CN109727493A - Based on the unmanned plane monitoring system of integrated answering machine and its response, ADS-B OUT/IN method - Google Patents
Based on the unmanned plane monitoring system of integrated answering machine and its response, ADS-B OUT/IN method Download PDFInfo
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Abstract
The present invention relates to unmanned plane blank pipe monitoring system technical fields, disclose the unmanned plane monitoring system based on integrated answering machine.Including the airborne end of UAV targets (including integrated answering machine, onboard flight control system, omnidirectional's dual-mode antenna and the airborne chain-circuit system being made of responder module and ADS-B module), air traffic control system ground surface end (including secondary radar, control tower end monitoring system and omnidirectional's dual-mode antenna) and UAV targets' ground control terminal (including flight monitoring computer and ground surface end chain-circuit system)；The integration answering machine and secondary radar, control tower end monitoring system, flight monitoring computer and airborne flight control system communicate to connect, omnidirectional's dual-mode antenna is used for the transceiver communication of air traffic control system ground surface end and the airborne end of UAV targets, and the airborne chain-circuit system, ground surface end chain-circuit system are used for the communications at UAV targets airborne end and UAV targets' ground control terminal.The technical solution realizes response, ADS-B OUT/IN method, simplifies equipment and effectively realizes monitoring.
Description
Technical field
The present invention relates to unmanned plane blank pipe monitoring system technical fields, are based especially on the unmanned plane monitoring system of integrated answering machine
System and its response, ADS-B OUT/IN method.
Background technique
With the continuous development of domestic Large freight unmanned plane, this kind of unmanned plane is due to flight time and aircarrier aircraft phase in the sky
Difference is no different, and flying area and flying height also will affect aircarrier aircraft, and how this kind of unmanned plane avoids the people in flight course
The line of flight of boat aircraft, guarantees that respective safe flight is particularly important.
It is current flight monitoring system platform building of the country in relation to bulk transport unmanned plane and not perfect, many large size nothings
It is man-machine also only to rest on the development and design stage；The large-scale unmanned plane that several families make a successful trial flight also only rests on development and takes a flight test rank
Section, thus the flight monitoring system or platform docked with civil aviation authority do not build it is perfect.
The many unmanned plane during flying monitoring systems occurred on the market are mainly for small and medium size unmanned aerial vehicles system, and the equipment for including
Excessively, structure is complicated, higher cost, and signal transmitting intermediary is excessive, such as patent [Authorization Notice No. CN101714300B]
In unmanned plane monitoring system include ADS-B system, have IN and OUT function, but cannot to air traffic control system send response ask
It asks that signal is responded, is adjusted for real-time airspace environment；Unmanned plane involved in patent [CN201610905166]
Flight monitoring system also needs to configure an inspection unmanned plane and goes monitoring UAV targets, hence it is evident that increases control difficulty and equipment
Cost；The airplane information on unmanned plane periphery is directly transferred to the ground of unmanned plane in patent [Authorization Notice No. CN105913692B]
Face control station goes the flight of control unmanned plane by ground control station, and the requirement to air traffic control system increases, in addition this kind of flight prison
Viewing system is mainly for low altitude airspace management；Unmanned plane during flying monitoring system in patent application [publication number CN107943091A]
Flight supervision equipment is mounted on ground surface end, equipment degrees of fusion is higher, but increases for the unmanned plane of single rack time monitoring cost
Add.
It is comprehensive it is found that the flight monitoring system of bulk transport unmanned plane has that the device is complicated at present, it is at high cost, function is insufficient and
Information transmits the disadvantages of intermediary is excessive.
Summary of the invention
The technical problems to be solved by the present invention are: more for above-mentioned unmanned plane monitoring system equipment, installation is complicated, function
Can be single, the excessive problem of at high cost and information transmission intermediary provides the unmanned plane monitoring system based on integrated answering machine
System and its response, ADS-B OUT/IN method.
The technical solution adopted by the invention is as follows: the unmanned plane monitoring system based on integrated answering machine, specifically include target without
Man-machine airborne end, air traffic control system ground surface end and UAV targets' ground control terminal；
The airborne end of UAV targets includes the integrated answering machine being made of responder module and ADS-B module, onboard flight
Control system, omnidirectional's dual-mode antenna and airborne chain-circuit system, the air traffic control system ground surface end include secondary radar, the monitoring of control tower end
System and omnidirectional's dual-mode antenna, UAV targets' ground control terminal include flight monitoring computer and ground surface end link system
System；
The integration answering machine and secondary radar, control tower end monitoring system, flight monitoring computer and airborne flight control system
Communication connection, omnidirectional's dual-mode antenna is used for the transceiver communication of air traffic control system ground surface end and the airborne end of UAV targets, described
The communication of airborne chain-circuit system, ground surface end chain-circuit system for the airborne end of UAV targets and UAV targets' ground control terminal passes
It is defeated.
Further, the responder module in the integrated answering machine and secondary radar carry out inquiry communication, and responder module gives two
Secondary radar provides that the A code of UAV targets, air pressure be high, sail information of GPS ground velocity, and sail information is transferred to control tower end
Monitoring system, control tower end monitoring system have answer supervision display interface, flight information are shown.
Further, the ADS-B module in the integrated answering machine passes through omnidirectional's dual-mode antenna for the A generation of UAV targets
The high sail information of code, flight number, GPS ground velocity, air pressure height, the address S, longitude and latitude is sent to control tower monitoring system, the monitoring of control tower end
Navigational parameter is shown to ADS-B monitoring display interface by system.
Further, in the navigational parameter of the UAV targets, the GPS ground velocity, air pressure height, longitude and latitude height are by airborne biography
Sensor obtains, and the address S immobilizes and obtained by air traffic control centre, and the flight number, A code are obtained by earth station,
The navigational parameter of the UAV targets of acquisition is transferred to airborne flight control system, and the airborne flight control system is transmitted through the cable to again
Integrated answering machine.
Further, the integrated answering machine receives A code, the longitude and latitude, air pressure of other aircrafts by omnidirectional's dual-mode antenna
High, GPS ground velocity sail information, and airborne flight control system is given by cable transmission, airborne flight control system passes through airborne link system
Sail information is sent to UAV targets' ground control terminal by system, ground surface end chain-circuit system.
The invention also discloses a kind of answer methods of unmanned plane monitoring system based on integrated answering machine, comprising:
UAV targets' responder module makes response after receiving the interrogation signal that air traffic control system ground surface end secondary radar is sent, instead
The response message of feedback includes the A code of UAV targets, air pressure height and GPS ground velocity and follows a certain form；
Air traffic control system ground surface end secondary radar answers the UAV targets' answer signal received by cable transmission to control tower end
Answer monitoring system；
Control tower end answer supervision system shows the UAV targets' answer signal received on answer supervision computer.
The invention also discloses a kind of ADS-B OUT methods of unmanned plane monitoring system based on integrated answering machine, comprising:
UAV targets fly in ground control station before taking off and control monitoring computer transponder modules setting ADS-B OUT state
Significance bit；
The onboard flight control system of UAV targets passes to integrated response by the airborne sail information that cable will acquire
Machine system；
ADS-B module in the integrated answering machine of UAV targets by omnidirectional's dual-mode antenna be constantly sent out target without
Man-machine A code, the address S, the sail information that flight number, air pressure is high, GPS ground velocity and longitude and latitude are high；
UAV targets' boat that control tower end monitoring system is sent by the ADS-B module that omnidirectional's dual-mode antenna receives UAV targets
Row information is simultaneously shown on ADS-B monitoring computer；
Air traffic control system control tower end blank pipe personnel according to ADS-B monitor computer on sail information and voice communication apparatus to target
Unmanned plane is monitored in real time and is dispatched.
The invention also discloses a kind of ADS-B IN methods of unmanned plane monitoring system based on integrated answering machine, comprising:
UAV targets fly in UAV targets' ground control station before taking off and control monitoring computer transponder modules setting
ADS-B IN state significance bit；
UAV targets' ADS-B module of integrated answering machine in flight course receives other aircrafts by omnidirectional's dual-mode antenna
The A code of transmission, longitude and latitude, the sail information of air pressure height and ground velocity；
The flight information of other aircrafts is transferred to the machine of UAV targets by cable by the integrated answering machine of UAV targets
Carry flight control system；
The airborne flight control system of UAV targets is believed the navigation of other aircrafts by airborne chain-circuit system, ground surface end chain-circuit system
Breath is transferred to ground control terminal；
Operator in UAV targets' ground control terminal monitors other aircrafts and UAV targets on computer according to flight
Sail information and voice communication apparatus realize the real-time monitoring and scheduling to UAV targets jointly.
Compared with prior art, having the beneficial effect that by adopting the above technical scheme
The airborne answering machine of UAV targets becomes one responder module and ADS-B module, and installation, maintenance and replacement are just
Benefit increases, and cost reduces；
Corresponding sail information acquired in the airborne transponder system of UAV targets is directed to onboard flight control system
With answering machine itself, guarantee the real-time and accuracy of UAV targets' flight information；
The airborne transponder system of UAV targets can also receive other while capable of constantly sending sail information in real time outward
The real-time flight information that aircraft is sent；
UAV targets can make real-time response according to the interrogation signal that air traffic control system ground surface end secondary radar is sent, and ensure that
The real-time and validity that air traffic control system monitors UAV targets；
UAV targets' control station can simultaneously real-time reception the machine and other aircrafts flight information, can real-time ensuring target without
Man-machine safety orderly flies and makes emergency reaction to emergency case.
Detailed description of the invention
Fig. 1 is the composed structure schematic diagram of the unmanned plane monitoring system of integrated answering machine of the invention.
Fig. 2 is the transport stream signal journey schematic diagram of the unmanned plane monitoring system of integrated answering machine of the invention.
Fig. 3 is the function and signal flow diagram of response part in integrated transponder system of the present invention；
Fig. 4 is the function and signal flow diagram of ADS-B OUT in integrated transponder system of the present invention；
Fig. 5 is the function and signal flow diagram of ADS-B IN in integrated transponder system of the present invention；
Fig. 6 is the flight information source of UAV targets and the biography at airborne end in integrated transponder system of the present invention
Pass process.
Specific embodiment
The present invention is described further with reference to the accompanying drawing.
As shown in Figure 1, a kind of unmanned plane monitoring system based on integrated answering machine, specifically include the airborne end of UAV targets,
Air traffic control system ground surface end and UAV targets' ground control terminal；The airborne end of UAV targets includes by responder module and ADS-
Integrated answering machine, onboard flight control system, omnidirectional's dual-mode antenna and the airborne chain-circuit system of B module composition, the blank pipe
System ground surface end includes secondary radar, control tower end monitoring system and omnidirectional's dual-mode antenna, UAV targets' ground control terminal
Including flight monitoring computer and ground surface end chain-circuit system；
The integration answering machine and secondary radar, control tower end monitoring system, flight monitoring computer and airborne flight control system
Communication connection, (air traffic control system ground surface end and the airborne control terminal of UAV targets have respective omnidirectional to omnidirectional's dual-mode antenna
Dual-mode antenna) it is used for the transceiver communication of air traffic control system ground surface end and the airborne end of UAV targets, the airborne chain-circuit system, ground
Chain-circuit system is held to be used for the communications at UAV targets airborne end and UAV targets' ground control terminal.As shown in Fig. 2, this reality
It applies in the system of example, integrated answering machine can receive the inquiry message of air traffic control system ground surface end secondary radar transmission, according to phase
The inquiry message answered makes response；Airborne integration transponder system is sent out UAV targets' flight information, target in real time
Unmanned aerial vehicle control terminal is obtained the sail information of UAV targets in real time and can also be obtained by ground surface end chain-circuit system
The response setting display interface of the sail information of other aircrafts in airspace, flight monitoring computer can show sail information
Show, the control tower end monitoring system of UAV targets' ground control terminal and air traffic control system ground surface end jointly carries out UAV targets real
When monitor, in combination with voice communication apparatus, realize and UAV targets monitored in real time and are dispatched.
The above-mentioned unmanned plane monitoring system based on integrated answering machine includes the answering of UAV targets, ADS-B OUT function
Can, ADS-B IN function.
One, answering process
As shown in Fig. 2, the secondary radar at air traffic control system control tower end sends interrogation signal to UAV targets；
UAV targets' responder module receives the inquiry of air traffic control system ground surface end secondary radar transmission by omnidirectional's dual-mode antenna
Signal, interrogation signal therein is sent by control tower end unified organizational system, not just for UAV targets, also directed to its of current airspace
Its aircraft；
Responder module feeds back response message to secondary radar by omnidirectional's dual-mode antenna, and the response message that secondary radar receives includes
The A code of UAV targets, air pressure height and GPS ground velocity；Detailed process are as follows: after UAV targets receive query message, machine
It carries flight control system and the relevant information of unmanned plane is passed into responder module；Responder module passes through omnidirectional's dual-mode antenna for target
The flight information (comprising the transmitting of airborne flight control system and answering machine itself setting) of unmanned plane is sent out according to certain format
Give air traffic control system ground surface end secondary radar；
UAV targets can basis by the flight information that omnidirectional's dual-mode antenna is sent to air traffic control system ground surface end secondary radar
Mode is selected, and specific mode includes full pass mode, A/S mode, A/S/C mode etc.；
By the UAV targets' answer signal received, (answer signal here includes airborne to air traffic control system ground surface end secondary radar
It is flight control system transmitting and answering machine itself setting) give control tower end answer supervision system by cable transmission；
Control tower end answer supervision system shows the UAV targets' answer signal received on answer supervision computer, blank pipe
UAV targets' information that personnel are shown by monitoring interface can monitor and track UAV targets in real time.
Two .ADS-B OUT functional sequences:
1. the preparation process of setting early period:
UAV targets and earth station normally power on, and check before navigating to UAV targets；
It is arranged accordingly in the integrated transponder modules of earth station's computer of UAV targets, by UAV targets one
Body answering machine ADS-B OUT function is opened, and specific setting option includes aviation management switch control, aviation management parameter setting and response
The selection setting of machine data；
The aviation management switch control item setting includes vacant lot state, position identification, mode switch, ADS-B OUT, air pressure height
Degree, ADS-B IN, oscillation switch；
The aviation management parameter setting includes A code, flight number and S mode address；
The answering machine data options setting does not include passing target data, passing most target datas down, pass nearest target down
Data have threat to pass at present；
2. the ADS-B OUT function and signals transmission of the present embodiment as shown in Figure 4
It is effective that ADS-B OUT corresponding state position is arranged in UAV targets in ground control station before take off；
The onboard flight control system of UAV targets passes to integrated response by the airborne sail information that cable will acquire
Machine system；
ADS-B module in the integrated answering machine of UAV targets by omnidirectional's dual-mode antenna be constantly sent out target without
Man-machine sail information, the unmanned plane sail information of transmission include high A code, the address S, flight number, air pressure, GPS ground velocity and
Longitude and latitude is high (longitude and latitude and geographical height)；Wherein the address S is fixed and invariable, from A code and flight number are transmitted by earth station,
And air pressure is high, GPS ground velocity and longitude and latitude and geographical height are measured by airborne sensor and obtained；
UAV targets' boat that control tower end monitoring system is sent by the ADS-B module that omnidirectional's dual-mode antenna receives UAV targets
Row information is simultaneously shown on ADS-B monitoring computer；
Air traffic control system control tower end blank pipe personnel monitor that the sail information on computer monitors in real time according to ADS-B, and cooperation is empty
Guard system and the voice communication apparatus of UAV targets are monitored in real time and are dispatched to UAV targets, common guarantee target without
Man-machine safe flight.
Airborne flight control system obtains the source of the sail information of UAV targets as shown in fig. 6, A code and flight number are earth stations
Setting sends airborne flight control system to by link, and the address S is that air traffic control system control tower end blank pipe personnel are passed by voice communication
The ground control station operator for passing UAV targets, is generally fixed and invariable, and operator monitors in ground control station and calculates
Onboard flight control system is given by link transmission after being arranged on machine, and longitude and latitude is high, air pressure is high, GPS ground velocity is all airborne sensing
Device passes to onboard flight control system.
Three .ADS-B IN functional sequences:
1. the preparation process of setting early period (as the preparation process of setting early period in ADS-B OUT functional sequence)
2. the ADS-B IN function and signals transmission of the present embodiment as shown in Figure 5
By ADS-B in the answering machine setup module of UAV targets' ground control station in being checked before the boat that UAV targets take off
The mode bit of IN is all set to effectively；
UAV targets' ADS-B module of integrated answering machine in flight course receives other aircrafts by omnidirectional's dual-mode antenna
The sail information of transmission；Because being mounted within the scope of the corresponding airspace of flight to outgoing in UAV targets' flight course
Other aircrafts (including aircarrier aircraft) of aircraft flight massaging device (such as ADS-B system) are sent to be sent out the machine flight letter in real time
Breath, so UAV targets can receive the sail information that other aircrafts are sent；
The received other aircraft flight information of the airborne answering machine ADS-B module of UAV targets include that (A code is aircraft to A code
Identification code), longitude and latitude, air pressure is high and ground velocity；
The flight information of other aircrafts is transferred to the machine of UAV targets by cable by the integrated answering machine of UAV targets
Carry flight control system；
The airborne flight control system of UAV targets is believed the navigation of other aircrafts by airborne chain-circuit system, ground surface end chain-circuit system
Breath is transferred to ground control terminal；
Operator in UAV targets' ground control terminal monitors other aircrafts and UAV targets on computer according to flight
Sail information and voice communication apparatus realize the real-time monitoring and scheduling to UAV targets jointly；Monitoring and scheduling process
In, the flight of UAV targets' ground control terminal monitoring computer by the sail information real-time display of other aircrafts, nobody
Operator in machine ground control terminal guarantees that UAV targets fly in the course line of safety according to the sail information of other aircrafts,
The voice communication apparatus of combining target unmanned plane monitors UAV targets in real time.
The invention is not limited to specific embodiments above-mentioned.The present invention expands to any new spy disclosed in the present specification
Sign or any new combination, and disclose any new method or process the step of or any new combination.If this field
Technical staff is altered or modified not departing from the unsubstantiality that spirit of the invention is done, should belong to right of the present invention and want
Seek the range of protection.
Claims (8)
1. the unmanned plane monitoring system based on integrated answering machine, which is characterized in that including the airborne end of UAV targets, blank pipe system
Ground surface end of uniting and UAV targets' ground control terminal；
The airborne end of UAV targets includes the integrated answering machine being made of responder module and ADS-B module, onboard flight
Control system, omnidirectional's dual-mode antenna and airborne chain-circuit system, the air traffic control system ground surface end include secondary radar, the monitoring of control tower end
System and omnidirectional's dual-mode antenna, UAV targets' ground control terminal include flight monitoring computer and ground surface end link system
System；
The integration answering machine and secondary radar, control tower end monitoring system, flight monitoring computer and airborne flight control system
Communication connection, omnidirectional's dual-mode antenna is used for the transceiver communication of air traffic control system ground surface end and the airborne end of UAV targets, described
The communication of airborne chain-circuit system, ground surface end chain-circuit system for the airborne end of UAV targets and UAV targets' ground control terminal passes
It is defeated.
2. as described in claim 1 based on the unmanned plane monitoring system of integrated answering machine, which is characterized in that the integration
Responder module and secondary radar in answering machine carry out inquiry communication, and responder module provides the A of UAV targets to secondary radar
Code, air pressure be high, GPS ground velocity sail information, and sail information is transferred to control tower end monitoring system, the control tower end monitoring
System has answer supervision display interface, and flight information is shown.
3. as claimed in claim 2 based on the unmanned plane monitoring system of integrated answering machine, which is characterized in that the integration
ADS-B module in answering machine by omnidirectional's dual-mode antenna by the A code of UAV targets, flight number, GPS ground velocity, air pressure it is high,
The high sail information of the address S, longitude and latitude is sent to control tower monitoring system, and navigational parameter is shown to ADS-B by control tower end monitoring system
Monitor display interface.
4. as claimed in claim 3 based on the unmanned plane monitoring system of integrated answering machine, which is characterized in that the target without
In man-machine navigational parameter, the GPS ground velocity, air pressure height, longitude and latitude height are obtained by airborne sensor, and the address S is fixed
It is constant and by air traffic control centre obtain, the flight number, A code by earth station acquisition, the navigation of the UAV targets of acquisition
Parameter is transferred to airborne flight control system, and the airborne flight control system is transmitted through the cable to integrated answering machine again.
5. as claimed in claim 4 based on the unmanned plane monitoring system of integrated answering machine, which is characterized in that the integration
Answering machine receives A code, longitude and latitude, the air pressure height of other aircrafts, the sail information of GPS ground velocity by omnidirectional's dual-mode antenna, and
Airborne flight control system is given by cable transmission, airborne flight control system will be navigated by water by airborne chain-circuit system, ground surface end chain-circuit system
Information is sent to UAV targets' ground control terminal.
6. the answer method of the unmanned plane monitoring system based on integrated answering machine characterized by comprising
UAV targets' responder module makes response after receiving the interrogation signal that air traffic control system ground surface end secondary radar is sent, instead
The response message of feedback includes the A code of UAV targets, air pressure height and GPS ground velocity；
Air traffic control system ground surface end secondary radar answers the UAV targets' answer signal received by cable transmission to control tower end
Answer monitoring system；
Control tower end answer supervision system shows the UAV targets' answer signal received on answer supervision computer.
7. the ADS-B OUT method of the unmanned plane monitoring system based on integrated answering machine characterized by comprising
UAV targets fly in ground control station before taking off and control monitoring computer transponder modules setting ADS-B OUT state
Significance bit；
The onboard flight control system of UAV targets passes to integrated response by the airborne sail information that cable will acquire
Machine system；
ADS-B module in the integrated answering machine of UAV targets by omnidirectional's dual-mode antenna be constantly sent out target without
Man-machine A code, the address S, the sail information that flight number, air pressure is high, GPS ground velocity and longitude and latitude are high；
UAV targets' boat that control tower end monitoring system is sent by the ADS-B module that omnidirectional's dual-mode antenna receives UAV targets
Row information is simultaneously shown on ADS-B monitoring computer；
Air traffic control system control tower end blank pipe personnel according to ADS-B monitor computer on sail information and voice communication apparatus to target
Unmanned plane is monitored in real time and is dispatched.
8. the ADS-B IN method of the unmanned plane monitoring system based on integrated answering machine characterized by comprising
UAV targets fly in UAV targets' ground control station before taking off and control monitoring computer transponder modules setting
ADS-B IN state significance bit；
UAV targets' ADS-B module of integrated answering machine in flight course receives other aircrafts by omnidirectional's dual-mode antenna
The A code of transmission, longitude and latitude, the sail information of air pressure height and ground velocity；
The flight information of other aircrafts is transferred to the machine of UAV targets by cable by the integrated answering machine of UAV targets
Carry flight control system；
The airborne flight control system of UAV targets is believed the navigation of other aircrafts by airborne chain-circuit system, ground surface end chain-circuit system
Breath is transferred to ground control terminal；
Operator in UAV targets' ground control terminal monitors other aircrafts and UAV targets on computer according to flight
Sail information and voice communication apparatus realize the real-time monitoring and scheduling to UAV targets jointly.
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| CN112017482A (en) * | 2019-05-28 | 2020-12-01 | 沃科波特有限公司 | Method and system for avoiding collision of aircraft with other flying objects |
| CN112165701A (en) * | 2020-10-28 | 2021-01-01 | 南京拓恒无人系统研究院有限公司 | Unmanned aerial vehicle communication response module and communication response method |
| CN112217559A (en) * | 2020-10-13 | 2021-01-12 | 中电科西北集团有限公司 | Branch unmanned aerial vehicle logistics operation and maintenance system |
| CN113744571A (en) * | 2020-05-29 | 2021-12-03 | 青岛云世纪信息科技有限公司 | Access terminal for converting unmanned aerial vehicle flight parameter information into air traffic control information format |
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| CN115209358A (en) * | 2022-07-15 | 2022-10-18 | 深圳市道通智能航空技术股份有限公司 | Method, apparatus and storage medium for transmitting auto-correlation monitoring broadcast information |
| CN115567613A (en) * | 2022-08-29 | 2023-01-03 | 西安爱生技术集团有限公司 | Encryption and decryption method for variable-word-length communication between flight control machine and airborne transponder |
| CN116778759A (en) * | 2023-08-18 | 2023-09-19 | 中航材利顿航空科技股份有限公司 | Aircraft real-time monitoring system and method |
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| CN115567613A (en) * | 2022-08-29 | 2023-01-03 | 西安爱生技术集团有限公司 | Encryption and decryption method for variable-word-length communication between flight control machine and airborne transponder |
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