CN207115778U - A kind of all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links - Google Patents

A kind of all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links Download PDF

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CN207115778U
CN207115778U CN201720448160.1U CN201720448160U CN207115778U CN 207115778 U CN207115778 U CN 207115778U CN 201720448160 U CN201720448160 U CN 201720448160U CN 207115778 U CN207115778 U CN 207115778U
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module
main control
data
links
sound
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黄伟
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Sichuan Nine Strong Communication Technology Co Ltd
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Sichuan Nine Strong Communication Technology Co Ltd
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Abstract

Aviation positioning anti-collision device field is the utility model is related to, specifically discloses a kind of all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links.The problem of aiming to solve the problem that existing beam volume excessive and causing the use range of beam to be restricted；The technical scheme that the application uses for：Radiofrequency signal is amplified and filtered including amplification module and passes to decoder module；The radiofrequency signal received is carried out Decoding Analysis and passes to main control module by decoder module；The positional information of receiving module detection aircraft simultaneously passes to main control module by USB interface；Main control module receives the information after Decoding Analysis and receiving position information and sends control signal and pass to sound-optical controller；Controlled by sound and light module sends alarm signal and passes to reminding module；Reminding module receives alarm signal and sends cue.The application product is light and handy, convenient installation, enable users at any time, anywhere, any occasion realize the seamless monitoring in round-the-clock, full spatial domain, full flight course.

Description

A kind of all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links
Technical field
Aviation beam field is the utility model is related to, it particularly relates to a kind of based on the general of 1090ES Data-Links Airborne vehicle three-dimensional collision prevention device.
Background technology
ADS-B systems (Automatic dependent surveillance broadcast system) are used as a kind of airborne equipment, realize between aircraft and aircraft , the data transfer between earth station and aircraft.Mainly include two kinds of mode of operations of 1090ES patterns and UAT patterns.1090ES Pattern mainly includes radio front end receiver, detection of preamble and decoding, Target track displaying part.ADS-B (1090ES) Data-Link Face station, by earth-space communication, receives using location information caused by airborne satellite-based navigation equipment and other airborne equipments as data source The ADS-B information of aerospace plane broadcast, the distribution of monitoring information is completed with information processing system by ground network distribution, on ground Controller's work station of face end system shows that flight track simultaneously carries out real-time tracking, realizes that traffic in spatial domain is covered to it is complete Face, detailed understanding, preferably provide traffic control service to flight.Existing beam is all based on traditional secondary radar mould Formula, equipment is complicated, and volume is big, and efficiency is low, can only adapt to existing medium-and-large-sized seating plane and use.General aviation aircraft volume Small, take-off weight is limited, and flying height is lower compared with airline carriers of passengers, requires airborne equipment small volume, in light weight, equipment is multiple Miscellaneous degree, but anticollision precision height is required, existing CAS can not meet to require.
The content of the invention
The purpose of this utility model is：For it is above-mentioned due to existing beam volume is excessive, equipment complexity High, the characteristics of cost is high and the problem of cause the use range of beam to be restricted, the utility model provides one kind and is based on The small volume of 1090ES Data-Links, all purpose aircraft three-dimensional collision prevention device that in light weight, cost is low.
The technical solution adopted in the utility model is as follows：
A kind of all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links, including：
Amplification module, the amplification of the radiofrequency signal progress radiofrequency signal of the airborne vehicle transmitting of reception and filtering process are simultaneously sent Radiofrequency signal after processing is to decoder module；
Decoder module, the radiofrequency signal that the amplification module of reception is sent carry out Decoding Analysis and send the letter after Decoding Analysis Breath is transferred to main control module；
Receiving module, detect the positional information of aircraft and sent by USB interface to main control module；
Main control module, receive the information after the Decoding Analysis that decoder module is sent and receive the position letter that receiving module is sent Cease and send a control signal to controlled by sound and light module；
Controlled by sound and light module, receive the control signal that main control module is sent and send alarm signal to reminding module；
Reminding module, receive the alarm signal that controlled by sound and light module is sent and send cue.
Specifically, reminding module includes loudspeaker and warning light.
Specifically, main control module uses computer.
Specifically, amplification module uses radiofrequency signal low-noise amplifier JZ-JQLNA2017-1090.
Specifically, decoder module uses MMIC- using 1090ES decoding processors JZ-JQ201711, JZ-JQ201711 JZJQ1090v1 chips and JD-JZJQ1090V2.1 chips are an integrally designed.
Specifically, receiving module uses BD/GPS signal receiving and decoding devices YD-220-IIIN.
The application relies on the data-signal of 1090ES data link interface Auto broadcast dependent surveillances to send and receive mode, Around obtaining on the basis of the position of civil aviaton, navigation and professional unmanned plane, comprehensive national electronic map realizes that orderly three-dimensional is prevented Hit.
The beam mainly minimizes industrial computer, radiofrequency signal low-noise amplifier, miniaturization integration by low-power consumption 1090ES decoder modules (decoding signals), receiving module (BD/GPS signal receiving and decodings module), sound-optical controller, prompting Module (loudspeaker and warning light) is formed, and main control module (low-power consumption miniaturization industrial computer) is by USB interface with 1090ES signals Decoder, BD/GPS signal receiving and decodings module, sound-optical controller are connected with each other, and sound-optical controller passes through audio frequency and lamp control cable Formed with prompting loudspeaker and warning light.Low-power consumption minimizes industrial computer expert and crosses the last nine general boat of the loading containing national electronic map Pocket beam software realizes all purpose aircraft anticollision prompting, aerial Situation Awareness and display, collision avoidance prompting and display, collision avoidance road Whether line correctly prompts.
Radiofrequency signal low-noise amplifier mainly completes the amplification and filtering of 1090MHz radiofrequency signals, 1090ES signal solutions The MMIC-JZJQ1090v1 chips and the last nine communication JD-JZJQ1090V2.1 chips that code module is then mainly communicated using the last nine The integrated 1090ES decoding process modules JZ-JQ201711 of design realizes the decoding and data point to 1090ES Data-Link data Analysis, and by USB port upload DF-17 18 data in industrial computer.BD/GPS signal receiving and decoding modules mainly use The YD-220-IIIN Big Dipper meets the positioning that GPS process chips realize common aero vehicle self-position, and data are uploaded To industrial computer.By realizing 4th area (detecting area, precautionary areas, announcement with the last nine all purpose aircraft anticollision software in industrial computer Police region, collision avoidance area) separate and handle.Industrial computer after processing is completed, will be accused by USB interface signal and audio output signal Alert information transmission controls loudspeaker and Optical Implementation acousto-optic hint and alarm to sound-optical controller by sound-optical controller.
In summary, by adopting the above-described technical solution, the beneficial effects of the utility model are：
1. the application is decoded simultaneously using integrated JZ-JQ201711 integrations 1090ES processing modules implement 1090ES data DF-17/18 data are reported to industrial computer by USB interface, then by sending alarm signal after processing, and control at acousto-optic Reason device responds, and acoustooptic processor controls loudspeaker and prompting to carry out alarm and corresponding prompting to the situation of aircraft again, keeps away Exempt from plane collision；The application realizes effective aviation monitoring in the range of the operating distance of beam, meets navigation user to handing over The demand of on-state gesture monitoring.The application product is light and handy, convenient installation, enable users at any time, anywhere, any occasion Realize the anticollision monitoring in round-the-clock, full spatial domain, full flight course.It is easy to maintenance, it is simple to operate.
2. radio frequency signal amplifiers are realized by the way of low noise amplification+SAW mini filters, using miniaturization And integrated design, while 5 digit control attenuation modules are added so as to reach guarantee signal for guarantee system overall dynamic range The problem of amplifying and taking into account dynamic range.
3. decoder module using integrated chip realize decoding, it is low in energy consumption, stability is good, small volume the characteristics of, the chip Possess integrated radio-frequency sampling, digital lower side frequency and data processing function, what the chip was be combined with each other using MMIC and SOP technologies Single 1090ES process chips.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art In the required accompanying drawing used be briefly described, it should be apparent that, drawings in the following description are only of the present utility model Some embodiments, for those of ordinary skill in the art, on the premise of not paying creative work, can also be according to this A little accompanying drawings obtain other accompanying drawings.By shown in accompanying drawing, above and other purpose of the present utility model, feature and advantage will more Clearly.The identical reference instruction identical part in whole accompanying drawings.Do not painted by actual size equal proportion scaling deliberately Accompanying drawing processed, it is preferred that emphasis is show purport of the present utility model.
Fig. 1 is the structure chart of the utility model airborne vehicle beam；
Fig. 2 is the concrete structure diagram of the utility model airborne vehicle beam；
Marked in figure：1- amplification modules；2- decoder modules；3- receiving modules；4- main control modules；5- controlled by sound and light modules； 6- reminding modules；1-1- radiofrequency signal low-noise amplifiers JZ-JQLNA2017-1090；2-1-1090ES decoding processors JZ- JQ201711；3-1-BD/GPS signal receiving and decoding devices YD-220-IIIN；4-1- minimizes industrial computer；5-1- controlled by sound and light Device；6-1- loudspeaker warning lights.
Embodiment
It is new below in conjunction with this practicality to make the purpose, technical scheme and advantage of the utility model embodiment clearer Accompanying drawing in type embodiment, the technical scheme in the embodiment of the utility model is clearly and completely described, it is clear that is retouched The embodiment stated is the utility model part of the embodiment, rather than whole embodiments.Generally here described in accompanying drawing and The component of the utility model embodiment shown can be configured to arrange and design with a variety of.
Therefore, the detailed description of the embodiment of the present utility model to providing in the accompanying drawings is not intended to limit requirement below The scope of the utility model of protection, but it is merely representative of selected embodiment of the present utility model.Based in the utility model Embodiment, the every other embodiment that those of ordinary skill in the art are obtained under the premise of creative work is not made, all Belong to the scope of the utility model protection.
It should be noted that：Similar label and letter represents similar terms in following accompanying drawing, therefore, once a certain Xiang Yi It is defined, then it further need not be defined and explained in subsequent accompanying drawing in individual accompanying drawing.
The application essentially discloses a kind of miniaturization, and the wide all purpose aircraft based on 1090ES Data-Links of use range is prevented Device is hit, in order to further illustrate present context, teachings herein will be combined and carry out detailed explanation.
The present invention is elaborated with reference to Fig. 1, Fig. 2.
Embodiment one
A kind of all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links, it is characterised in that including：
Amplification module 1, the amplification of the radiofrequency signal progress radiofrequency signal of the airborne vehicle transmitting of reception and filtering process are concurrent The radiofrequency signal after processing is sent to decoder module 2；
Decoder module 2, after the radiofrequency signal that the amplification module of reception is sent carries out Decoding Analysis and sends Decoding Analysis Information transmission is to main control module 4；
Receiving module 3, detect the positional information of aircraft and sent by USB interface to main control module 4；
Main control module 4, receive the information after the Decoding Analysis that decoder module 2 is sent and receive the position that receiving module 3 is sent Confidence ceases and sends a control signal to controlled by sound and light module 5；
Controlled by sound and light module 5, receive the control signal that main control module is sent and send alarm signal to reminding module；
Reminding module 6, receive the alarm signal that controlled by sound and light module 5 is sent and send cue.
Embodiment two
On the basis of all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links of embodiment one, amplification module 1 Using radiofrequency signal low-noise amplifier JZ-JQLNA2017-1090；Decoder module 2 is using 1090ES decoding process Device JZ-JQ201711；Receiving module 3 is using BD/GPS signal receiving and decoding devices YD-220-IIIN；Main control module 4 is using small-sized Chemical industry computer；Controlled by sound and light module 5 directly uses sound-optical controller 5-1；Reminding module 6 uses and is based on sound-optical controller 5-1 The loudspeaker and warning light of control.
Beam mainly minimizes industrial computer, radiofrequency signal low-noise amplifier, miniaturization integration by low-power consumption 1090ES decoder modules (decoding signals), receiving module (BD/GPS signal receiving and decodings module), sound-optical controller, prompting Module (loudspeaker and warning light) is formed, and main control module (low-power consumption miniaturization industrial computer) is by USB interface with 1090ES signals Decoder, BD/GPS signal receiving and decodings module, sound-optical controller are connected with each other, and sound-optical controller passes through audio frequency and lamp control cable Formed with prompting loudspeaker and warning light.Low-power consumption minimizes industrial computer expert and crosses the last nine general boat of the loading containing national electronic map Pocket beam software realizes all purpose aircraft anticollision prompting, aerial Situation Awareness and display, collision avoidance prompting and display, collision avoidance road Whether line correctly prompts.
Radiofrequency signal low-noise amplifier mainly completes the amplification and filtering of 1090MHz radiofrequency signals, 1090ES signal solutions The MMIC-JZJQ1090v1 chips and the last nine communication JD-JZJQ1090V2.1 chips that code module is then mainly communicated using the last nine The integrated 1090ES decoding process modules JZ-JQ201711 of design realizes the decoding and data point to 1090ES Data-Link data Analysis, and by USB port upload DF-17 18 data in industrial computer.BD/GPS signal receiving and decoding modules mainly use The YD-220-IIIN Big Dipper meets the positioning that GPS process chips realize common aero vehicle self-position, and data are uploaded To industrial computer.By realizing 4th area (detecting area, precautionary areas, announcement with the last nine all purpose aircraft anticollision software in industrial computer Police region, collision avoidance area) separate and handle.Industrial computer after processing is completed, will be accused by USB interface signal and audio output signal Alert information transmission controls loudspeaker and Optical Implementation acousto-optic hint and alarm to sound-optical controller by sound-optical controller.

Claims (6)

  1. A kind of 1. all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links, it is characterised in that including：
    Amplification module (1), the amplification of the radiofrequency signal progress radiofrequency signal of the airborne vehicle transmitting of reception and filtering process are simultaneously sent Radiofrequency signal after processing is to decoder module (2)；
    Decoder module (2), the radiofrequency signal that the amplification module of reception is sent carry out Decoding Analysis and send the letter after Decoding Analysis Breath is transferred to main control module (4)；
    Receiving module (3), detect the positional information of aircraft and sent by USB interface to main control module (4)；
    Main control module (4), receive the information after the Decoding Analysis that decoder module (2) is sent and receive what receiving module (3) was sent Positional information simultaneously sends a control signal to controlled by sound and light module (5)；
    Controlled by sound and light module (5), receive the control signal that main control module is sent and send alarm signal to reminding module；
    Reminding module (6), receive the alarm signal that controlled by sound and light module (5) is sent and send cue；
    Controlled by sound and light module and reminding module are used with main control module integrated design.
  2. A kind of 2. all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links as claimed in claim 1, it is characterised in that Reminding module (6) includes loudspeaker and warning light uses integrated design with main control module.
  3. A kind of 3. all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links as claimed in claim 1, it is characterised in that Main control module (4) is using miniaturization computer.
  4. A kind of 4. all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links as claimed in claim 1, it is characterised in that Amplification module (1) uses radiofrequency signal low-noise amplifier JZ-JQLNA2017-1090 (1-1).
  5. A kind of 5. all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links as claimed in claim 1, it is characterised in that Decoder module (2) uses 1090ES decoding processors JZ-JQ201711 (2-1).
  6. A kind of 6. all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links as claimed in claim 1, it is characterised in that Receiving module uses BD/GPS signal receiving and decoding device YD-220-IIIN (3-1).
CN201720448160.1U 2017-04-26 2017-04-26 A kind of all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links Active CN207115778U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720448160.1U CN207115778U (en) 2017-04-26 2017-04-26 A kind of all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720448160.1U CN207115778U (en) 2017-04-26 2017-04-26 A kind of all purpose aircraft three-dimensional collision prevention device based on 1090ES Data-Links

Publications (1)

Publication Number Publication Date
CN207115778U true CN207115778U (en) 2018-03-16

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Country Status (1)

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