CN106507896B - High accuracy precision guided weapon system optics target simulator - Google Patents
High accuracy precision guided weapon system optics target simulatorInfo
- Publication number
- CN106507896B CN106507896B CN200810078494.XA CN200810078494A CN106507896B CN 106507896 B CN106507896 B CN 106507896B CN 200810078494 A CN200810078494 A CN 200810078494A CN 106507896 B CN106507896 B CN 106507896B
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- CN
- China
- Prior art keywords
- dimensional turntable
- pitching
- data acquisition
- guided missile
- acquisition control
- 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.)
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Abstract
The present invention relates to a kind of high accuracy precision guided weapon system optics target simulator, belongs to the guided missile test set of technical area, it includes data acquisition control device, controlling machine box, dimensional turntable and support and optical imaging device；Controlling machine box pass through cable connection with dimensional turntable, it is connected with RS-232 serial ports with the main frame of data acquisition control device, the core of controlling machine box is the single-chip microcomputer of TNC80C196, its effect is the control instruction and data that receiving data acquisition control device sends, and controls dimensional turntable and completes level, elevating movement；Horizontal moment motor of the dimensional turntable by vertical rotation axis and with tachometer is mounted on the mounting surface of movable supporting frame, dimensional turntable is " U " type frame structure, and the two ends of " U " type frame are respectively provided with pitching moment motor, pitching speed measuring motor, pitching potentiometer and pitching buffer limiter.The equipment can complete the test before the Second Echelon Maintenance of guided missile and guided missile on-hook to TV terminal guidance guided missile.
Description
Technical field
The present invention relates to a kind of high-precision precision guided weapon system optics target simulator, belong to technical area
Guided missile test set.
Background technology
Guided missile optics cabin is a part for certain type of missile, and its stabilization system test and tracking system are debugged
Can only qualitatively measure after complete.In order to the adjustment of certain type of missile optics cabin and its stabilization system test
Debugged with tracking system and carry out quantitative measurement, and can adjusted in certain type of missile optics cabin assembling factory, technology
The place such as test cell completes to carry out semi-automatic survey to guided missile optics cabin and its systems stabilisation and TV tracker system
Examination.
The content of the invention：
In order to overcome the shortcoming of prior art, the present invention provides a kind of high-precision precision guided weapon system optics
Target simulator, it can enable guided missile in the limited place such as laboratory or technical area, guided missile storehouse, real
Existing its catches target, tracking target capabilities and some quiet, dynamic state indexs and provides qualitative, quantitative measurement results,
Test before the Second Echelon Maintenance of completion guided missile and guided missile on-hook to TV terminal guidance guided missile.
The technical scheme adopted by the invention to solve the technical problem is that：It includes：
Data acquisition control device：Including display, keyboard, mouse and main frame；
Controlling machine box：With dimensional turntable by cable connection, the main frame RS-232 with data acquisition control device
Serial port is connected, and the core of controlling machine box is TNC80C196 single-chip microcomputer, and it is to receive data acquisition that it, which is acted on,
Control instruction and data that control device is sent, control optical imaging device and dimensional turntable；
Dimensional turntable and support：Horizontal moment motor of the dimensional turntable by vertical rotation axis and with tachometer is mounted in
On the mounting surface of movable supporting frame, horizontal moment motor drives dimensional turntable to make to horizontally rotate, and dimensional turntable is
" U " type frame structure, the two ends of " U " type frame are equipped with pitching moment motor, pitching speed measuring motor, pitching electricity
Position device and pitching buffer limiter, pitching moment motor drive " U " type frame make the motion of pitch orientation, pitching
Potentiometer exports the position quantity of pitching.The axle center of vertical rotation axis and horizontal rotating shaft is respectively provided with a red laser
Device, the left and right and bottom for the red hot spot alignment guided missile front-end optical cabin front portion that three red lasers are sent
Three measurement points；
Optical imaging device：Optical imaging device is in dimensional turntable, and its front end is equipped with lens assembly, mirror
Head assembly is made up of camera lens, target and lighting device, and instrument bulb is housed in lighting device.
The present invention can enable guided missile in the limited place such as laboratory or technical area, guided missile storehouse, realize it
Catch target, tracking target capabilities and some quiet, dynamic state indexs and provide qualitative, quantitative measurement results, it is complete
Test before into the Second Echelon Maintenance of guided missile and guided missile on-hook to TV terminal guidance guided missile.
Brief description of the drawings
The present invention is further described with reference to the accompanying drawings and examples.
Fig. 1 is dimensional turntable of the present invention and support front view；
Fig. 2 is dimensional turntable of the present invention and support left view；
Fig. 3 is the A direction views in Fig. 2 of the present invention；
Fig. 4 is the B-B sectional views in Fig. 2 of the present invention；
Fig. 5 is controlling machine box servo-drive system block diagram of the present invention.
Embodiment
The present invention include data acquisition control device, controlling machine box, dimensional turntable 8 and support 10 and optics into
As device 15.
Described data acquisition control device includes display, keyboard, mouse and main frame.
Described controlling machine box and dimensional turntable 8 are by cable connection, the main frame with data acquisition control device
Connected with RS-232 serial ports, the order that main frame is sent is received by serial port, and to main frame loopback target mould
Intend the current information of device, the core of controlling machine box is TNC80C196 single-chip microcomputer, it is to receive data that it, which is acted on,
Control instruction and data that acquisition control device is sent, control optical imaging device 2 and dimensional turntable 8, such as
Shown in Fig. 5.
As Figure 1-4, described dimensional turntable 8 is by vertical rotation axis and the horizontal moment with tachometer is electric
Machine 9 is on the mounting surface of movable supporting frame 10, and horizontal moment motor 9 drives dimensional turntable 8 to make level
Rotate, dimensional turntable 8 is " U " type frame structure, the two ends of " U " type frame are equipped with pitching moment motor 3, bowed
Speed measuring motor 6, pitching potentiometer 7 and pitching buffer limiter 14 are faced upward, pitching moment motor 3 drives " U "
Type frame 15 makees the motion of pitch orientation, and pitching potentiometer 7 exports the position quantity of pitching.Described vertical rotation axis
Be respectively provided with a red laser 4,5,12 with the axle center of horizontal rotating shaft, three red lasers 4,5,
The anterior left and right and measurement point of bottom three in the 12 red hot spot alignment guided missile front-end optical cabins sent, so
It can just make target simulator camera lens and optics cabin camera lens on an axle, otherwise, target can not be imaged on optics
On the camera lens of cabin.
Described optical imaging device 2 is in dimensional turntable 8, and its front end is equipped with lens assembly.Lens group
Part is made up of camera lens, target 1 and lighting device, and instrument bulb is housed in lighting device, and bulb is replaceable.
Operation principle：
1st, optical analog target is formed
Optical analog target is completed by optical module.Optical module has following functions：1) optical mode, is produced
Intend target, the target for being carved with target figure is placed on the focal plane of rear lens, by optical system below into infinite
Remote target is as being simulated target；2) in, the brightness of variation targets, the illuminator for changing optical module
Bulb voltage, reaches the luminosity of control bulb, so that the brightness of variation targets.Wherein in controlling machine box
Brightness power board, luminance signal is amplified, lighting.Brilliance control instruction is by RS-232 serial ports by leading
Machine is sent.Main frame can send out 16 grades of orders, and system default is 05 grade during start, and the order more than 15 is located
Manage as the order less than 15.
2nd, the kinetic characteristic of optical analog target
Dimensional turntable 8 can be rotated in the range of ± 22 ° in the horizontal direction, in+6 °~-22 ° models of pitch orientation
Enclose interior swing.The rotation of dimensional turntable 8, drives optical imaging device 2 to move, equivalent to target and bullet
Relative motion.Due to being equipped with speed and position sensor in dimensional turntable 8, the motion of dimensional turntable 8 is led to
Cross speed and position sensor can measure dimensional turntable 8 in level and the direction of pitching two velocity of rotation and institute at any time
The position at place, while on the one hand to give digital display circuit display speed big for the level surveyed, luffing speed and position
Small and residing angle position, the servo-drive system composition negative velocity feedback and location negative that controlling machine box are fed back to again is anti-
Feedback.
Claims (2)
1. a kind of high-precision precision guided weapon system optics target simulator, it is characterised in that：It includes：
Data acquisition control device：Including display, keyboard, mouse and main frame；
Controlling machine box：With dimensional turntable (8) cable connection, the main frame RS-232 with data acquisition control device
Serial port is connected, and the core of controlling machine box is TNC80C196 single-chip microcomputer, for receiving data acquisition control
Control instruction and data that device is sent, control optical imaging device (2) and dimensional turntable (8)；
Dimensional turntable (8) and support (10)：The water of dimensional turntable (8) by vertical rotation axis and with tachometer
Flat torque motor (9) is on the mounting surface of movable supporting frame (10), and horizontal moment motor (9) is rotated
Dimensional turntable (8) is driven to make to horizontally rotate, dimensional turntable (8) is " U " type frame structure, " U " type frame
Two ends delay equipped with pitching moment motor (3), pitching speed measuring motor (6), pitching potentiometer (7) and pitching
Limiter (14) is rushed, pitching moment motor (3) drives optical imaging device (2) to be rotated in pitch orientation,
Pitching potentiometer (7) export pitching position quantity, the axis hole of vertical rotation axis built with red laser (12),
Left and right is respectively equipped with a red laser (4,5) in the axis hole of horizontal rotating shaft, three red lasers (4,5,
12) the left and right and measurement point of bottom three of the red hot spot alignment guided missile front-end optical cabin front portion sent；
Optical imaging device (2)：Optical imaging device (2) is in dimensional turntable (8), optical imagery
Device (2) front end is equipped with lens assembly, and lens assembly is made up of camera lens, target (1) and lighting device,
Instrument bulb is housed in lighting device.
2. high-precision precision guided weapon system optics target simulator according to claim 1, it is special
Levy and be：Described dimensional turntable (8) is rotated in the range of ± 22 ° in the horizontal direction ,+6 ° of pitch orientation~
Rotated in the range of -22 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200810078494.XA CN106507896B (en) | 2008-12-09 | 2008-12-09 | High accuracy precision guided weapon system optics target simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200810078494.XA CN106507896B (en) | 2008-12-09 | 2008-12-09 | High accuracy precision guided weapon system optics target simulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106507896B true CN106507896B (en) | 2012-07-25 |
Family
ID=58359024
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200810078494.XA Active CN106507896B (en) | 2008-12-09 | 2008-12-09 | High accuracy precision guided weapon system optics target simulator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106507896B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108535738A (en) * | 2018-03-22 | 2018-09-14 | 北京控制工程研究所 | A kind of multiple spurs is from dot laser three-dimensional close-range imaging simulator and analogy method |
-
2008
- 2008-12-09 CN CN200810078494.XA patent/CN106507896B/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108535738A (en) * | 2018-03-22 | 2018-09-14 | 北京控制工程研究所 | A kind of multiple spurs is from dot laser three-dimensional close-range imaging simulator and analogy method |
| CN108535738B (en) * | 2018-03-22 | 2020-04-10 | 北京控制工程研究所 | Multi-distance-point laser three-dimensional close-range imaging simulator and simulation method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR03 | Grant of secret patent right | ||
| DC01 | Secret patent status has been lifted | ||
| DCSP | Declassification of secret patent |