CN106896497A - The calculation method of adjustable storehouse moral mirror pilot angle in high precision - Google Patents
The calculation method of adjustable storehouse moral mirror pilot angle in high precision Download PDFInfo
- Publication number
- CN106896497A CN106896497A CN201611232485.2A CN201611232485A CN106896497A CN 106896497 A CN106896497 A CN 106896497A CN 201611232485 A CN201611232485 A CN 201611232485A CN 106896497 A CN106896497 A CN 106896497A
- Authority
- CN
- China
- Prior art keywords
- mirror
- formula
- angle
- moral
- storehouse moral
- 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
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/0012—Optical design, e.g. procedures, algorithms, optimisation routines
Abstract
The calculation method of adjustable storehouse moral mirror pilot angle, is related to fields of measurement in high precision, can obtain accurate adjustable storehouse moral mirror pilot angle expression formula.The method is：In laser transmitting system, shoot laser of the incident laser after multiple storehouse moral mirrors and adjustable storehouse moral mirror reflect is oriented parallel to boresight direction, eventually points to the extraterrestrial target being located on imaging optical system optical axis extended line；When the azimuth that extraterrestrial target deviates the optical axis is A, deviates the angle of pitch of the optical axis for E, by adjusting adjustable storehouse moral mirror around its own azimuth axis rotation β angle, after rotating γ angles further around its own pitch axis, make shoot laser pointing space target again；The β angles, the solution formula such as formula (2) at γ angles, formula (3) are shown, and A, E are known： The pilot angle of adjustable storehouse moral mirror is solved with formula (2), (3), high shoot laser pointing accuracy can be obtained under any turntable tracking error.
Description
Technical field
The present invention relates to field of measuring technique, and in particular to a kind of calculation method of the adjustable storehouse moral mirror pilot angle of high accuracy.
Background technology
In electro-optical countermeasure svstem, conventional turn back microscope group and storehouse moral microscope group change laser beam direction finally make laser light
Beam is along the direction outgoing parallel to the optical axis.In laser transmitting system wherein, incident laser passes sequentially through storehouse moral mirror one 1, storehouse
Moral mirror 22, storehouse moral mirror 33, storehouse moral mirror 44, adjustable storehouse moral mirror 5 turn back after outgoing, its principle is as shown in Figure 1.Pointing turntable
After the optical axis deviates tracked target, can just correct what is caused by the tracking error of pointing turntable by adjusting adjustable storehouse moral mirror 5
Shoot laser error in pointing, makes outgoing laser alignment tracked target, so as to improve the pointing accuracy of shoot laser.Adjustable storehouse moral
Mirror 5 has the advantages that small volume, compact conformation, fast response time, high precision, bandwidth are high, and size and the tracking of its pilot angle turn
The tracking error of platform carries out the high precision solution core that adjustable storehouse moral mirror 5 is controlled at last to pilot angle and asks into certain functional relation
Topic.
At present, it is general using the pilot angle of the adjustable storehouse moral mirror 5 of actual measurement and the error in pointing of shoot laser and to the data obtained
The method being fitted obtains the functional relation of description both sides relation, and this method acquired results are not accurate enough, there is certain mistake
Difference, it is impossible to shoot laser pointing accuracy higher is all obtained under any turntable tracking error.
The content of the invention
In order to obtain accurate adjustable storehouse moral mirror pilot angle expression formula, the present invention provides a kind of adjustable storehouse moral mirror control of high accuracy
The calculation method at angle processed.
The present invention is as follows to solve the technical scheme that technical problem is used：
The calculation method of the adjustable storehouse moral mirror pilot angle of high accuracy of the invention, comprises the following steps：
Step one, in imaging optical system, extraterrestrial target images in CCD target surfaces, when extraterrestrial target deviate the optical axis side
When parallactic angle is A, the angle of pitch of the deviation optical axis is E, the picture of extraterrestrial target deviates MDa, center of CCD target surfaces picture in the azimuth direction
Unit, in the pitch direction MDe, center of deviation CCD target surfaces pixel, relation such as formula (1) institute between described MDa, MDe and A, E
Show：
In formula (1)：The unit of A, E is rad, and the unit of pixel dimension is micron, the unit of imaging optical system focal length
It is millimeter；
Step 2, in laser transmitting system, incident laser is anti-through turn back mirror, storehouse moral microscope group and adjustable storehouse moral mirror of multiple
After penetrating, along the direction outgoing parallel to the optical axis, and the extraterrestrial target being located on imaging optical system optical axis extended line is eventually pointed to；
When extraterrestrial target deviate the optical axis azimuth for A, deviate the optical axis the angle of pitch be E when, by adjust adjustable storehouse moral mirror around its from
Body azimuth axis rotation β angle, after rotating γ angles further around its own pitch axis, makes shoot laser pointing space target again；The β
Angle, the solution formula such as formula (2) at γ angles, formula (3) are shown：
The beneficial effects of the invention are as follows：The present invention in order to obtain accurate adjustable storehouse moral mirror pilot angle expression formula, by building
The Mathematical Modeling of relation between the vertical adjustable storehouse moral mirror pilot angle of description and shoot laser direction, and be analyzed, derive form
The analytic equation formula (2) and formula (3) of succinct adjustable storehouse moral mirror pilot angle.Asked using formula (2) and formula (3) by facts have proved
The pilot angle of adjustable storehouse moral mirror is solved, high shoot laser pointing accuracy can be obtained under any turntable tracking error.
Brief description of the drawings
Fig. 1 is laser transmitting system schematic diagram.
Fig. 2 is that tracking error A, E resolves schematic diagram in imaging optical system.
Fig. 3 resolves schematic diagram for adjustable storehouse moral mirror pilot angle of the invention.
Fig. 4 is adjustable storehouse moral mirror reflex schematic diagram.
In figure：1st, storehouse moral mirror one, 2, storehouse moral mirror two, 3, storehouse moral mirror three, 4, storehouse moral mirror four, 5, adjustable storehouse moral mirror, 6, CCD targets
Face.
Specific embodiment
The present invention is described in further detail below in conjunction with accompanying drawing.
In order to obtain the expression formula of the accurate adjustable pilot angle of storehouse moral mirror 5, the present invention derives the succinct adjustable storehouse of form
The analytic equation of the pilot angle of moral mirror 5.As shown in Figure 3 and Figure 4, the resolving side of the adjustable storehouse moral mirror pilot angle of high accuracy of the invention
Method, its detailed process is as follows：
Step one, the tracking error for calculating tracking table
As shown in Fig. 2 in imaging optical system, extraterrestrial target P2It is imaged on CCD target surfaces 6.As extraterrestrial target P2
When on the optical axis extended line of imaging optical system, the center of CCD target surfaces 6 will be imaged in, if extraterrestrial target P2Deviate optical axis δ angles
I.e. the tracking error of tracking table is A (extraterrestrial target P2Deviate the optical axis azimuth), E (extraterrestrial target P2Deviate the pitching of the optical axis
Angle) when, extraterrestrial target P2Picture deviate MDa, 6 center of CCD target surfaces pixel in the azimuth direction, deviate CCD in the pitch direction
MDe, 6 center of target surface pixel.Described MDa and MDe is respectively orientation miss distance and pitching miss distance, and each moment
Orientation miss distance MDa, pitching miss distance MDe are known, therefore conventional orientation miss distance MDa, pitching miss distance MDe are represented
Tracking error A, E of tracking table.Orientation miss distance MDa, between pitching miss distance MDe and tracking error A, E of tracking table
Relation such as formula (1) shown in：
In formula (1)：The unit of tracking error A, E of tracking table is rad, and the unit of pixel dimension is micron (μm), into
As the unit of optical system focal length is millimeter (mm).
Step 2, the pilot angle for calculating adjustable storehouse moral mirror 5
As shown in Figure 1 and Figure 4, in laser transmitting system, debug using multiple storehouse moral mirrors and by optics, made incident sharp
Light is incided in initial position (i.e. a in Fig. 3 along the direction parallel to trunnion axis1Place) adjustable storehouse moral mirror 5 on, through adjustable
Shoot laser after storehouse moral mirror 5 reflects is oriented parallel to boresight direction, points to and is located on imaging optical system optical axis extended line
Extraterrestrial target P2.Extraterrestrial target P2After deviateing optical axis δ angles, adjustable storehouse moral mirror 5 needs to adjust its own pilot angle, so that parallel
Shoot laser after the incident laser of trunnion axis reflects through adjustable storehouse moral mirror 5 being capable of pointing space target P again2。
As shown in figure 3, setting up space coordinates, in space coordinates, Z axis are trunnion axis, are also incident laser
Incident direction, X-axis is the optical axis, is also the exit direction of shoot laser.
When adjustable storehouse moral mirror 5 is in initial position a1During place, the pitch axis ab and trunnion axis of adjustable storehouse moral mirror 5 are into 45 degree
Angle, pitch axis ab is located on straight line z1, straight line z1In XOZ planes；Azimuth axis cd overlaps with Y-axis, and azimuth axis cd is located at straight
Line y1On, straight line y1In Y-axis；Normal oe is located at straight line x1On, straight line x1In XOZ planes.
Adjustable storehouse moral mirror 5 is adjusted first around its own azimuth axis cd rotation βs angle, and now, adjustable storehouse moral mirror 5 is in position a2
Place, the pitch axis ab of adjustable storehouse moral mirror 5 is located at straight line z2On, straight line z2In XOZ planes；Azimuth axis cd overlaps with Y-axis, side
Position axle cd is located at straight line y2On, straight line y2In Y-axis, straight line y2With straight line y1Overlapped with Y-axis；Normal oe is located at straight line x2
On, straight line x2In XOZ planes.Now, straight line x1With straight line x2Between angle be β angles, straight line z1With straight line z2Between
Angle is also β angles.
Then adjustable storehouse moral mirror 5 is adjusted again around its own pitch axis ab rotation γ angles, and now, adjustable storehouse moral mirror 5 is in position
Put a3Place, the pitch axis ab of adjustable storehouse moral mirror 5 is located at straight line z3On, straight line z3With straight line z2Overlap, straight line z3Positioned at XOZ planes
It is interior；Azimuth axis cd is located at straight line y3On；Normal oe is located at straight line x3On.Now, straight line x2With straight line x3Between angle be γ
Angle, straight line y3Angle between Y-axis is also γ angles.
By adjusting adjustable storehouse moral mirror 5 first around its own azimuth axis cd rotation βs angle, γ is rotated further around its own pitch axis ab
Behind angle, shoot laser can be made to be directed away from the extraterrestrial target P at optical axis δ angles again2.Above-mentioned β angles solution formula such as formula (2) institute
Show, shown in the solution formula such as formula (3) at γ angles：
In formula (2) and formula (3)：A and E are respectively extraterrestrial target P2Deviate azimuth and the angle of pitch of the optical axis, the value of A and E
Can be solved according to formula (1).
The above is only the preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art
For member, under the premise without departing from the principles of the invention, some improvements and modifications can also be made, these improvements and modifications also should
It is considered as protection scope of the present invention.
Claims (1)
1. the calculation method of the adjustable storehouse moral mirror pilot angle of high accuracy, it is characterised in that comprise the following steps：
Step one, in imaging optical system, extraterrestrial target (P2) CCD target surfaces (6) are imaged in, as extraterrestrial target (P2) deviate regard
When the azimuth of axle is A, the angle of pitch of the deviation optical axis is E, extraterrestrial target (P2) picture deviate CCD target surfaces in the azimuth direction
(6) MDa, center pixel, in the pitch direction deviation CCD target surface (6) MDe, center pixel, between described MDa, MDe and A, E
Relation such as formula (1) shown in：
In formula (1)：The unit of A, E is rad, and the unit of pixel dimension is micron, and the unit of imaging optical system focal length is milli
Rice；
Step 2, in laser transmitting system, incident laser is anti-through turn back mirror, storehouse moral microscope group and adjustable storehouse moral mirror (5) of multiple
After penetrating, along the direction outgoing parallel to the optical axis, and the extraterrestrial target being located on imaging optical system optical axis extended line is eventually pointed to
(P2)；As extraterrestrial target (P2) deviate the optical axis azimuth for A, deviate the optical axis the angle of pitch be E when, by adjusting adjustable storehouse moral
Mirror (5) after rotating γ angles further around its own pitch axis, makes shoot laser pointing space again around its own azimuth axis rotation β angle
Target (P2)；The β angles, the solution formula such as formula (2) at γ angles, formula (3) are shown：
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611232485.2A CN106896497A (en) | 2016-12-28 | 2016-12-28 | The calculation method of adjustable storehouse moral mirror pilot angle in high precision |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611232485.2A CN106896497A (en) | 2016-12-28 | 2016-12-28 | The calculation method of adjustable storehouse moral mirror pilot angle in high precision |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106896497A true CN106896497A (en) | 2017-06-27 |
Family
ID=59198934
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611232485.2A Pending CN106896497A (en) | 2016-12-28 | 2016-12-28 | The calculation method of adjustable storehouse moral mirror pilot angle in high precision |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106896497A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109471252A (en) * | 2018-11-02 | 2019-03-15 | 北京仿真中心 | A kind of complexity optical scene spatial movement simulator |
| CN114755818A (en) * | 2022-05-19 | 2022-07-15 | 中国科学院长春光学精密机械与物理研究所 | Device and method for adjusting German optical path of large-aperture telescope warehouse |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5115355A (en) * | 1990-11-27 | 1992-05-19 | Thermo Electron Technologies Corp. | Compact coude optics system |
| US20070229994A1 (en) * | 2006-03-30 | 2007-10-04 | Raytheon Company | Pointable optical system with coude optics having a short on-gimbal path length |
-
2016
- 2016-12-28 CN CN201611232485.2A patent/CN106896497A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5115355A (en) * | 1990-11-27 | 1992-05-19 | Thermo Electron Technologies Corp. | Compact coude optics system |
| US20070229994A1 (en) * | 2006-03-30 | 2007-10-04 | Raytheon Company | Pointable optical system with coude optics having a short on-gimbal path length |
Non-Patent Citations (2)
| Title |
|---|
| 乔健 等: ""水平式两轴转台中库德光路的快速装调"", 《光学 精密工程》 * |
| 薛乐堂 等: ""快速反射镜姿态角的高精度解算"", 《光学 精密工程》 * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109471252A (en) * | 2018-11-02 | 2019-03-15 | 北京仿真中心 | A kind of complexity optical scene spatial movement simulator |
| CN109471252B (en) * | 2018-11-02 | 2021-09-10 | 北京仿真中心 | Complex optical scene space motion simulation device |
| CN114755818A (en) * | 2022-05-19 | 2022-07-15 | 中国科学院长春光学精密机械与物理研究所 | Device and method for adjusting German optical path of large-aperture telescope warehouse |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105510899B (en) | A kind of coaxial detecting system of laser radar and its automatic calibrating method | |
| CN109186944B (en) | Airborne multi-optical-axis optical load optical axis consistency calibration method | |
| CN107132636A (en) | A kind of aspherical primary mirror reflecting surface debugs benchmark calibration method and its system | |
| CN105066910B (en) | Electro-optic crystal Z axis deviate angle measuring device and measuring method | |
| US10821911B2 (en) | Method and system of camera focus for advanced driver assistance system (ADAS) | |
| CN103837080B (en) | Sub-micrometer precision coaxial confocal towards micro assemby is directed at detection method and device | |
| CN105116515A (en) | Off-axis tri-reflector zooming optical system adjusting method | |
| CN107478195A (en) | One kind is based on optical space object status measurement apparatus and its measuring method | |
| CN104539829A (en) | Optical-mechanical structure based on infrared area array detector scanning imaging | |
| CN105823420A (en) | Method for precise derivation of light-return energy center coordinates of pyramid combined part | |
| US20150268346A1 (en) | Optical axis directing apparatus | |
| CN106249427B (en) | A kind of optic axis adjusting method based on laser imaging | |
| CN106896497A (en) | The calculation method of adjustable storehouse moral mirror pilot angle in high precision | |
| CN103226240B (en) | Multi-channel normal incidence imaging system and installation and adjustment method thereof | |
| CN106918447A (en) | Target automatic direction regulating formula plain shaft parallelism detection method and device | |
| CN206038278U (en) | Concave mirror imaging measurement telephoto lens modulation transfer function's device | |
| CN109579776A (en) | Anti-interference big working distance autocollimation and method in high precision | |
| CN108827596A (en) | One kind being applied to the novel common phase detection method of sectional type spliced telescope and device | |
| CN103345038A (en) | Cube-corner prism vertical type optical axis determining system and method | |
| CN103092001A (en) | Device for adjusting position and angle of light beam | |
| US8531657B2 (en) | Micro-radian class line of sight and centration stabilization system | |
| CN111928774A (en) | Target tracking, positioning and measuring method based on combination of camera and range finder | |
| CN103344212A (en) | Laser target for measuring shield attitude angle and measuring method of laser target | |
| US10337857B2 (en) | Multi-spectral boresight alignment methods and systems | |
| CN102038552A (en) | High-precision diagnostic equipment collimation method and device thereof |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170627 |
|
| WD01 | Invention patent application deemed withdrawn after publication |