages such as strong maneuverability, low cost, good system compatibility and flexible and rapid system deployment. Within radar coverage, the maneuvering ADS-B control system is an effective supplement to the radar surveillance means, can provide correction or blind compensation for the radar surveillance means; and out of the radar coverage, the maneuvering ADS-B control system serves as an independent surveillance means, and can monitor and command aircrafts in the surveillance scope.
Description
Technical field
The utility model relates to blank pipe surveillance technology field, particularly relates to a kind of motor driven control system based on Automatic dependent surveillance broadcast.
Background technology
Since the reform and opening-up, China is being explored aspect the airspace management reform of low latitude, and low latitude airspace management policies and regulations are put into effect in succession, and operational management is updated, and the guarantee means improve, and pilot reform has obtained first-stage success.In this simultaneously, must see that the low latitude airspace management exists also that the spatial domain is divided inadequately rationally, the not enough science of management system, operating mechanism inadequately smooth and easy, rules and regulations are not well established, safety responsibility distinct, service guarantee problem such as perfect inadequately inadequately, also have big gap with General Aviation user and the public's expectation.
Automatic dependent surveillance broadcast (ADS-B) is to utilize aircraft to broadcast the precise location information that is generated by airborne satellite-based navigation and positioning system automatically, receive this information by uphole equipment and other aircrafts by aeronautical data chain, satellite system, aircraft and ground based system are realized the integrative coordinated supervision in the empty world by the high-speed data chain.ADS-B has not only overcome some problems of traditional radar surveillance means, and has advantages such as precision height, turnover rate height, applied range, uphole equipment construction and maintenance cost are low.
As an important surveillance technology in the following new navigation system, at radar-covered area, ADS-B will be as effectively the replenishing of radar surveillance means, to its calibration or mend blind; At non-radar-covered area, ADS-B will become a kind of means that independently monitor, a kind of new supervision means are provided.Present ADS-B can adopt 1090 expansion interrupted oscillations (1090ES), general-purpose accessing transmitting-receiving UAT and very high frequency(VHF) data chain pattern 4(VDL4) etc. several data chains realize, especially adopt that 1090ES data chain cost is low, system compatibility good, and applied range.
The utility model content
In order to overcome the problem that there is blind spot in radar surveillance of the prior art, a kind of surveillance technology based on motor driven ADS-B control system is proposed, effectively mend blind to traditional supervision blind spot and calibration.
The utility model adopts following technical scheme: a kind of motor driven control system based on Automatic dependent surveillance broadcast, and described system comprises voice communication device, Satellite Receiving system, 1090ES data chain land station, location management system, information and transaction processing system; Also comprise mobile device, each above-mentioned system integration is installed on the mobile device, satisfies the mobile control of system.
In the above-mentioned control system, described mobile device is for carrying car.
In the above-mentioned control system, the shelter car that described year car is four-wheel drive.
Wherein, carry a car and provide mounting platform and motor-driven transportation for system, arrive the work place after, the staff can launch vehicle, erects a television antenna, behind the opening device, carry out work on the seat in can being sitting in.Carrying car not only provides the operating space that power supply, illumination, air-conditioning, support fixation system etc. also are provided, and this guarantees the trouble-free operation that motor driven control system can be under various environment.
Voice communication device provides ground-ground Speech Communication and ground-air Speech Communication ability for motor driven ADS-B control system, finishes the transmission to sky of navigational intelligence, meteorologic information and flight information etc. simultaneously and serves.Operating personnel use ground to air radio set to realize communicating by letter of ground and aircraft, it mainly is the voice communication with the pilot, by to all communicate by letter with the plane, ground speech synthesis scheduling of (control phone, transposer station and intercom) of communication to empty VHF, HF, realize that air traffic control, navigational matters manage and sky is broadcasted
Satellite Receiving system is made up of Satellite Receiving system, satellite earth antenna, protocol converter etc., this equipment is by the receiving radar monitor message, for motor driven ADS-B control system provides other monitor messages except the ADS-B monitor message, the system that makes can merge different monitoring datas, realizes accurate tracking and the supervision of target.
1090ES data chain land station is made up of 1090ES data chain land station main frame, ADS-B receiving antenna and GPS receiving antenna etc.After this equipment receives the ADS-B message of aircraft broadcasting at 1090ES data chain land station main frame, therefrom extract the S pattern address, identifying information (ID), longitude and latitude of aircraft, highly, information such as speed, course, be assembled into the report that meets the ASTERIX standard, form the air scout data, be transferred to planning management seat and the control commander seat of information and service process subsystem by network, by the report of ADS-B flight path is converted to flight track curve intuitively, can obtain the detailed state parameter of aircraft, be used for air traffic control.
Location management system is made up of NTP network time server, the network switch, GNSS antenna etc., this system receives the GNSS satellite data, produce the Network Synchronization clock data, be sent to other equipment by LAN (Local Area Network), finishing the functions such as time synchronized, zone of responsibility setting of location, each equipment of system of system, is accurately prerequisite and the guarantee of operation of system.
Information and transaction processing system: formed by control commander seat, planning management seat, server, KVM control desk, portable PC, ADS-B information access gateway, mobile 3G module, printer etc., this system provides data processing function and work seat man machine operation interface, finishes control commander and flight service function.Wherein control command function comprises: situation supervision, early warning and alarm, flight planning and flight path pairing, flight collision identification, the supervision of flight path consistance, control transfer etc.; The flight service comprises: navigational intelligence service, meteorologic information service, flight information service.
Motor driven ADS-B control system is by the aircraft information in 1090ES data chain or the satellite link receiving control spatial domain, and after these information are carried out a series of fusion treatment, for ground Control Centre provides flight information in this spatial domain, be convenient to the real-time accurate tracking target of ground Control Centre and monitor peripheral spatial domain traffic; The ground that system provides by telephone system in ground to air radio set and the seat on the other hand-ground Speech Communication and ground-air Speech Communication ability are finished the transmission to sky of navigational intelligence, meteorologic information and flight information etc. and are served.The internal lan network that each equipment room of system is formed by the network switch communicates.Motor driven ADS-B control system can ensure General Aviation Flight and army's aerial mission, implements air traffic control commander and flight plan management.
Advantage of the present utility model is: motor driven ADS-B control system has mobility strong, cost is low, system compatibility good, system disposes and flexibly and fast waits advantage.At radar-covered area, motor driven ADS-B control system effectively replenishes as the radar surveillance means, to its calibration or mend blind; At non-radar-covered area, motor driven ADS-B control system can monitor commander to the aircraft in the monitoring range as a kind of means that independently monitor.
Description of drawings
The utility model will illustrate by embodiment and with reference to the mode of accompanying drawing, wherein:
Fig. 1 is system's composition diagram of motor driven ADS-B control system of the present invention;
Fig. 2 handles block diagram for system data.
Embodiment
Below in conjunction with accompanying drawing the utility model is described further.
In motor driven ADS-B control system operational process, provide reliable and stable physical support by carrying car system other subsystem for motor driven ADS-B control system, as running environment stably, stable electric power supply etc.
The NTP network time server receives GNSS location and the time synchronized data A1 that the GNSS satellite sends by the GNSS antenna in as Fig. 1 and Fig. 2, and by the network switch equipment that is connected internal lan is transmitted network time service data B1, guaranteed the time synchronized of all computing machines, instrument, equipment in the motor driven ADS-B control system internal lan network.
In speech equipment as depicted in figs. 1 and 2, ground to air radio set receives and sends voice signal A4 to aircraft by the radio station dual-mode antenna, realization is the voice communication with the pilot, and voice data B4 is sent to control commander system and datalogger by LAN (Local Area Network); Words are then by to all communicate by letter with the plane, ground speech synthesis scheduling of (control phone, transposer station and intercom) of communication to empty VHF, HF in the seat, realize that air traffic control, navigational matters manage and sky is broadcasted; Datalogger carries out complete record to the data that speech equipment produces, and playback is provided.
In Satellite Receiving system subsystem as depicted in figs. 1 and 2, the A3 data of Satellite Receiving system receiving antenna received communication satellite broadcasting via satellite transmission, and formation B3 packet, be sent to planning management seat etc. by LAN (Local Area Network), comprise information on services such as flight announcement, radar data information, navigational information and weather data, and these information processings are become information and the transaction processing system of giving behind the C3.
In 1090ES data chain land station subsystem as depicted in figs. 1 and 2,1090ES data chain land station's main frame and ADS-B omnidirectional antenna and reception are from the 1090ES data chain message data A2 of aerial aircraft, and through 112 original messages of decoding acquisition, original message is resolved reorganization, obtain the CAT021 flight path report of standard, output to information and transaction processing system by Ethernet; 1090ES data chain land station main frame carries out real-time self check simultaneously, determine local state according to self-detection result, cooperate information such as GNSS time that the GNSS satellite that receives sends, position to form the CAT023 status report with the GNSS receiving antenna in conjunction with 1090ES data chain land station main frame, output to information and transaction processing system by Ethernet, these two data is the B2 among Fig. 2.
As shown in Fig. 1 and Fig. 2, control commander system and planning management seat obtain every data that other subsystem provides by the network switch, these data are handled, merged, and by work seat man machine operation interface, finish flight service functions such as control command function such as situation supervision, early warning and alarm, flight planning and flight path pairing, the supervision of flight path consistance and navigational intelligence service, meteorologic information service, flight information service.The KVM control desk cooperates server by the network switch various device in the motor driven ADS-B control system internal lan network to be carried out condition monitoring.The ADS-B data that ADS-B information access gateway can produce 1090ES data chain land station subsystem are to the mapping of ADS-B army style formula.
Mobile 3G module receives the data A5 of internet, produces the B5 data and sends into portable PC, is used for finishing relevant demonstration and the operation of notice to airmen, flight information, meteorologic information.
Printer provides high-quality print service for control commander system, planning management seat, server, portable PC etc.
Disclosed all features in this instructions except mutually exclusive feature, all can make up by any way.
Disclosed arbitrary feature in this instructions (comprising any accessory claim, summary and accompanying drawing) is unless special narration all can be replaced by other equivalences or the alternative features with similar purpose.That is, unless special narration, each feature is an example in a series of equivalences or the similar characteristics.
The above only is preferred embodiment of the present utility model; not in order to limit the utility model; all any modifications of within spirit of the present utility model and principle, doing, be equal to and replace and improvement etc., all should be included within the protection domain of the present utility model.
Claims (3)
1. the motor driven control system based on Automatic dependent surveillance broadcast is characterized in that described system comprises voice communication device, Satellite Receiving system, 1090ES data chain land station, location management system, information and transaction processing system; Also comprise mobile device, each above-mentioned system integration is installed on the mobile device, satisfies the mobile control of system.
2. a kind of motor driven control system based on Automatic dependent surveillance broadcast according to claim 1 is characterized by described mobile device for carrying car.
3. a kind of motor driven control system based on Automatic dependent surveillance broadcast according to claim 2, the shelter car that to it is characterized by described year car be four-wheel drive.
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| Application Number | Priority Date | Filing Date | Title |
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| CN 201320115849 CN203165241U (en) | 2013-03-14 | 2013-03-14 | Maneuvering control system based on broadcast type automatic dependent surveillance |
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| CN 201320115849 CN203165241U (en) | 2013-03-14 | 2013-03-14 | Maneuvering control system based on broadcast type automatic dependent surveillance |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103617749A (en) * | 2013-11-15 | 2014-03-05 | 中国航空无线电电子研究所 | Onboard system and method for managing land-air commands |
| CN103646569A (en) * | 2013-12-03 | 2014-03-19 | 海丰通航科技有限公司 | General aviation low-altitude monitor and service system |
| CN104637348A (en) * | 2014-12-22 | 2015-05-20 | 华北计算技术研究所 | Portable emergency controlling system and emergency controlling method thereof |
| CN107564340A (en) * | 2017-09-12 | 2018-01-09 | 周俊杰 | Unattended aircraft information gathering transmission surface process and device |
| CN107578646A (en) * | 2017-08-28 | 2018-01-12 | 梁晓龙 | low slow small target detection monitoring management system and method |
| CN109544997A (en) * | 2018-12-27 | 2019-03-29 | 四川九洲空管科技有限责任公司 | A kind of mobile control tower based on blank pipe communication and surveillance technology |
| CN111245501A (en) * | 2020-01-16 | 2020-06-05 | 海丰通航科技有限公司 | Communication module and command center server applied to very high frequency aviation radio station |
| CN111882927A (en) * | 2020-07-03 | 2020-11-03 | 中国民用航空总局第二研究所 | 1090ES link ADS-B technology-based command operation management system and method |
| CN112700679A (en) * | 2020-12-09 | 2021-04-23 | 四川九洲空管科技有限责任公司 | Cooperative low-altitude airspace target monitoring system |
-
2013
- 2013-03-14 CN CN 201320115849 patent/CN203165241U/en not_active Expired - Lifetime
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103617749A (en) * | 2013-11-15 | 2014-03-05 | 中国航空无线电电子研究所 | Onboard system and method for managing land-air commands |
| CN103617749B (en) * | 2013-11-15 | 2015-12-09 | 中国航空无线电电子研究所 | A kind of airborne land dummy instruction management system and management method thereof |
| CN103646569A (en) * | 2013-12-03 | 2014-03-19 | 海丰通航科技有限公司 | General aviation low-altitude monitor and service system |
| CN103646569B (en) * | 2013-12-03 | 2016-06-08 | 海丰通航科技有限公司 | A kind of general aviation low-altitude monitor and service system |
| CN104637348A (en) * | 2014-12-22 | 2015-05-20 | 华北计算技术研究所 | Portable emergency controlling system and emergency controlling method thereof |
| CN107578646A (en) * | 2017-08-28 | 2018-01-12 | 梁晓龙 | low slow small target detection monitoring management system and method |
| CN107564340A (en) * | 2017-09-12 | 2018-01-09 | 周俊杰 | Unattended aircraft information gathering transmission surface process and device |
| CN109544997A (en) * | 2018-12-27 | 2019-03-29 | 四川九洲空管科技有限责任公司 | A kind of mobile control tower based on blank pipe communication and surveillance technology |
| CN111245501A (en) * | 2020-01-16 | 2020-06-05 | 海丰通航科技有限公司 | Communication module and command center server applied to very high frequency aviation radio station |
| CN111882927A (en) * | 2020-07-03 | 2020-11-03 | 中国民用航空总局第二研究所 | 1090ES link ADS-B technology-based command operation management system and method |
| CN112700679A (en) * | 2020-12-09 | 2021-04-23 | 四川九洲空管科技有限责任公司 | Cooperative low-altitude airspace target monitoring system |
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Granted publication date: 20130828 |
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| CX01 | Expiry of patent term |