CN109814105A - A kind of control system for aircraft obstruction lamps and its method based on Radar Technology - Google Patents
A kind of control system for aircraft obstruction lamps and its method based on Radar Technology Download PDFInfo
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- CN109814105A CN109814105A CN201910167380.0A CN201910167380A CN109814105A CN 109814105 A CN109814105 A CN 109814105A CN 201910167380 A CN201910167380 A CN 201910167380A CN 109814105 A CN109814105 A CN 109814105A
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- aviation obstruction
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- 238000005516 engineering process Methods 0.000 title claims abstract description 16
- 238000000034 method Methods 0.000 title claims abstract description 12
- 230000005540 biological transmission Effects 0.000 claims description 15
- 238000012545 processing Methods 0.000 claims description 15
- 238000001514 detection method Methods 0.000 claims description 6
- 238000012544 monitoring process Methods 0.000 claims description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract description 2
- 229910052799 carbon Inorganic materials 0.000 abstract description 2
- 238000005265 energy consumption Methods 0.000 abstract description 2
- 238000004891 communication Methods 0.000 description 5
- 230000004888 barrier function Effects 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 241001465382 Physalis alkekengi Species 0.000 description 2
- 238000013500 data storage Methods 0.000 description 2
- 230000004397 blinking Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
Abstract
The invention discloses a kind of control system for aircraft obstruction lamps and its method based on Radar Technology, Connectors for Active Phased Array Radar monitors low altitude airspace aircraft where high-lager building, monomer-type building group, the Aircraft position information provided using radar and the building location information marked, low flyer is calculated by controlling terminal and has been marked at a distance from building, differentiates the two distance and controls the unlatching of aviation obstruction beacon.The opening time of aviation obstruction beacon is greatly reduced, aviation obstruction beacon lighting time reduces 95%-98%, reduces light pollution, reduces energy consumption, reduces carbon emission, improves the service life of boat lamp.
Description
Technical field
The present invention relates to radar electric technical fields, and in particular to a kind of aviation obstruction beacon control system based on Radar Technology
System and its method.
Background technique
With the depth development of civil-military inosculation, low latitude resource is made full use of to have become the common recognition of society, country will gradually open
Low altitude airspace is put, low flyer such as helicopter, dirigible, unmanned plane will be widely applied, but high-lager building is to low flyer
There are major safety risks in night flying.The solution taken at present is to install aviation obstruction beacon on building top, in energy
Aviation obstruction beacon is lighted when degree of opinion is low, vectored flight object evacuation.
It is mark obstacle that aviation obstruction beacon (AviaT1ion ObsT1rucT1ion lighT1), which is also known as navigational lighting aid equipment,
The extraordinary lamps and lanterns of object, are under the jurisdiction of navigational lighting aid equipment Industry.Extraordinary lamps and lanterns of the aviation obstruction beacon as mark barrier, prevent low
Sky flight aircraft (including helicopter) high-rise is knocked in navigation at night, often work in high building, bridge, chimney,
The environment such as communication iron tower.
And these above-mentioned working environments are substantially all disposed within residential neighborhood, it is contemplated that light pollution and general purpose photograph
The difference of bright lamp, aviation obstruction beacon are not used generally and are always on, and in the prior art frequently with flashing mode, but are passed through relative to aircraft
The whole lighting time of time, aviation obstruction beacon are longer, and there are still following disadvantages: 1, night a large amount of high-intensitive aviation obstruction beacons
It lights, causes light pollution, illuminate sky, destroy dark natural environment, influence the rest of human and animal, America and Europe has prohibited
Only；2, high-intensitive aviation obstruction beacon power is big, consumes mass energy；3, prolonged blinking mode be easy to cause obstruction light
It breaks down, reduces its service life.
Summary of the invention
The problems in background in view of the above technology, it is an object of the present invention to provide a kind of aviation obstruction beacons based on Radar Technology
Control system and its method.
In order to achieve the goal above, the technical solution adopted by the present invention are as follows:
A kind of control system for aircraft obstruction lamps based on Radar Technology, including controlling terminal, radar terminal and several aviations
Obstruction light；
The controlling terminal includes data reception module, data processing module, data transmission module and data storage mould
Block, the radar terminal and controlling terminal communication connection, the aviation obstruction beacon pass through Ethernet and the controlling terminal
Communication connection；
The radar terminal is used to monitor the location information of acquisition low flyer；
The data memory module is for being stored in advance the building location information marked；
The data reception module is used to receive the Aircraft position information that the radar terminal provides, and is sent to data
Processing module；
The data processing module differentiates the two distance simultaneously for calculating low flyer and having marked at a distance from building
It is sent to data transmission module；
The data transmission module is used for the data connection established between data processing module and aviation obstruction beacon.
The control method of control system for aircraft obstruction lamps based on Radar Technology as described above, specific method include as follows
Step:
S1. the building location information A marked, geographical location, elevation information including building are acquired, and is input to
The controlling terminal, while inputting the target set point C1 of mark building and aircraft distance；
S2. the position letter of aircraft is obtained according to certain detection mode rotated detection low flyer using Radar Technology
Cease the information such as B, including geographical location, height, speed；
S3. the location information B that the data reception module receiving step S2 of controlling terminal is obtained, builds in combination with what is marked
Object location information A is built, is handled by data processing module, the distance value of mark building with the aircraft detected is obtained
C2；
S4. when the two distance C2 is less than target set point C1, data transmission module will handle signal and be sent to aviation barrier
Hinder lamp, control aviation obstruction beacon is opened；
S5. real-time update radar terminal is by the location information B of the aircraft of acquisition, when both monitoring that distance C2 is greater than mesh
When marking setting value C1, data transmission module will handle signal and be sent to aviation obstruction beacon, and control aviation obstruction beacon is closed.
Compared with prior art, the invention has the following advantages that
1, by radar surveillance low altitude airspace, when there is flying object close to high-lager building, aviation obstruction beacon is just opened, greatly
Reducing the opening time of aviation obstruction beacon greatly, aviation obstruction beacon lighting time reduces 95%-98%, reduces light pollution,
Natural ecological environment is restored；
2, the aviation obstruction beacon opening time is short, reduces energy consumption, reduces carbon emission；
3, automatic monitoring in radar 24 hours, On-line Control aviation obstruction beacon are unattended；
4, since the opening time of lamp is short, the service life of boat lamp is improved.
Detailed description of the invention
Fig. 1 is control system for aircraft obstruction lamps structural block diagram of the invention.
Specific embodiment
Below in conjunction with attached drawing, detailed description of the preferred embodiments.It should be understood that this place is retouched
The specific embodiment stated is merely to illustrate and explain the present invention, and is not intended to restrict the invention.
A kind of control system for aircraft obstruction lamps based on Radar Technology, including controlling terminal, radar terminal and several aviations
Obstruction light；
The controlling terminal includes data reception module, data processing module, data transmission module and data storage mould
Block, the radar terminal and controlling terminal communication connection, the aviation obstruction beacon pass through Ethernet and the controlling terminal
Communication connection；
The radar terminal is used to monitor the location information of acquisition low flyer；
The data memory module is for being stored in advance the building location information marked；
The data reception module is used to receive the Aircraft position information that the radar terminal provides, and is sent to data
Processing module；
The data processing module differentiates the two distance simultaneously for calculating low flyer and having marked at a distance from building
It is sent to data transmission module；
The data transmission module is used for the data connection established between data processing module and aviation obstruction beacon.
The control method of control system for aircraft obstruction lamps based on Radar Technology as described above, specific method include as follows
Step:
S1. the building location information A marked, geographical location, elevation information including building are acquired, and is input to
The controlling terminal, while inputting the target set point C1 of mark building and aircraft distance；
S2. the position letter of aircraft is obtained according to certain detection mode rotated detection low flyer using Radar Technology
Cease the information such as B, including geographical location, height, speed；
S3. the location information B that the data reception module receiving step S2 of controlling terminal is obtained, builds in combination with what is marked
Object location information A is built, is handled by data processing module, the distance value of mark building with the aircraft detected is obtained
C2；
S4. when the two distance C2 is less than target set point C1, data transmission module will handle signal and be sent to aviation barrier
Hinder lamp, control aviation obstruction beacon is opened；
S5. real-time update radar terminal is by the location information B of the aircraft of acquisition, when both monitoring that distance C2 is greater than mesh
When marking setting value C1, data transmission module will handle signal and be sent to aviation obstruction beacon, and control aviation obstruction beacon is closed.
The basic principles, main features and advantages of the present invention have been shown and described above.The technology of the industry
Personnel are it should be appreciated that the present invention is not limited to the above embodiments, and what is described in the above embodiment and the description is only the present invention
Principle, various changes and improvements may be made to the invention without departing from the spirit and scope of the present invention, these variation and
Improvement is both fallen in the range of claimed invention.The present invention claims protection scope by appended claims and its
Equivalent defines.
Claims (2)
1. a kind of control system for aircraft obstruction lamps based on Radar Technology, which is characterized in that including controlling terminal, radar terminal and
Several aviation obstruction beacons；
The controlling terminal includes data reception module, data processing module, data transmission module and data memory module, institute
State that radar terminal is communicated to connect with the controlling terminal, the aviation obstruction beacon by Ethernet communicates connection with the controlling terminal
It connects；
The radar terminal is used to monitor the location information of acquisition low flyer；
The data memory module is for being stored in advance the building location information marked；
The data reception module is used to receive the Aircraft position information that the radar terminal provides, and is sent to data processing
Module；
The data processing module is for calculating low flyer and marked at a distance from building, differentiating the two distance and sending
To data transmission module；
The data transmission module is used for the data connection established between data processing module and aviation obstruction beacon.
2. a kind of control method of the control system for aircraft obstruction lamps based on Radar Technology as described in claim 1, feature
It is, specific method includes the following steps:
S1. the building location information A marked, geographical location, elevation information including building are acquired, and is input to described
Controlling terminal, while inputting the target set point C of mark building and aircraft distance1；
S2. the location information B of aircraft is obtained according to certain detection mode rotated detection low flyer using Radar Technology,
Including information such as geographical location, height, speed；
S3. the location information B that the data reception module receiving step S2 of controlling terminal is obtained, in combination with the building marked
Location information A, is handled by data processing module, obtains the distance value C of mark building with the aircraft detected2；
S4. as the two distance C2Less than target set point C1When, data transmission module is sent to aviation obstruction beacon for signal is handled,
Aviation obstruction beacon is controlled to open；
S5. real-time update radar terminal is by the location information B of the aircraft of acquisition, when both monitoring distance C2It is set greater than target
Definite value C1When, data transmission module will handle signal and be sent to aviation obstruction beacon, and control aviation obstruction beacon is closed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910167380.0A CN109814105A (en) | 2019-03-06 | 2019-03-06 | A kind of control system for aircraft obstruction lamps and its method based on Radar Technology |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910167380.0A CN109814105A (en) | 2019-03-06 | 2019-03-06 | A kind of control system for aircraft obstruction lamps and its method based on Radar Technology |
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| CN109814105A true CN109814105A (en) | 2019-05-28 |
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| CN201910167380.0A Pending CN109814105A (en) | 2019-03-06 | 2019-03-06 | A kind of control system for aircraft obstruction lamps and its method based on Radar Technology |
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110241926A1 (en) * | 2007-07-17 | 2011-10-06 | Eric David Laufer | Method and system for reducing light pollution |
| US20120319871A1 (en) * | 2011-03-17 | 2012-12-20 | Hughey & Phillips, Llc | Lighting and Collision Alerting System |
| WO2015065253A1 (en) * | 2013-10-29 | 2015-05-07 | Saab Ab | Method and control unit for controlling one or several warning lights in a wind turbine site to minimize light pollution |
| CN207367391U (en) * | 2017-08-11 | 2018-05-15 | 唐坚 | Monitoring system for low-latitude flying |
-
2019
- 2019-03-06 CN CN201910167380.0A patent/CN109814105A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110241926A1 (en) * | 2007-07-17 | 2011-10-06 | Eric David Laufer | Method and system for reducing light pollution |
| US20120319871A1 (en) * | 2011-03-17 | 2012-12-20 | Hughey & Phillips, Llc | Lighting and Collision Alerting System |
| WO2015065253A1 (en) * | 2013-10-29 | 2015-05-07 | Saab Ab | Method and control unit for controlling one or several warning lights in a wind turbine site to minimize light pollution |
| CN207367391U (en) * | 2017-08-11 | 2018-05-15 | 唐坚 | Monitoring system for low-latitude flying |
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