CN109541711A - It is a kind of based on staring infrared unmanned plane warning system and method - Google Patents
It is a kind of based on staring infrared unmanned plane warning system and method Download PDFInfo
- Publication number
- CN109541711A CN109541711A CN201811358052.0A CN201811358052A CN109541711A CN 109541711 A CN109541711 A CN 109541711A CN 201811358052 A CN201811358052 A CN 201811358052A CN 109541711 A CN109541711 A CN 109541711A
- Authority
- CN
- China
- Prior art keywords
- unit
- unmanned plane
- information conversion
- processing unit
- signal processing
- 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.)
- Pending
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
- G01V8/00—Prospecting or detecting by optical means
- G01V8/10—Detecting, e.g. by using light barriers
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/03—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Life Sciences & Earth Sciences (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geophysics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Transforming Light Signals Into Electric Signals (AREA)
- Photometry And Measurement Of Optical Pulse Characteristics (AREA)
- Closed-Circuit Television Systems (AREA)
Abstract
The invention discloses a kind of based on staring infrared unmanned plane warning system and method, this method comprises: the instruction of the aobvious control computer (9) of servo control unit (4) receipt signal processing unit forwarding, control the rotation of two axis servo mechanisms (6), compensation thermal infrared imager (1) is stared to 360 ° of scene panoramic imageries, pass through the first photoelectric information conversion unit (2), second photoelectric information conversion unit (7) and signal processing unit (8) send data to aobvious control computer (9), pass through Panoramagram montage, panoramic picture is shown on aobvious control interface, object detection information aobvious control computer (9) is sent to by signal processing unit (8) simultaneously to be shown on control interface, form the round-the-clock real-time unmanned plane warning system of a complete closed loop.Present system connection relationship is simple and reliable, easy to maintenance, has excellent performance.
Description
Technical field
It is especially a kind of based on staring infrared unmanned plane alarm the present invention relates to a kind of unmanned plane warning system and method
System and method.
Background technique
In recent years, unmanned plane market rapidly increases, take photo by plane, survey and draw, delivery, the every field such as rescue play effect.
But following there are also " trouble ", unmanned plane " black to fly " often occurs, and influences flight normal flight, upsets public safety, danger
Evil military security.Anti- unmanned plane demand is increasingly strong, and countries in the world all are stepping up to formulate and release anti-unmanned plane strategy.Due to more
Unmanned plane size is small, and mostly flies under complex environment for number " black to fly ", and radar is not easy detection and vulnerable to interference, therefore based on solidifying
It comes into being depending on infrared unmanned plane warning system.Not only need realization to nobody based on infrared unmanned plane warning system is stared
The alarm of machine will also be presented 360 ° of panorama clear images for manually participating in improving accuracy rate, therefore also panoramic picture be needed to spell
Connection function.
Summary of the invention
The purpose of the present invention is to provide a kind of based on infrared unmanned plane warning system and method is stared, and solves radar not
Easily detection, vulnerable to interference the problem of.
Based on above-mentioned technical problem, the present invention proposes a kind of based on staring infrared unmanned plane warning system, comprising: stares
Compensate thermal infrared imager, the first photoelectric information conversion unit, GPS positioning time service module, servo control unit, power supply unit, two
Axis servo mechanism, the second photoelectric information conversion unit, signal processing unit and aobvious control computer.
Wherein, compensation thermal infrared imager, photoelectric information conversion unit, GPS positioning time service module, SERVO CONTROL list are stared
Member, power supply unit are mounted in two axis servo mechanisms, and servo control unit controls 360 ° of two axis servo mechanisms continuous turnovers, are formed
Infrared reconnaissance and detection subsystem, photoelectric information conversion module will stare compensation thermal infrared imager shooting infrared digital image,
The information of communication instruction and GPS positioning time service module is converted to optical signal by electric signal and is transmitted；Power supply unit is given respectively
It states each unit and power input is provided；
Photoelectric information conversion unit, signal processing unit form portable aobvious control point together with aobvious control Automated library system
System；The optical signal that photoelectric information conversion module will be received from the photoelectric information conversion module of infrared reconnaissance and detection subsystem
Be converted to electric signal, after signal processing unit receives various data, complete data analysis and image procossing, will treated figure
As and data computer is sent to by network interface, control interface display by computer is aobvious.
The present invention also proposes a kind of based on staring infrared unmanned plane alarm method, it is characterised in that specific steps are as follows:
Infrared reconnaissance and detection subsystem are placed on spacious place or eminence by the first step, are connect with portable display & control system；
System electrification, computer booting, into aobvious control interface；
Time and location information are passed through into the first light by communication interface after the completion of the positioning of second step GPS positioning time service module
Power information converting unit, the second photoelectric information conversion unit and signal processing unit are sent to aobvious control interface and are shown, simultaneously
The second synchronization signal of GPS positioning time service module output, which is sent to, stares compensation thermal infrared imager；
The aobvious control computer of third step control sends " search imaging " instruction, the signal processing unit processes instruction:
A) 360 ° of two axis servo mechanisms continuous turnovers are controlled by servo control unit；
B) starting of compensation thermal infrared imager " search imaging " mode is stared, when controlling exposure starting according to second synchronization signal
It carves, the time for exposure is controlled according to instruction, is completed to 360 ° of panoramic imageries；
4th step photoelectric information conversion module forwards picture signal increases to signal processing unit by target detection and image
After strong display processing, scene image and unmanned plane target warning information are issued into aobvious control computer by network interface, show control computer
Panorama Mosaic is completed, and warning information is labeled, is shown on control interface.
It is of the invention to be disturbed small with all weather operations based on staring infrared unmanned plane warning system, and there is panorama
Image is presented in real time, participates in improving accuracy rate convenient for artificial, will have very wide application prospect in anti-unmanned plane field.
Detailed description of the invention
Fig. 1 is that the present invention is based on the communication link map interlinkings for staring infrared unmanned plane warning system.
1. staring compensation 2. first photoelectric conversion information unit 3.GPS of thermal infrared imager positioning 4. servo of time service module
Control unit
5. the aobvious control meter of 6. liang of 7. photoelectric information conversion unit of axis servo mechanism, 8. signal processing units 9. of power supply unit
Calculation machine
Specific embodiment
Below in conjunction with Fig. 1, description of specific embodiments of the present invention.
Embodiment 1
The present invention proposes a kind of based on staring infrared unmanned plane warning system comprising: stare compensation thermal infrared imager
1, the first photoelectric information conversion unit 2, GPS positioning time service module 3, servo control unit 4, power supply unit 5, two axis servo mechanisms
6, photoelectric information conversion unit 7, signal processing unit 8 and aobvious control computer 9.
Wherein stare compensation thermal infrared imager 1, the first photoelectric information conversion unit 2, GPS positioning time service module 3, servo control
Unit 4 processed, power supply unit 5 are mounted in two axis servo mechanisms 6, and servo control unit (4) controls two axis servo mechanisms, 360 ° of companies
Continuous turnover forms infrared reconnaissance and detection subsystem, stares the Cameralink infrared digital figure that compensation thermal infrared imager 1 is shot
The information of picture, RS422 communication instruction and GPS positioning time service module 3 is converted electrical signals to by the first photoelectric information conversion module 2
Optical signal is transmitted；It is fixed that power supply unit 5 respectively stares compensation thermal infrared imager 1, the first photoelectric information conversion unit 2, GPS
Position time service module 3, servo control unit 4 provide power input.
Second photoelectric information conversion unit 7, signal processing unit 8 and aobvious control computer 9 integrate, and are formed portable
The optical signal received is converted to electric signal by aobvious control subsystem, the second photoelectric information conversion unit 7, and signal processing unit 8 connects
After receiving various data, data analysis and image procossing are completed, treated image and data by network interface are sent to calculating
Machine, by the aobvious control interface display of computer.
Embodiment 2
It is a kind of based on staring infrared unmanned plane alarm method, it is characterised in that specific steps are as follows:
Infrared reconnaissance and detection subsystem are placed on spacious place or eminence by the first step, are connect with portable display & control system；
System electrification, computer booting, into aobvious control interface；
Time and location information are passed through RS232 interface after the completion of positioning and pass through first by second step GPS positioning time service module 3
Photoelectric information conversion unit 2, the second photoelectric information conversion unit 7 and signal processing unit 8 are sent to aobvious control interface and are shown,
The second synchronization signal of GPS positioning time service module output simultaneously, which is sent to, stares compensation thermal infrared imager 1；
The aobvious control computer 9 of third step control sends " search imaging " instruction, and signal processing unit 8 handles the instruction:
A) 360 ° of two axis servo mechanisms continuous turnovers are controlled by servo control unit 4；
B) starting of compensation thermal infrared imager 1 " search imaging " mode is stared, when controlling exposure starting according to second synchronization signal
It carves, the time for exposure is controlled according to instruction, is completed to 360 ° of panoramic imageries；
4th the second photoelectric information conversion of step unit 7 forwards picture signal to signal processing unit 8, by target detection and
After image enhancement display processing, scene image and unmanned plane target warning information are issued into aobvious control computer by network interface, show control
Computer completes Panorama Mosaic, and warning information is labeled, and is shown on control interface.
So far, the alarm of unmanned plane target is realized.
It is of the invention to be disturbed small with all weather operations based on staring infrared unmanned plane warning system, and there is panorama
Image is presented in real time, participates in improving accuracy rate convenient for artificial, will have very wide application prospect in anti-unmanned plane field.
Claims (5)
1. a kind of based on staring infrared unmanned plane warning system, characterized in that it comprises: stare compensation thermal infrared imager
(1), the first photoelectric information conversion unit (2), GPS positioning time service module (3), servo control unit (4), power supply unit (5), two
Axis servo mechanism (6), the second photoelectric information conversion unit (7), signal processing unit (8) and aobvious control computer (9)；
Wherein, it stares compensation thermal infrared imager (1), the first photoelectric information conversion unit (2), GPS positioning time service module (3), watch
Take control unit (4), power supply unit (5) is mounted in two axis servo mechanisms (6), servo control unit (4) two axis servos of control
The continuous turnover of (6) 360 ° of mechanism, forms infrared reconnaissance and detection subsystem,
Photoelectric information conversion module (2) will stare compensation thermal infrared imager (1) shooting infrared digital image, communication instruction and
The information of GPS positioning time service module (3) is transmitted after being converted to optical signal by electric signal；
Power supply unit (5) provides power input to above-mentioned each unit respectively；
Photoelectric information conversion unit (9), signal processing unit (8) and aobvious control computer (10) integrate, and are formed portable
Aobvious control subsystem, photoelectric information conversion module (7) will connect from infrared reconnaissance and the photoelectric information conversion module (2) of detection subsystem
The optical signal received is converted to electric signal, after signal processing unit (8) receives various data, completes at data analysis and image
Treated image and data by network interface are sent to computer (9), show control computer (9) completion Panorama Mosaic by reason,
And be labeled warning information, by the aobvious control interface display of computer.
2. unmanned plane warning system according to claim 1, which is characterized in that described to stare compensation thermal infrared imager (1)
Captured infrared digital image is Cameralink infrared digital image.
3. unmanned plane warning system according to claim 1, which is characterized in that the communication instruction is that RS422 communication refers to
It enables.
4. a kind of based on staring infrared unmanned plane alarm method, which is characterized in that the steps include:
Infrared reconnaissance is connect by the first step with detection subsystem with portable display & control system；System electrification, computer (9) booting,
Into aobvious control interface；
Time and location information are passed through the first light by communication interface after the completion of GPS positioning time service module (3) positioning by second step
Power information converting unit (2), the second photoelectric information conversion unit (7) and signal processing unit (8) are sent to aobvious control interface and carry out
It has been shown that, while the second synchronization signal of GPS positioning time service module (3) output is sent to and stares compensation thermal infrared imager (1)；
Third step controls aobvious control computer (9) and sends " search imaging " instruction, and signal processing unit (8) handles the instruction:
A) 360 ° of two axis servo mechanisms continuous turnovers are controlled by servo control unit (4)；
B) compensation thermal infrared imager (1) starting " search imaging " mode is stared, exposure initial time is controlled according to second synchronization signal,
The time for exposure is controlled according to instruction, is completed to 360 ° of panoramic imageries；
4th step, through the first photoelectric information conversion module (2), the second photoelectric information conversion module (7) forwarding picture signal to letter
Number processing unit (8), after target detection and image enhancement display processing, by scene image and unmanned plane target warning information
Aobvious control computer (9) is issued by network interface, control computer (9) is shown and completes Panorama Mosaic, and warning information is labeled,
It is shown on control interface.
5. unmanned plane alarm method according to claim 4, which is characterized in that the communication interface is that RS232 communication connects
Mouthful.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811358052.0A CN109541711A (en) | 2018-11-15 | 2018-11-15 | It is a kind of based on staring infrared unmanned plane warning system and method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811358052.0A CN109541711A (en) | 2018-11-15 | 2018-11-15 | It is a kind of based on staring infrared unmanned plane warning system and method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109541711A true CN109541711A (en) | 2019-03-29 |
Family
ID=65847603
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811358052.0A Pending CN109541711A (en) | 2018-11-15 | 2018-11-15 | It is a kind of based on staring infrared unmanned plane warning system and method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109541711A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202018341U (en) * | 2011-03-11 | 2011-10-26 | 赵进豪 | Target scene-based staring thermal imager correcting mechanism |
| US9164515B1 (en) * | 2010-03-17 | 2015-10-20 | The United States Of America As Represented By The Secretary Of The Navy | Navigating in GPS denied environments using a dedicated aerial vehicle |
| EP2937798A1 (en) * | 2013-10-28 | 2015-10-28 | Korea Aerospace Research Institute | System for analyzing risk of collision based on csm |
| CN204895880U (en) * | 2015-08-27 | 2015-12-23 | 中国农业科学院农业资源与农业区划研究所 | Unmanned aerial vehicle carries location and shoots device |
| CN105763851A (en) * | 2016-04-05 | 2016-07-13 | 赣州市金电电子设备有限公司 | Forest fire prevention video monitoring and early warning system based on electronic government affair network platform |
| CN106370309A (en) * | 2016-11-07 | 2017-02-01 | 上海资誉电子科技有限公司 | Low-level small target infrared search system |
| CN108010065A (en) * | 2017-11-07 | 2018-05-08 | 西安天和防务技术股份有限公司 | Low target quick determination method and device, storage medium and electric terminal |
| CN108614273A (en) * | 2016-12-09 | 2018-10-02 | 中国人民解放军92232部队 | A kind of airborne two waveband photoelectricity wide area is scouted and tracks of device and method |
-
2018
- 2018-11-15 CN CN201811358052.0A patent/CN109541711A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9164515B1 (en) * | 2010-03-17 | 2015-10-20 | The United States Of America As Represented By The Secretary Of The Navy | Navigating in GPS denied environments using a dedicated aerial vehicle |
| CN202018341U (en) * | 2011-03-11 | 2011-10-26 | 赵进豪 | Target scene-based staring thermal imager correcting mechanism |
| EP2937798A1 (en) * | 2013-10-28 | 2015-10-28 | Korea Aerospace Research Institute | System for analyzing risk of collision based on csm |
| CN204895880U (en) * | 2015-08-27 | 2015-12-23 | 中国农业科学院农业资源与农业区划研究所 | Unmanned aerial vehicle carries location and shoots device |
| CN105763851A (en) * | 2016-04-05 | 2016-07-13 | 赣州市金电电子设备有限公司 | Forest fire prevention video monitoring and early warning system based on electronic government affair network platform |
| CN106370309A (en) * | 2016-11-07 | 2017-02-01 | 上海资誉电子科技有限公司 | Low-level small target infrared search system |
| CN108614273A (en) * | 2016-12-09 | 2018-10-02 | 中国人民解放军92232部队 | A kind of airborne two waveband photoelectricity wide area is scouted and tracks of device and method |
| CN108010065A (en) * | 2017-11-07 | 2018-05-08 | 西安天和防务技术股份有限公司 | Low target quick determination method and device, storage medium and electric terminal |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11869234B2 (en) | Subject tracking systems for a movable imaging system | |
| US11039086B2 (en) | Dual lens system having a light splitter | |
| Leininger et al. | Autonomous real-time ground ubiquitous surveillance-imaging system (ARGUS-IS) | |
| CN202043246U (en) | Remote data collector for fixed wing unmanned plane line inspection | |
| EP2867873B1 (en) | Surveillance process and apparatus | |
| Marks et al. | Characterization of the AWARE 10 two-gigapixel wide-field-of-view visible imager | |
| CN102480615A (en) | Image target area tracking system and method and computer program product | |
| CN102866480B (en) | Large view field optical imaging system based on computing imaging technology | |
| CN210526874U (en) | Airborne three-light photoelectric pod system | |
| US20140049654A1 (en) | Information providing system, information providing device, image capture device, and computer program | |
| CN105959519A (en) | Ship-borne acoustic-optic-electric three-in-one law enforcement evidence-obtaining system | |
| CN113890977B (en) | Airborne video processing device and unmanned aerial vehicle with same | |
| CN114554093B (en) | Image acquisition system and target tracking method | |
| JP6482855B2 (en) | Monitoring system | |
| CN102291568A (en) | Accelerated processing method of large-view-field intelligent video monitoring system | |
| CN103002249A (en) | Image splicing based SDI (serial digital interface) panorama pickup system | |
| CN104580895A (en) | Airborne imaging system with synchronous camera shooting and photographing capacity | |
| CN100562102C (en) | Be used to catch the wide field's image and the method and system of area-of-interest wherein | |
| Minwalla et al. | Experimental evaluation of PICAS: An electro-optical array for non-cooperative collision sensing on unmanned aircraft systems | |
| CN109541711A (en) | It is a kind of based on staring infrared unmanned plane warning system and method | |
| CN108108396A (en) | A kind of aircraft take photo by plane picture splicing management system | |
| CN105323540A (en) | Intelligent control four-axis aircraft with multiple cameras | |
| US20190378400A1 (en) | Method and apparatus for gathering visual data using an augmented-reality application | |
| CN106156764B (en) | Realize the optical tracking system and its control method of high speed tracking | |
| CN205356525U (en) | Unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190329 |
|
| WD01 | Invention patent application deemed withdrawn after publication |