CN105371701B - television guidance seeker dynamic simulator - Google Patents
television guidance seeker dynamic simulator Download PDFInfo
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- CN105371701B CN105371701B CN201510865865.9A CN201510865865A CN105371701B CN 105371701 B CN105371701 B CN 105371701B CN 201510865865 A CN201510865865 A CN 201510865865A CN 105371701 B CN105371701 B CN 105371701B
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- guidance
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- azimuth
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Abstract
The invention relates to a television guidance seeker dynamic simulator, and belongs to the technical field of optoelectronics applications. The television guidance seeker dynamic simulator simulates an acquisition and tracking technology of an air-to-ground television guidance weapon to a target, and simulates an air angle maneuvering process of the air-to-ground television guidance weapon relative to the target. The television guidance seeker dynamic simulator comprises a rotary table, a television tracker, an image guidance processor and a comprehensive control computer, wherein the rotary table consists of a sliding block, a sliding seat, a pitching motor, perpendicular shafts, a machine base and an azimuth motor tachometer unit; a simulation video output port of the television tracker is connected with a video input port of the image guidance processor; the pitching motor, the azimuth motor and a tachometer are connected with the image guidance processor; the image guidance processor is connected with the comprehensive control computer mutually; and a video output port of the image guidance processor is connected with a simulation video input port of the comprehensive control computer.
Description
Technical field
The invention belongs to photovoltaic applications technical field, it is related to a kind of TV guidance target seeker kinetic-simulator.
Background technology
With the extensive application of TV precision guided weapon, using the TV sensor to TV precision guided weapon for the laser
The technology disturbed is arisen at the historic moment；At present, in order to test these Laser interferometers systems, mostly adopt domestic television weapon
The mode of throw-off practice, but costly；And, Laser interferometers system is generally laid in by near attack area, therefore live shell inspection
Test the safety of serious threat personnel and equipment.Therefore, researching and developing a kind of TV guidance target seeker kinetic-simulator has become this area
Technical staff's problem demanding prompt solution.
Content of the invention
In order to overcome the above-mentioned deficiencies of the prior art, the invention provides a kind of TV guidance target seeker kinetic-simulator,
This simulator can simulate the acquisition and tracking technology to target for the Air-Ground television weapon, simulates Air-Ground television weapon phase
Aerial angle mobile process to target.
To achieve these goals, the technical solution adopted in the present invention is: a kind of TV guidance target seeker dynamic analog
Device, including turntable, television tracking device, image guidance datatron and Comprehensive control computer；Described turntable by slide block, slide,
Pitching motor, vertical axises, support and azimuth-drive motor test the speed unit composition, be provided with the slideway of arc, slide block in the top surface of slide
Match with slideway, pitching motor is fixed on slide, the bottom of slide is fixed on the top of vertical axises, vertical axises and orientation electricity
The machine unit that tests the speed is arranged in support, and the test the speed inner flange of unit of vertical axises and azimuth-drive motor is fixedly and coaxially connected；Described electricity
It is fixed on slide block depending on tracker, the video input mouth phase of the analog video delivery outlet of television tracking device and image guidance datatron
Even, the first input port of pitching motor is connected with the first delivery outlet of image guidance datatron, and azimuth-drive motor tests the speed in unit just
Position the second input port of motor is connected with the second delivery outlet of image guidance datatron, and azimuth-drive motor tests the speed tachometer in unit
3rd delivery outlet is connected with the 3rd input port of image guidance datatron, and the first communication port of image guidance datatron is controlled with comprehensive
Second communication port interconnection, the video output of image guidance datatron and the analog video of Comprehensive control computer of computer processed
Input port is connected.
Described vertical axises are connected with support by bearing.
Described vertical axises are arranged on azimuth-drive motor and test the speed the top of unit.
Be fixed with limited block at the top of described support, be fixed with gag lever post in the bottom of slide, gag lever post with spacing
Block matches.
Described television tracking device is fixed on the top surface of slide block by equipment connecting plate.
The bottom of described slide is fixed on the top of vertical axises by orientation connecting plate.
Beneficial effects of the present invention:
The TV guidance target seeker kinetic-simulator of the present invention, can simulate the process of precision guided weapon lock onto target,
And there is dynamic collimation function, can be in the attack overall process of the dynamic lock onto target of ground simulation Air-Ground television weapon.
Brief description
Fig. 1 is the circuit theory diagrams of the TV guidance target seeker kinetic-simulator of the present invention；
Fig. 2 is the work process flow chart of the TV guidance target seeker kinetic-simulator of the present invention；
Fig. 3 is the structural representation of the turntable of the present invention；
The image of display on the display of Comprehensive control computer when Fig. 4 is initially directed at cooperative target for the present invention；
The image of display on the display of Comprehensive control computer when Fig. 5 locks cooperative target for the present invention；
Fig. 6 be turntable from after motion tracking cooperative target, the present invention is when relocking cooperative target, Comprehensive control computer
The image of display on display；
When Fig. 7 is for disturbing after laser unlatching, the present invention departs from cooperative target, the display of Comprehensive control computer shows
Image；
When Fig. 8 rotates for turntable, cooperative target departs from television tracking device visual field, aobvious on the display of Comprehensive control computer
The image showing；
The image of display on the display of Comprehensive control computer when Fig. 9 loses for cooperative target；
Figure 10 be the present invention during the jamming effectiveness of testing laser jamming equipment, turntable action schematic diagram；
In figure, 1 TV guidance target seeker kinetic-simulator, 2 turntables, 21 equipment connecting plates, 22 slides,
23 limited blocks, 24 vertical axises, 25 bearings, 26 supports, 27 orientation connecting plates, 28 slide blocks, 29 gag lever posts,
3 television tracking devices, 31 analog video delivery outlets, 4 image guidance datatrons, 41 first communication ports, 42 first is defeated
Outlet, 43 second delivery outlets, 44 the 3rd input ports, 45 video input mouths, 46 video outputs, 5 Comprehensive Control
Computer, 51 second communication ports, 52 analog video input ports, 6 cooperative targets, 7 Laser interferometers equipment；8 orientation
Motor speed measuring unit, 81 azimuth-drive motors, 811 second input ports, 82 tachometers, 821 the 3rd delivery outlets, 9 pitching
Motor, 91 first input ports.
Specific embodiment
The present invention is described in further detail with specific embodiment below in conjunction with the accompanying drawings.
As shown in Figure 1, Figure 3, a kind of TV guidance target seeker kinetic-simulator 1, including turntable 2, television tracking device 3, figure
As guidance datatron 4 and Comprehensive control computer 5；Described turntable 2 by slide block 28, slide 22, pitching motor 9, vertical axises 24,
The support 26 and azimuth-drive motor unit 8 that tests the speed forms, and is provided with the slideway of arc in the top surface of slide 22, slide block 28 and slideway match
Close, form the angle change of pitch orientation, pitching motor 9 is fixed on the sidepiece of slide 22, and the bottom of slide 22 is fixed on vertically
The top of axle 24, the vertical axises 24 and azimuth-drive motor unit 8 that tests the speed is arranged in support 26, vertical axises 24 and azimuth-drive motor tachometer
The inner flange of group 8 is fixedly and coaxially connected；
Described television tracking device 3 is fixed on slide block 28, analog video delivery outlet 31 and the image system of television tracking device 3
The video input mouth 45 leading datatron 4 is connected, and the first input port 91 of pitching motor 9 is defeated with the first of image guidance datatron 4
Outlet 42 is connected, and azimuth-drive motor tests the speed the of the second input port 811 of azimuth-drive motor 81 and image guidance datatron 4 in unit 8
Two delivery outlets 43 are connected, and azimuth-drive motor tests the speed the 3rd delivery outlet 821 of tachometer 82 and image guidance datatron 4 in unit 8
3rd input port 44 is connected, the first communication port 41 of image guidance datatron 4 and the second communication port 51 of Comprehensive control computer 5
Interconnection, the video output 46 of image guidance datatron 4 is connected with the analog video input port 52 of Comprehensive control computer 5.
Described vertical axises 24 are connected with support 26 by bearing 25.
Described vertical axises 24 are arranged on azimuth-drive motor and test the speed the top of unit 8.
It is fixed with the limited block 23 of sector at the top of described support 26, be fixed with gag lever post in the bottom of slide 22
29, gag lever post 29 is matched with limited block 23, makes slide 22 make the Finite rotation of horizontal direction, angle rotatable scope be-
120°~120°.
Described television tracking device 3 is fixed on the top surface of slide block 28 by equipment connecting plate 21.
The bottom of described slide 22 is fixed on the top of vertical axises 24 by orientation connecting plate 27.
Described television tracking device 3 is made up of camera lens, image controller (ccd), pretreatment circuit, shell and adapter；
Television tracking device 3 exports pal standard analog video.
Described image guidance datatron 4 is by servo controller, azimuth driver, pitch drive, DC source, image
Process plate, cabinet and adapter composition, wherein, servo controller is by Switching Power Supply, the control Ji Yu Digital Signal Processing (dsp)
Plate forms, and servo controller constitutes digital servo control using self-control Digital Signal Processing (dsp) panel as control core
System processed；The driving power supply of pitch drive adopts the direct-current switch power supply of model qnic-12 of Chaoyang power supply company: 220v
Exchange input, exports 24v, 0.5a DC voltage, and the drive module of pitch drive is used for receiving the tune of servo controller transmission
Frequency pulse width signal, drives pitching motor 9 to operate.
Described vertical axises 24, the support 26 and azimuth-drive motor unit 8 that tests the speed is vertical axises system, for supporting whole turntable
2, provide azimuth axis for turntable 2 simultaneously, realize orientation gyration.
Described pitching motor 9 adopts motor, model wn04ga15.
Described azimuth-drive motor test the speed unit 8 adopt DC moment-tachometer, model j160lyx03a-c01g,
Wherein, azimuth-drive motor 81 adopts permanent magnet D.C. torque motor to directly drive, and tachometer 82 is velocity feedback element.
The model mztrox morphis qxt of the described image pick-up card of Comprehensive control computer 5, Comprehensive Control
The address card of computer 5 adopts the asynchronous serial communication card of moxa company；The software pattern of Comprehensive control computer 5 adopts response
Mode carries out data interaction, using the data of the servo controller of image guidance datatron 4 as clock sync signal.
The specific work process of the present embodiment is described below in conjunction with the accompanying drawings.
The purpose of the present embodiment: the jamming effectiveness of testing laser jamming equipment 7, concrete test process is as follows:
Step one: set as shown in Fig. 2 being placed on TV guidance target seeker kinetic-simulator 1 and being test for Laser interferometers
In the range of standby 7 coverage；The preset cooperative target 6 joining examination is so that cooperative target 6 is disposed adjacent with Laser interferometers equipment 7；
Step 2: connect the power supply of image guidance datatron 4；
Step 3: television tracking device 3 is directed at cooperative target 6, makes the TV that cooperative target 6 is in television tracking device 3 regard
In, television tracking device 3 obtains the analog video of cooperative target 6, the figure now showing on the display of Comprehensive control computer 5
As shown in Figure 4；
Step 4: TV guidance target seeker kinetic-simulator 1 opens automatic tracking function, automatically locks cooperative target 6
In field of view center；
Detailed process is as follows: observes cooperative target 6 on the display of Comprehensive control computer 5, Comprehensive Control calculates
Machine 5 sends TV track instruction to image guidance datatron 4, and image guidance datatron 4 is to the analog video obtaining in step 3
Processed, tracking gate locks cooperative target, the image such as Fig. 5 institute now showing on the display of Comprehensive control computer 5
Show, television tracking device 3 exports the TV miss distance information of resolving to Comprehensive control computer 5 and image guidance datatron simultaneously
3 servo controller, servo controller carries out closed loop control according to TV miss distance information, by pitching motor 9 and orientation electricity
Machine 81 controls turntable 2 to rotate, is accurately directed at cooperative target 6, and television tracking device 3 relocks cooperative target 6, now Comprehensive Control
On the display of computer 5, the image of display is as shown in fig. 6, this process is simulated television guidance target seeker dynamic lock onto target mistake
Journey；
Step 5: Laser interferometers equipment 7 starts, transmitting interference laser；TV guidance target seeker kinetic-simulator 1 will be unable to
Normal locking cooperative target 6, from motion tracking failure, cooperative target 6 is lost；
Detailed process is as follows: under the laser effective illuminated of Laser interferometers equipment 7, the image meeting of television tracking device 3 output
Saturation or interference hot spot occur, now, the image meeting distortion of the image processing board resolving of image guidance datatron 4, lead to follow the tracks of
Ripple goalkeeper departs from cooperative target 6, and now on the display of Comprehensive control computer 5, the image of display is as shown in Figure 7；Depart from cooperation
It will be " false information " that target 6 further results in the miss distance that image processing board calculates, and servo controller will be according to this " false letter
Breath " control turntable 2 rotates so that cooperative target 6 television tracking device 3 relatively produces angle change, departs from visual field, now comprehensive control
On the display of computer 5 processed, the image of display is as shown in Figure 8；The laser of Laser interferometers equipment 7 persistently disturbs, television tracking device
3 lock unsuccessfully, and cooperative target 6 is lost, now on the display of Comprehensive control computer 5 display image as shown in figure 9, this
Process is also simulated television guidance target seeker dynamic unlocking object procedure.
As shown in Figure 10, Laser interferometers equipment 7 destroy the extraction process to cooperative target 6 for the television tracking device 3, make TV with
Track device 3 extracts error message, leads to the miss distance being sent to servo controller to be wrong, servo controller is according to this mistake
Information, adjustment turntable 2 rotate, make turntable 2 by the inceptive direction facing cooperative target 6, transition deviating from inceptive direction rotation,
And the angle after rotating is excessive, cooperative target 6 is led to thoroughly to disappear from the visual field of television tracking device 3.
Claims (6)
1. a kind of TV guidance target seeker kinetic-simulator, including turntable, television tracking device, image guidance datatron and comprehensive control
Computer processed is it is characterised in that described turntable is tested the speed by slide block, slide, pitching motor, vertical axises, support and azimuth-drive motor
Unit forms, and is provided with the slideway of arc in the top surface of slide, slide block is matched with slideway, pitching motor is fixed on slide,
The bottom of slide is fixed on the top of vertical axises, and the vertical axises and azimuth-drive motor unit that tests the speed is arranged in support, vertical axises and side
The inner flange of position motor speed measuring unit is fixedly and coaxially connected；Described television tracking device is fixed on slide block, television tracking device
Analog video delivery outlet is connected with the video input mouth of image guidance datatron, the first input port of pitching motor and image guidance
First delivery outlet of datatron is connected, and azimuth-drive motor tests the speed the second input port of azimuth-drive motor and image guidance datatron in unit
The second delivery outlet be connected, azimuth-drive motor test the speed tachometer in unit the 3rd delivery outlet defeated with the 3rd of image guidance datatron the
Entrance is connected, and the first communication port of image guidance datatron is interconnected with the second communication port of Comprehensive control computer, image guidance
The video output of datatron is connected with the analog video input port of Comprehensive control computer.
2. TV guidance target seeker kinetic-simulator according to claim 1 is it is characterised in that described vertical axises pass through
Bearing is connected with support.
3. TV guidance target seeker kinetic-simulator according to claim 1 is it is characterised in that described vertical axises are arranged
Above azimuth-drive motor tests the speed unit.
4. TV guidance target seeker kinetic-simulator according to claim 1 is it is characterised in that top in described support
Portion is fixed with limited block, is fixed with gag lever post in the bottom of slide, and gag lever post is matched with limited block.
5. TV guidance target seeker kinetic-simulator according to claim 1 is it is characterised in that described television tracking device
It is fixed on the top surface of slide block by equipment connecting plate.
6. TV guidance target seeker kinetic-simulator according to claim 1 is it is characterised in that the bottom of described slide
It is fixed on the top of vertical axises by orientation connecting plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510865865.9A CN105371701B (en) | 2015-12-01 | 2015-12-01 | television guidance seeker dynamic simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510865865.9A CN105371701B (en) | 2015-12-01 | 2015-12-01 | television guidance seeker dynamic simulator |
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| Publication Number | Publication Date |
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| CN105371701A CN105371701A (en) | 2016-03-02 |
| CN105371701B true CN105371701B (en) | 2017-02-01 |
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ID=55374115
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510865865.9A Expired - Fee Related CN105371701B (en) | 2015-12-01 | 2015-12-01 | television guidance seeker dynamic simulator |
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Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106338222B (en) * | 2016-09-23 | 2017-10-24 | 哈尔滨工业大学 | A kind of optical target dynamic simulation system with spheric motion track |
| CN106679504B (en) * | 2017-01-09 | 2018-08-10 | 中国人民解放军武汉军械士官学校 | A kind of simulated laser guidance experimental method and system |
| CN107358665A (en) * | 2017-07-11 | 2017-11-17 | 山东建筑大学 | A kind of automatic card taking safety-protection system for highway |
| CN107369217A (en) * | 2017-07-11 | 2017-11-21 | 山东建筑大学 | A kind of automatic card taking system for expressway tol lcollection card taking |
| CN107544259B (en) * | 2017-10-20 | 2019-12-24 | 中国科学院长春光学精密机械与物理研究所 | Method and system for guiding servo control to realize rapid overshoot-free tracking |
| CN109885101B (en) * | 2019-01-04 | 2022-02-22 | 北京测威科技有限公司 | Method and system for simulating missile terminal guidance by using unmanned aerial vehicle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3953132A (en) * | 1972-07-03 | 1976-04-27 | Rmc Research Corporation | System for registering position of element |
| CN102410785A (en) * | 2011-12-13 | 2012-04-11 | 林德福 | Turntable for semi-physical simulation of laser terminally guided projectile |
| CN102620605A (en) * | 2012-03-31 | 2012-08-01 | 林德福 | Global positioning system (GPS) and inertial navigation system (INS) combination guidance system for semi-physical simulation |
| CN105659881B (en) * | 2008-06-11 | 2014-02-12 | 北京航空航天大学 | Guidance control technical flying emulation platform |
| CN104360891A (en) * | 2014-10-10 | 2015-02-18 | 中国航天科技集团公司第四研究院第四十一研究所 | Emulational simple target simulation system for visible image guided missiles and simulation method thereof |
| CN104677203A (en) * | 2013-11-26 | 2015-06-03 | 哈尔滨智晟天诚科技开发有限公司 | Photoelectric tracking system based on turntable control |
-
2015
- 2015-12-01 CN CN201510865865.9A patent/CN105371701B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3953132A (en) * | 1972-07-03 | 1976-04-27 | Rmc Research Corporation | System for registering position of element |
| CN105659881B (en) * | 2008-06-11 | 2014-02-12 | 北京航空航天大学 | Guidance control technical flying emulation platform |
| CN102410785A (en) * | 2011-12-13 | 2012-04-11 | 林德福 | Turntable for semi-physical simulation of laser terminally guided projectile |
| CN102620605A (en) * | 2012-03-31 | 2012-08-01 | 林德福 | Global positioning system (GPS) and inertial navigation system (INS) combination guidance system for semi-physical simulation |
| CN104677203A (en) * | 2013-11-26 | 2015-06-03 | 哈尔滨智晟天诚科技开发有限公司 | Photoelectric tracking system based on turntable control |
| CN104360891A (en) * | 2014-10-10 | 2015-02-18 | 中国航天科技集团公司第四研究院第四十一研究所 | Emulational simple target simulation system for visible image guided missiles and simulation method thereof |
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