[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

CN114967022B - Optical calibration method of autocollimating dynamic target based on double theodolite - Google Patents

Optical calibration method of autocollimating dynamic target based on double theodolite Download PDF

Info

Publication number
CN114967022B
CN114967022B CN202210431438.XA CN202210431438A CN114967022B CN 114967022 B CN114967022 B CN 114967022B CN 202210431438 A CN202210431438 A CN 202210431438A CN 114967022 B CN114967022 B CN 114967022B
Authority
CN
China
Prior art keywords
theodolite
posture
mirror
sub
calibration
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.)
Active
Application number
CN202210431438.XA
Other languages
Chinese (zh)
Other versions
CN114967022A (en
Inventor
李响
周晨
常帅
宋延嵩
董岩
赵馨
高亮
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Changchun University of Science and Technology
Original Assignee
Changchun University of Science and Technology
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Changchun University of Science and Technology filed Critical Changchun University of Science and Technology
Priority to CN202210431438.XA priority Critical patent/CN114967022B/en
Publication of CN114967022A publication Critical patent/CN114967022A/en
Application granted granted Critical
Publication of CN114967022B publication Critical patent/CN114967022B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B7/00Mountings, adjusting means, or light-tight connections, for optical elements
    • G02B7/003Alignment of optical elements
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C1/00Measuring angles
    • G01C1/02Theodolites
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C15/00Surveying instruments or accessories not provided for in groups G01C1/00 - G01C13/00
    • G01C15/02Means for marking measuring points
    • G01C15/06Surveyors' staffs; Movable markers
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B7/00Mountings, adjusting means, or light-tight connections, for optical elements
    • G02B7/003Alignment of optical elements
    • G02B7/004Manual alignment, e.g. micromanipulators
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00Energy generation of nuclear origin
    • Y02E30/10Nuclear fusion reactors

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Optical Radar Systems And Details Thereof (AREA)
  • Mounting And Adjusting Of Optical Elements (AREA)

Abstract

An auto-collimation dynamic target optical calibration method based on double theodolites belongs to the technical field of optical detection and calibration, and particularly relates to an auto-collimation dynamic target structure and a calibration scheme. The invention solves the problem of high difficulty in assembling and calibrating the existing auto-collimation dynamic target. The invention adopts a double theodolite to realize the installation and correction process, firstly adopts a rotary optical axis and a test reference radiation mirror to determine the main and initial positions and the postures of the first theodolite, then the first theodolite carries out installation and correction on the first light guide mirror, then adjusts the relative postures of a sub-optical path and the rotary optical axis, finally carries out installation and correction on the postures of the second light guide mirror, and completes the installation and correction process of the sub-optical path and the light guide mirror. The invention realizes the quick assembly and correction of the coaxiality of the dynamic target sub-optical path and the optical axis of the guide lens, improves the assembly and correction efficiency aiming at the dynamic target, and reduces the technical requirements on operators. The invention is suitable for the technical field of manufacturing and debugging of auto-collimation dynamic targets.

Description

基于双经纬仪的自准直动态靶标光学装校方法Optical calibration method of autocollimating dynamic target based on double theodolite

技术领域technical field

本发明属于光学检测与装校技术领域,具体涉及到基于双经纬仪的自准直动态靶标子光路与导向镜装校方法。The invention belongs to the technical field of optical detection and installation and calibration, and in particular relates to an autocollimation dynamic target sub-optical path and a guide mirror installation and calibration method based on double theodolites.

背景技术Background technique

动态靶标常用于各种跟踪系统的跟踪性能测试。传统的动态靶标通过模拟无穷远处运动目标,使被测跟踪系统对目标进行跟踪,再借助其他测量仪器完成被测跟踪系统的跟踪性能和系统参数的检测,检测过程繁琐。与传统的动态靶标不同,自准直动态靶标不仅可以模拟无穷远处运动目标,还能接收由被测跟踪系统发射的光束,实现对被测系统跟踪精度的直接测量。Dynamic targets are often used in tracking performance tests of various tracking systems. The traditional dynamic target simulates the moving target at infinity, makes the tracking system under test track the target, and then completes the detection of the tracking performance and system parameters of the tracking system under test with the help of other measuring instruments, and the detection process is cumbersome. Different from the traditional dynamic target, the self-collimating dynamic target can not only simulate the moving target at infinity, but also receive the beam emitted by the tracking system under test, so as to realize the direct measurement of the tracking accuracy of the system under test.

由于自准直动态靶标同时包含接收单元、发射单元以及摇臂等结构,大大增加了系统装校的难度。现有的装校方法只是利用平行光管进行装校,装校不同组件时需移动平行光管,极为不方便。因此,如何完成自准直动态靶标子光路、光学天线以及旋转导向镜光轴一致性的装校是难以解决的问题,目前迫切需要一种能够满足自准直动态靶标光路装校的方法。Since the self-collimating dynamic target includes structures such as receiving unit, transmitting unit and rocker arm at the same time, the difficulty of system installation and calibration is greatly increased. The existing calibration method only uses the collimator for calibration, and it is extremely inconvenient to move the collimator during calibration of different components. Therefore, how to complete the calibration of the sub-optical path of the autocollimation dynamic target, the optical antenna and the consistency of the optical axis of the rotating guide mirror is a difficult problem to solve. At present, there is an urgent need for a method that can satisfy the calibration of the optical path of the autocollimation dynamic target.

综上因素,由于现有的自准直动态靶标同时包含接收单元、发射单元以及摇臂等结构,造成系统装校的难度大。To sum up the above factors, since the existing self-collimating dynamic target includes structures such as receiving unit, transmitting unit and rocker arm at the same time, it is very difficult to install and calibrate the system.

发明内容Contents of the invention

本发明解决了现有自准直动态靶标装校难度大的问题。本发明采用双经纬仪,先对第一导向镜进行装校,然后再依据该第一导向镜对第二导向镜进行装校。The invention solves the problem that the existing self-collimating dynamic target is difficult to install and calibrate. The present invention adopts double theodolite, firstly adjusts the first guide mirror, and then adjusts the second guide mirror according to the first guide mirror.

本发明所述的基于双经纬仪的自准直动态靶标光学装校方法是采用双经纬仪实现自准直动态靶的导光镜和子光路的同轴装校,所述装校方法包括:The self-collimating dynamic target optical calibration method based on the double theodolite of the present invention is to adopt the double theodolite to realize the coaxial calibration of the light guide mirror and the sub-optical path of the self-collimating dynamic target, and the calibration method includes:

步骤一、通过自准直动态靶标装校工装26固定旋转光轴15,采用第一经纬仪17结合测试基准反射镜16完成基准反射镜16与旋转光轴15的光轴一致性装校,此时第一经纬仪17的姿态为A;Step 1. Fix the rotating optical axis 15 through the self-collimating dynamic target installation tool 26, and use the first theodolite 17 in combination with the test reference mirror 16 to complete the alignment of the optical axis consistency between the reference mirror 16 and the rotating optical axis 15. At this time The posture of the first theodolite 17 is A;

步骤二、调整第一经纬仪17旋转45°、变成姿态C;调整确定第二经纬仪20的位置和初始姿态B;Step 2, adjust the first theodolite 17 to rotate 45 °, become attitude C; adjust and determine the position and initial attitude B of the second theodolite 20;

步骤三、安装第一导光镜21,通过第二经纬仪调整所述第一导光镜21的姿态,对所述第一导光镜21与旋转光轴15的夹角的校准,完成所述第一导光镜21的装校;此时所述第二经纬仪的姿态为D;Step 3, install the first light guide mirror 21, adjust the posture of the first light guide mirror 21 through the second theodolite, and calibrate the angle between the first light guide mirror 21 and the rotating optical axis 15, and complete the described The installation of the first light guide mirror 21; the attitude of the second theodolite is D now;

步骤四、拆下所述第一导向镜21和测试基准反射镜16;Step 4, remove the first guide mirror 21 and the test reference mirror 16;

步骤五、将子光路13及卡式天线14整体安装到回转光轴15的左端,调整第一经纬仪17的姿态恢复到姿态A,通过所述第一经纬仪17校准子光路13和卡式天线14的姿态,完成子光路13和卡式天线14的装校;Step five, install the sub-optical path 13 and the cassette antenna 14 as a whole on the left end of the rotating optical axis 15, adjust the posture of the first theodolite 17 to return to posture A, and calibrate the sub-optical path 13 and the cassette antenna 14 through the first theodolite 17 attitude, complete the installation of the sub-optical path 13 and the card antenna 14;

步骤六、取下基准反射镜2;将第一导向镜21安装到原来位置,并通过安装定位销固定;Step 6, remove the reference mirror 2; install the first guide mirror 21 to the original position, and fix it by installing the positioning pin;

步骤七、安装第二导光镜19,通过第一经纬仪17结合第二经纬仪20调整第二导光镜19的姿态,完成所述第二导光镜19的装校。Step 7: Install the second light guide mirror 19 , adjust the posture of the second light guide mirror 19 through the first theodolite 17 and the second theodolite 20 , and complete the installation and calibration of the second light guide mirror 19 .

进一步,对所述步骤一的具体方法举例说明为:Further, the specific method of the step 1 is exemplified as follows:

将旋转光轴15固定在自准直动态靶标装校工装26上;Fix the rotating optical axis 15 on the autocollimating dynamic target installation and calibration tooling 26;

在所述旋转光轴15内部设置的固定基准反射镜的凸台25上固定测试基准反射镜16;Fix the test reference mirror 16 on the boss 25 of the fixed reference mirror provided inside the rotating optical axis 15;

将第一经纬仪17置于所述旋转光轴15右侧,并保持其为水平姿态,然后,调整其位置和姿态,使得所述第一经纬仪17发射的光束经基准反射镜16反射之后再次入射至第一经纬仪17内形成成像十字光斑;Place the first theodolite 17 on the right side of the rotating optical axis 15, and keep it as a horizontal posture, then adjust its position and posture so that the light beam emitted by the first theodolite 17 is incident again after being reflected by the reference reflector 16 To form an imaging cross spot in the first theodolite 17;

控制旋转光轴15转动,直到所述第一经纬仪17中的成像十字光斑移动至与其十字线中心位置,完成基准反射镜16与旋转光轴15的光轴一致性装校;标记此时第一经纬仪17的姿态为A,并记录所述姿态A的方位与俯仰数值。Control the rotating optical axis 15 to rotate until the imaging cross spot in the first theodolite 17 moves to the center position of its crosshair, and complete the alignment of the optical axis of the reference mirror 16 and the rotating optical axis 15; mark the first The attitude of the theodolite 17 is A, and the azimuth and elevation values of the attitude A are recorded.

进一步,对所述步骤二的具体方法举例说明为:Further, the specific method of the step 2 is illustrated as follows:

将所述第一经纬仪17方位旋转45°、变成姿态C,将第二经纬仪20调整其处于水平姿态,通过调整第二经纬仪20的位置、姿态,使第一经纬仪17发射的光进入到第二经纬仪20中并形成成像十字光斑、并使得所述成像十字光斑移动至所述第二经纬仪20的十字线中心位置,此时第二经纬仪20姿态为初始姿态B,并记录该姿态下的方位与俯仰数值。The first theodolite 17 azimuth is rotated 45 °, becomes attitude C, the second theodolite 20 is adjusted it is in horizontal attitude, by adjusting the position, the attitude of the second theodolite 20, the light that the first theodolite 17 is emitted enters the second theodolite In the second theodolite 20, an imaging cross spot is formed, and the imaging cross spot is moved to the crosshair center position of the second theodolite 20. At this moment, the attitude of the second theodolite 20 is the initial attitude B, and the orientation under the attitude is recorded. and pitch values.

进一步,对所述步骤三的具体方法举例说明为:Further, the specific method of the step 3 is exemplified as follows:

调整第二经纬仪20的方位旋转45°、使其指向第一导向镜21的安装位置;Adjust the azimuth rotation of the second theodolite 20 for 45° so that it points to the installation position of the first guide mirror 21;

在所述安装位置安装第一导向镜21;Install the first guide mirror 21 at the installation position;

控制第二经纬仪20发射光束,使得经所述第一导向镜21反射的光束入射至所述第二经纬仪20形成成像十字光斑,调整所述第一导向镜21的姿态,直到所述十字光斑移动至所述第二经纬仪20的中心十字线中心位置,完成第一导向镜21与旋转光轴15夹角的校准;此时,第一导向镜21的姿态D。Control the second theodolite 20 to emit light beams, so that the light beams reflected by the first guide mirror 21 enter the second theodolite 20 to form an imaging cross spot, adjust the attitude of the first guide mirror 21 until the cross spot moves To the center position of the central cross line of the second theodolite 20 , the calibration of the angle between the first guiding mirror 21 and the rotating optical axis 15 is completed; at this time, the attitude D of the first guiding mirror 21 .

进一步,对所述步骤五的具体方法举例说明为:Further, the specific method of the step five is exemplified as:

将子光路13及卡式天线14整体安装到回转光轴15的左端;The sub-optical path 13 and the card antenna 14 are integrally installed on the left end of the rotating optical axis 15;

将第一经纬仪17的姿态调整成姿态A,然后发出光束,使所述光束经卡式天线14上的基准反射镜2反射、并在所述第一经纬仪17中形成成像十字光斑;The attitude of the first theodolite 17 is adjusted to attitude A, and then the light beam is sent, and the light beam is reflected by the reference reflector 2 on the card antenna 14, and the imaging cross spot is formed in the first theodolite 17;

通过调整子光路13及卡式天线14整体姿态,直到所述成像十字光斑移动到所述第一经纬仪17的十字线中心位置,实现子光路的光轴与旋转轴的光轴校准,完成子光路13的装校。By adjusting the overall posture of the sub-optical path 13 and the card antenna 14 until the imaging cross spot moves to the center position of the crosshairs of the first theodolite 17, the optical axis of the sub-optical path and the optical axis of the rotation axis are aligned, and the sub-optical path is completed. 13 outfits.

进一步,对所述步骤七的具体方法举例说明为:Further, the specific method of the step 7 is exemplified as:

取下基准反射镜2,将第二导向镜19安装在所述摇臂18的第一导向镜的安装位置;Take off the reference reflector 2, and install the second guide mirror 19 at the installation position of the first guide mirror of the rocker arm 18;

将第一经纬仪17旋转60度变成姿态F;Turn the first theodolite 17 into attitude F by 60 degrees;

调整第二经纬仪20的姿态,使得所述第二经纬仪20接收到的成像十字光斑位于所述第二经纬仪20的十字线中心位置,此时,第二经纬仪20的位置和姿态为E;Adjust the posture of the second theodolite 20, so that the imaging cross spot that the second theodolite 20 receives is located at the crosshair center position of the second theodolite 20, at this moment, the position and the posture of the second theodolite 20 are E;

将所述第二经纬仪20的角度旋转120°变成姿态H,使其发射的光束对准第二导向镜19;Rotate the angle of the second theodolite 20 by 120° to become attitude H, so that the light beam it emits is aimed at the second guide mirror 19;

子光路13发射光束,所述光束经第一导向镜21反射后发射至第二导向镜19,经所述第二导向镜19反射后入射至第二经纬仪20,在所述第二经纬仪20内形成成像十字光斑;The sub-optical path 13 emits light beams, and the light beams are reflected by the first guide mirror 21 and then sent to the second guide mirror 19, and then incident on the second theodolite 20 after being reflected by the second guide mirror 19, in the second theodolite 20 Form an imaging cross spot;

调整第二导向镜19的姿态、使得所述成像十字光斑移动至第二经纬仪20中的十字线中心位置,通过定位销固定第二导向镜19,完成所述第二导光镜19的装校。Adjust the posture of the second guide mirror 19 so that the imaging cross spot moves to the center position of the crosshairs in the second theodolite 20, fix the second guide mirror 19 by positioning pins, and complete the installation and calibration of the second guide mirror 19 .

进一步,所述子光路13和卡式天线14固定在一起形成一个整体,所述整体方法举例说明包括:Further, the sub-optical circuit 13 and the card antenna 14 are fixed together to form a whole, and the whole method includes:

将自准直动态靶标子光路13及卡式天线14整体安装在子光路装校工装1上,所述装校工装1固定于水平光学平台4上;The self-collimating dynamic target sub-optical path 13 and the card antenna 14 are integrally installed on the sub-optical path calibration tool 1, and the calibration tool 1 is fixed on the horizontal optical platform 4;

安装基准反射镜2于卡式光学天线14次镜预留位置处;Install the reference reflector 2 at the position reserved for the 14th secondary mirror of the card-type optical antenna;

控制平行光管3发射光束入射至基准反射镜2,并经所述基准反射镜2反射回平行光管3,并所述平行光管3之后入射至平行管相机24中形成成像光斑;Control the collimator 3 to emit light beams to enter the reference mirror 2, and reflect back to the collimator 3 through the reference mirror 2, and then the collimator 3 is incident into the collimator camera 24 to form an imaging spot;

调整子光路装校工装1姿态,使得所述成像光斑位于平行光管相机24视场中心位置,完成所述卡式天线14与平行光管3的光轴校准;Adjust the posture of the sub-optical path installation and calibration tooling 1 so that the imaging spot is located at the center of the field of view of the collimator camera 24, and complete the optical axis calibration of the cassette antenna 14 and the collimator 3;

对子光路13内部结构进行装校。The internal structure of the sub-optical path 13 is adjusted.

本发明解决了现有自准直动态靶标装校难度大的问题。具体有益效果包括:The invention solves the problem that the existing self-collimating dynamic target is difficult to install and calibrate. Specific beneficial effects include:

1、本发明使用双经纬仪来实现导向镜和子光路的同轴装校,与现有技术相比较,不需要通过不断的移动平行光管来保证光轴一致性的操作,本发明中采用双经纬仪的相互配合来保证二者光轴一致性的装校,提高了装校效率。1. The present invention uses double theodolites to realize the coaxial alignment of the guide mirror and the sub-optical paths. Compared with the prior art, it does not need to continuously move the collimator to ensure the consistency of the optical axis. Double theodolites are used in the present invention Cooperate with each other to ensure the installation and calibration of the consistency of the optical axes of the two, which improves the efficiency of installation and calibration.

2、按照本发明提出的自准直动态靶标的双经纬仪装校方法进行操作,只需要双经纬仪进行校准,且其中一个经纬仪的转动角度已确定,大大降低了对操作者的技术要求,提高了操作效率,同时有效避免了由于装校操作人员专业技能不熟练而影响装校效率及准确性。2. Operate according to the double theodolite installation and calibration method of the self-collimating dynamic target proposed by the present invention, only need double theodolite to calibrate, and the rotation angle of one of the theodolites has been determined, which greatly reduces the technical requirements for the operator and improves the At the same time, it effectively avoids the impact on the efficiency and accuracy of the installation and calibration due to the unskilled professional skills of the installation and calibration operators.

本发明适用于对自准直动态靶标的装校操作,可以应用于自准直动态靶标的加工制造技术领域中,也可以应用于自准直动态靶标的试验测试技术领域中。The invention is applicable to the installation and calibration operation of the self-collimating dynamic target, can be applied to the technical field of processing and manufacturing of the self-collimating dynamic target, and can also be applied to the technical field of experiment testing of the self-collimating dynamic target.

附图说明Description of drawings

本发明上述的和/或附加的方面和优点从下面结合附图对实施例的描述中将变得明显和容易理解,其中:The above and/or additional aspects and advantages of the present invention will become apparent and easy to understand from the following description of the embodiments in conjunction with the accompanying drawings, wherein:

图1为本发明所述的基于双经纬仪的自准直动态靶标光学装校方法的示意图。Fig. 1 is a schematic diagram of the self-collimation dynamic target optical alignment method based on double theodolite according to the present invention.

图2为实施方式一所述的子光路装校方法示意图。FIG. 2 is a schematic diagram of the sub-optical path alignment method described in the first embodiment.

图3为实施方式八所述的子光路13内部结构示意图。FIG. 3 is a schematic diagram of the internal structure of the sub-optical path 13 described in the eighth embodiment.

图4为实施方式八所述的子光路13的光路图。FIG. 4 is an optical path diagram of the sub-optical path 13 described in the eighth embodiment.

图中:子光路装校工装1、基准反射镜2、平行光管3、水平安装平台4、子光路13、卡式天线14、旋转光轴15、测试基准反射镜16、第一经纬仪17、摇臂18、第二导向镜19、第二经纬仪20、第一导向镜21、子光路安装板22、平行管相机24、旋转光轴中测试基准反射镜安装凸台25、自准直动态靶标装校工装26。In the figure: sub-optical path installation and calibration tooling 1, reference mirror 2, collimator 3, horizontal installation platform 4, sub-optical path 13, card antenna 14, rotating optical axis 15, test reference mirror 16, first theodolite 17, Rocker arm 18, second guiding mirror 19, second theodolite 20, first guiding mirror 21, sub-optical path mounting plate 22, parallel tube camera 24, test reference mirror mounting boss 25 in the rotating optical axis, and self-collimating dynamic target School tooling 26.

子光路13包括:激光接收相机5、激光接收镜头6、激光接收反射镜7、分光镜8、偏摆镜9、红外分光镜10、激光发射单元11、红外发射单元12、子光路安装框架23。The sub-optical path 13 includes: a laser receiving camera 5, a laser receiving lens 6, a laser receiving mirror 7, a beam splitter 8, a deflection mirror 9, an infrared beam splitter 10, a laser emitting unit 11, an infrared emitting unit 12, and a sub-optical path installation frame 23 .

具体实施方式Detailed ways

下面结合附图将对本发明的多种实施方式进行清楚、完整地描述。通过参考附图描述的实施例是示例性的,旨在用于解释本发明,而不能理解为对本发明的限制。Various embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. The embodiments described by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention.

实施方式一.参见图1和图2说明本实施方式。本实施方式所述的是一种基于双经纬仪的自准直动态靶标光学装校方法是采用双经纬仪实现自准直动态靶的导光镜和子光路的同轴装校,所述装校方法包括:Embodiment 1. Refer to FIG. 1 and FIG. 2 to illustrate this embodiment. What this embodiment describes is a kind of self-collimating dynamic target optical calibration method based on double theodolite, which is to use double theodolite to realize the coaxial calibration of the light guide mirror and the sub-optical path of the self-collimating dynamic target. The calibration method includes :

步骤一、通过自准直动态靶标装校工装26固定旋转光轴15,采用第一经纬仪17结合测试基准反射镜16完成测试基准反射镜16与旋转光轴15的光轴一致性装校,此时第一经纬仪17的姿态为A;Step 1. Fix the rotating optical axis 15 through the self-collimating dynamic target installation and calibration tool 26, and use the first theodolite 17 in combination with the test reference mirror 16 to complete the calibration of the optical axis consistency between the test reference mirror 16 and the rotating optical axis 15. The attitude of the first theodolite 17 is A;

步骤二、调整第一经纬仪17旋转45°变成姿态C;调整确定第二经纬仪20的位置和初始姿态B;Step 2, adjust the first theodolite 17 to rotate 45 ° and become attitude C; adjust and determine the position and initial attitude B of the second theodolite 20;

步骤三、安装第一导光镜21,通过第二经纬仪20调整所述第一导光镜21的姿态,对所述第一导光镜21与旋转光轴15的夹角的校准,完成所述第一导光镜21的装校;此时所述第二经纬仪的姿态为D;Step 3, install the first light guide mirror 21, adjust the posture of the first light guide mirror 21 through the second theodolite 20, and calibrate the angle between the first light guide mirror 21 and the rotating optical axis 15, and complete the Describe the adornment calibration of the first light guide mirror 21; Now the attitude of the second theodolite is D;

步骤四、拆下所述第一导向镜21和测试基准反射镜16;Step 4, remove the first guide mirror 21 and the test reference mirror 16;

步骤五、将子光路13及卡式天线14整体安装到回转光轴15的左端,调整第一经纬仪17的姿态恢复到姿态A,通过所述第一经纬仪17校准子光路13和卡式天线14的姿态,完成子光路13和卡式天线14的装校;Step five, install the sub-optical path 13 and the cassette antenna 14 as a whole on the left end of the rotating optical axis 15, adjust the posture of the first theodolite 17 to return to posture A, and calibrate the sub-optical path 13 and the cassette antenna 14 through the first theodolite 17 attitude, complete the installation of the sub-optical path 13 and the card antenna 14;

步骤六、取下基准反射镜2;将第一导向镜21安装到原来位置,并通过安装定位销固定;Step 6, remove the reference mirror 2; install the first guide mirror 21 to the original position, and fix it by installing the positioning pin;

步骤七、安装第二导光镜19,通过第一经纬仪17结合第二经纬仪20调整第二导光镜19的姿态,完成所述第二导光镜19的装校。Step 7: Install the second light guide mirror 19 , adjust the posture of the second light guide mirror 19 through the first theodolite 17 and the second theodolite 20 , and complete the installation and calibration of the second light guide mirror 19 .

本实施方式所装校的自准直动态靶标结构参见图1所示:子光路13通过子光路安装板22与卡式天线14固定连接,所述卡式天线14嵌入并固定在旋转光轴15内,所述旋转光轴15与摇臂18通过轴承同轴连接,轴承内圈和旋转光轴外圈连接,轴承外圈和摇臂18内圈连接,此处为摇臂18与卡式天线14相对旋转,所述摇臂18上设置有第一导光镜安装位置和第二导光镜安装位置,分别用于固定第一导光镜21和第二导光镜19。The structure of the self-collimating dynamic target installed in this embodiment is shown in Figure 1: the sub-optical path 13 is fixedly connected to the clip-type antenna 14 through the sub-optical path mounting plate 22, and the clip-type antenna 14 is embedded and fixed on the rotating optical axis 15 Inside, the rotating optical axis 15 is coaxially connected to the rocker arm 18 through a bearing, the inner ring of the bearing is connected to the outer ring of the rotating optical axis, and the outer ring of the bearing is connected to the inner ring of the rocker arm 18, here the rocker arm 18 and the cassette antenna 14 is relatively rotated, and the rocker arm 18 is provided with a first light guide mirror installation position and a second light guide mirror installation position, which are respectively used to fix the first light guide mirror 21 and the second light guide mirror 19 .

本实施方式,采用双经纬仪(第一经纬仪17和第二经纬仪20)完成装校,所述经纬仪可以采用莱卡经纬仪。In this embodiment, a double theodolite (the first theodolite 17 and the second theodolite 20) is used to complete the calibration, and the theodolite can be a Lycra theodolite.

本实施方式中所述的子光路13及卡式天线14整体是装校之后的整体结构。所述子光路13及卡式天线14的装校采用现有方法实现即可。The sub-optical path 13 and the card antenna 14 described in this embodiment are overall structures after installation and calibration. The installation and calibration of the sub-optical path 13 and the card antenna 14 can be realized by existing methods.

本实施方式所述的装校方法,首先采用第一经纬仪完成旋转光轴15和测试基准反射镜16的光轴一致性装校,其中,测试基准反射镜16的位置即为卡式天线14中次镜的位置。然后通过第一经纬仪17来确定第二经纬仪20的位置和初始姿态B;之后,通过两个经纬仪对第一导光镜21装校,之后再对第二导光镜19进行装校。In the calibration method described in this embodiment, at first the first theodolite is used to complete the optical axis consistency calibration of the rotating optical axis 15 and the test reference reflector 16, wherein the position of the test reference reflector 16 is the position of the card antenna 14. The position of the secondary mirror. Then the position and the initial attitude B of the second theodolite 20 are determined by the first theodolite 17; after that, the first light guide mirror 21 is calibrated by the two theodolites, and then the second light guide mirror 19 is calibrated.

该方法与现有技术相比较,不需要使用平行光管、以及多次移动平行光管的操作,操作减半。Compared with the prior art, this method does not need to use the collimator and the operation of moving the collimator multiple times, and the operation is halved.

该方法中,第一经纬仪确定位置之后,只需要调整俯仰角度即可,第二经纬仪的位置是通过第一经纬仪17来确定的,操作简单、且对操作者技术技能要求低,能有效保证装校相率以及装校的精准度。In this method, after the first theodolite determines the position, it is only necessary to adjust the pitch angle, and the position of the second theodolite is determined by the first theodolite 17. The calibration rate and the accuracy of the calibration.

实施方式二.本实施方式是对实施方式一所述的一种基于双经纬仪的自准直动态靶标光学装校方法中,步骤一的实现方法的举例说明,所述步骤一包括:Embodiment two. This embodiment is an example of the implementation method of step one in a kind of self-collimating dynamic target optical calibration method based on double theodolite described in embodiment one, and described step one includes:

将旋转光轴15固定在自准直动态靶标装校工装26上;Fix the rotating optical axis 15 on the autocollimating dynamic target installation and calibration tooling 26;

在所述旋转光轴15内部设置的固定基准反射镜的凸台25上固定测试基准反射镜16;Fix the test reference mirror 16 on the boss 25 of the fixed reference mirror provided inside the rotating optical axis 15;

将第一经纬仪17置于所述旋转光轴15右侧,并保持其为水平姿态,然后,调整其位置和姿态,使得所述第一经纬仪17发射的光束经基准反射镜16反射之后再次入射至第一经纬仪17内形成成像十字光斑;Place the first theodolite 17 on the right side of the rotating optical axis 15, and keep it as a horizontal posture, then adjust its position and posture so that the light beam emitted by the first theodolite 17 is incident again after being reflected by the reference reflector 16 To form an imaging cross spot in the first theodolite 17;

控制旋转光轴15转动,直到所述第一经纬仪17中的成像十字光斑移动至与其十字线中心位置,完成基准反射镜16与旋转光轴15的光轴一致性装校;此时第一经纬仪17与测试基准反射镜16同光轴,标记此时第一经纬仪17的姿态为A,并记录所述姿态A的方位与俯仰数值。Control the rotating optical axis 15 to rotate until the imaging cross spot in the first theodolite 17 moves to the center position of its crosshairs, and complete the alignment of the optical axis of the reference mirror 16 and the rotating optical axis 15; at this time, the first theodolite 17 is on the same optical axis as the test reference reflector 16, marks the attitude of the first theodolite 17 at this time as A, and records the azimuth and elevation values of the attitude A.

实施方式三.本实施方式是对实施方式一所述的一种基于双经纬仪的自准直动态靶标光学装校方法中,步骤二的实现方法的举例说明,所述步骤二的具体方法为:Embodiment three. This embodiment is an illustration of the implementation method of step 2 in a kind of self-collimating dynamic target optical calibration method based on double theodolite described in embodiment 1, and the specific method of described step 2 is:

将所述第一经纬仪17方位旋转45°、变成姿态C,将第二经纬仪20调整其处于水平姿态,通过调整第二经纬仪20的位置、姿态,使第一经纬仪17发射的光束入射至第二经纬仪20中并形成成像十字光斑、并使得所述成像十字光斑移动至所述第二经纬仪20的十字线中心位置,此时第二经纬仪20姿态为初始姿态B,并记录该姿态下的方位与俯仰数值。The first theodolite 17 azimuth is rotated 45 °, becomes attitude C, the second theodolite 20 is adjusted it is in horizontal attitude, by adjusting the position, the attitude of the second theodolite 20, the light beam that the first theodolite 17 is launched is incident on the second theodolite In the second theodolite 20, an imaging cross spot is formed, and the imaging cross spot is moved to the crosshair center position of the second theodolite 20. At this moment, the attitude of the second theodolite 20 is the initial attitude B, and the orientation under the attitude is recorded. and pitch values.

实施方式四.本实施方式是对实施方式一所述的一种基于双经纬仪的自准直动态靶标光学装校方法中,步骤三的实现方法的举例说明,所述步骤三的具体方法为:Embodiment 4. This embodiment is an illustration of the implementation method of step 3 in a kind of self-collimating dynamic target optical calibration method based on double theodolite described in embodiment 1, and the specific method of described step 3 is:

调整第二经纬仪20的方位旋转45°、使其指向第一导向镜21的安装位置;Adjust the azimuth rotation of the second theodolite 20 for 45° so that it points to the installation position of the first guide mirror 21;

在所述第一导向镜安装位置安装第一导向镜21;installing a first guide mirror 21 at the installation position of the first guide mirror;

控制第二经纬仪20发射光束,使得所述发射光束经所述第一导向镜21反射的光束入射至所述第二经纬仪20形成成像十字光斑,调整所述第一导向镜21的姿态,直到所述十字光斑移动至所述第二经纬仪20的中心十字线中心位置,完成第一导向镜21与旋转光轴15夹角的校准;此时,第一导向镜21的姿态D,此时,所述第一导向镜21与旋转光轴15的夹角为45°,该姿态能够有效保证复位时的定位精度。Control the second theodolite 20 to emit light beams, so that the light beams reflected by the first theodolite 21 of the emitted light beams are incident on the second theodolite 20 to form an imaging cross spot, and adjust the attitude of the first guide mirror 21 until the The cross spot moves to the central position of the cross line of the second theodolite 20 to complete the calibration of the angle between the first guide mirror 21 and the rotating optical axis 15; at this time, the posture D of the first guide mirror 21, at this time, the The included angle between the first guiding mirror 21 and the rotating optical axis 15 is 45°, and this attitude can effectively ensure the positioning accuracy during reset.

第二经纬仪20发射光输的光程为:所发射光束入射至第一导向镜21、被反射至测试基准反射镜16,经该测试基准反射镜16反射之后再次入射至第一导向镜21、经该第一导向镜21反射之后入射至第二经纬仪20。The optical path of the second theodolite 20 emitting light output is: the emitted light beam is incident on the first guide mirror 21, is reflected to the test reference reflector 16, and is incident on the first guide mirror 21 again after the test reference reflector 16 is reflected. After being reflected by the first guide mirror 21, it enters the second theodolite 20 .

实施方式五.本实施方式是对实施方式一所述的一种基于双经纬仪的自准直动态靶标光学装校方法中,步骤五的实现方法的举例说明,所述步骤五的具体方法为:Embodiment five. This embodiment is an illustration of the implementation method of step five in a kind of self-collimating dynamic target optical correction method based on double theodolite described in embodiment one, and the specific method of described step five is:

将子光路13及卡式天线14整体安装到回转光轴15的左端,此时所述卡式天线14次镜背部装有基准反射镜2,所述基准反射镜2与测试基准反射镜16的位置不相同,基准反射镜2安装在卡式天线次镜背部预留位置处,旋转光轴15内部有桁架结构,桁架结构中心有安装测试基准反射镜16的安装凸台25;The sub-optical path 13 and the card antenna 14 are integrally installed on the left end of the optical axis of rotation 15. At this time, the reference reflector 2 is installed on the back of the 14 secondary mirrors of the card antenna, and the reference reflector 2 and the test reference reflector 16 The positions are different. The reference reflector 2 is installed at the reserved position on the back of the card-type antenna secondary mirror. There is a truss structure inside the rotating optical axis 15. In the center of the truss structure, there is a mounting boss 25 for installing the test reference reflector 16;

将第一经纬仪17的姿态调整成姿态A,然后发出光束,使所述光束经卡式天线14上的基准反射镜2反射、并在所述第一经纬仪17中形成成像十字光斑;The attitude of the first theodolite 17 is adjusted to attitude A, and then the light beam is sent, and the light beam is reflected by the reference reflector 2 on the card antenna 14, and the imaging cross spot is formed in the first theodolite 17;

通过调整子光路13及卡式天线14整体姿态,直到所述成像十字光斑移动到所述第一经纬仪17的十字线中心位置,此时子光路13光轴与经纬仪17光轴重合,实现子光路的光轴与旋转轴的光轴校准,完成子光路13和卡式天线14的装校。By adjusting the overall posture of the sub-optical path 13 and the card antenna 14, until the imaging cross spot moves to the center position of the crosshairs of the first theodolite 17, the optical axis of the sub-optical path 13 coincides with the optical axis of theodolite 17 to realize the sub-optical path The optical axis of the optical axis and the optical axis of the rotating shaft are calibrated, and the assembly of the sub-optical path 13 and the card antenna 14 is completed.

实施方式六.本实施方式是对实施方式一所述的一种基于双经纬仪的自准直动态靶标光学装校方法中,步骤七的实现方法的举例说明,所述步骤七的具体方法为:Embodiment six. This embodiment is an illustration of the implementation method of step seven in a kind of self-collimating dynamic target optical calibration method based on double theodolite described in embodiment one, and the specific method of described step seven is:

取下基准反射镜2,将第二导向镜19安装在所述摇臂18的第一导向镜的安装位置;Take off the reference reflector 2, and install the second guide mirror 19 at the installation position of the first guide mirror of the rocker arm 18;

将第一经纬仪17旋转60°变成姿态F;The first theodolite 17 is rotated 60 ° and becomes posture F;

调整第二经纬仪20的姿态,使得所述第二经纬仪20接收到的成像十字光斑位于所述第二经纬仪20的十字线中心位置,此时,第二经纬仪20的位置和姿态为E;Adjust the posture of the second theodolite 20, so that the imaging cross spot that the second theodolite 20 receives is located at the crosshair center position of the second theodolite 20, at this moment, the position and the posture of the second theodolite 20 are E;

将所述第二经纬仪20的角度旋转120°变成姿态H,使其发射的光束对准第二导向镜19;Rotate the angle of the second theodolite 20 by 120° to become attitude H, so that the light beam it emits is aimed at the second guide mirror 19;

子光路13发射光束,所述光束经第一导向镜21反射后发射至第二导向镜19,经所述第二导向镜19反射后入射至第二经纬仪20,在所述第二经纬仪20内形成成像十字光斑;The sub-optical path 13 emits light beams, and the light beams are reflected by the first guide mirror 21 and then sent to the second guide mirror 19, and then incident on the second theodolite 20 after being reflected by the second guide mirror 19, in the second theodolite 20 Form an imaging cross spot;

调整第二导向镜19的姿态、使得所述成像十字光斑移动至第二经纬仪20中的十字线中心位置,此时,表明所述第二导向镜19与旋转光轴15的夹角为45°,通过定位销固定第二导向镜19,完成所述第二导光镜19的装校。Adjust the posture of the second guide mirror 19 so that the imaging cross spot moves to the center position of the crosshairs in the second theodolite 20. At this time, it shows that the angle between the second guide mirror 19 and the rotating optical axis 15 is 45° , the second guide mirror 19 is fixed by positioning pins, and the installation and calibration of the second light guide mirror 19 is completed.

实施方式七.本实施方式是对实施方式一所述的一种基于双经纬仪的自准直动态靶标光学装校方法中,所述子光路13和卡式天线14固定在一起形成一个整体,所述整体采用现有装校方法实现即可。本实施方式给出一种装校方法:Embodiment 7. This embodiment is a kind of self-collimating dynamic target optical calibration method based on double theodolite described in Embodiment 1. The sub-optical path 13 and the card antenna 14 are fixed together to form a whole, so Said whole can be realized by adopting the existing installation method. This embodiment provides a kind of calibration method:

将自准直动态靶标子光路13和卡式天线14通过子光路安装板固定连接之后,固定在子光路装校工装1上,所述装校工装1固定于水平光学平台4上;After the self-collimating dynamic target sub-optical path 13 and the card antenna 14 are fixedly connected through the sub-optical path mounting plate, they are fixed on the sub-optical path installation and calibration tool 1, and the installation and calibration tool 1 is fixed on the horizontal optical platform 4;

安装基准反射镜2于卡式光学天线14次镜预留位置处;Install the reference reflector 2 at the position reserved for the 14th secondary mirror of the card-type optical antenna;

控制平行光管3发射光束入射至基准反射镜2,并经所述基准反射镜2反射回平行光管3,并所述平行光管3之后入射至平行管相机24中形成成像光斑;Control the collimator 3 to emit light beams to enter the reference mirror 2, and reflect back to the collimator 3 through the reference mirror 2, and then the collimator 3 is incident into the collimator camera 24 to form an imaging spot;

调整子光路装校工装1姿态,使得所述成像光斑位于平行光管相机24视场中心位置,此时卡式天线14与平行光管3的光轴重合,完成所述卡式天线14与平行光管3的光轴校准;Adjust the posture of the sub-optical path installation and calibration tooling 1 so that the imaging spot is located at the center of the field of view of the collimator camera 24. At this time, the card antenna 14 coincides with the optical axis of the collimator 3, and the card antenna 14 is aligned with the parallel beam. Optical axis calibration of light pipe 3;

对子光路13内部结构进行装校。The internal structure of the sub-optical path 13 is adjusted.

所述平行光管3发射的光束可以采用可见光实现,例如:采用波长为600nm的光束,采用可见光的光束更方便在装校过程中对光路的观察。The light beam emitted by the collimator 3 can be realized by using visible light, for example: using a light beam with a wavelength of 600nm, which is more convenient to observe the optical path during the installation and calibration process.

所述平行光管可以采用为多焦面平行光管。The collimator can be adopted as a multi-focal plane collimator.

实施方式八.本实施方式是对实施方式七所述的一种基于双经纬仪的自准直动态靶标光学装校方法中,对子光路13内部结构进行装校的方法的举例说明,所述方法为:Embodiment 8. This embodiment is an example of the method for adjusting the internal structure of the sub-optical path 13 in a kind of self-collimation dynamic target optical adjustment method based on double theodolite described in Embodiment 7. The method for:

分别调整激光接收反射镜7与分光镜8的姿态,使得平行光管3发射的光束在到达所述激光接收反射镜7与分光镜8时,均位于镜片中心位置;Adjust the postures of the laser receiving reflector 7 and the beam splitter 8 respectively, so that the light beam emitted by the collimator 3 is located at the center of the lens when reaching the laser receiving reflector 7 and the beam splitter 8;

安装偏摆镜9与红外分光镜10,分别调整二者的姿态,使得平行光管3发射的光束在分别到达所述安装偏摆镜9与红外分光镜10时均处于镜片中心位置;Install the yaw mirror 9 and the infrared beam splitter 10, and adjust the postures of the two respectively, so that the light beams emitted by the collimator 3 are all in the center of the lens when they respectively arrive at the installed yaw mirror 9 and the infrared beam splitter 10;

对激光接收单元整体进行装校,确定所述激光接收单元整体的姿态;Assembling and calibrating the laser receiving unit as a whole, and determining the attitude of the laser receiving unit as a whole;

安装红外发射单元12,调整所述红外发射单元12的姿态以及其与红外分光镜10的整体姿态,完成红外发射单元12和红外分光镜10的装校;Install the infrared emitting unit 12, adjust the posture of the infrared emitting unit 12 and its overall posture with the infrared beam splitter 10, and complete the installation of the infrared emitting unit 12 and the infrared beam splitter 10;

安装并调整激光发射单元11的姿态,进行装校,完成子光路13内部的装校;Install and adjust the attitude of the laser emitting unit 11, perform calibration, and complete the calibration inside the sub-optical path 13;

所述调整激光发射单元11的姿态的过程为:调整其姿态,使得其发射光束经过子光路13与卡式天线14入射至平行光管相机24内形成成像光斑位于所述平行光管相机24视场中心位置,完成姿态调整。The process of adjusting the attitude of the laser emitting unit 11 is: adjust its attitude so that its emitted light beam passes through the sub-optical path 13 and the card antenna 14 and enters the collimator camera 24 to form an imaging spot located in the field of view of the collimator camera 24. The center position of the field to complete the attitude adjustment.

本实施方式所述的子光路的结构参见图3和图4所示,激光发射单元11发射光束至红外分光镜10的一侧,红外发射单元12发射红外光束至所述红外分光镜10的另一侧,所述激光发射单元11发射光束至红外分光镜10后、经该红外分光镜10透射的光束与经该红外分光镜10折射的红外光束形成一束光发射至偏摆镜9,所述偏摆镜9将入射光反射后发送给分光镜8,经所述分光镜8反射的光束发送给激光接收反射镜7,经所述激光接收反射镜7反射的光束发送至激光接收相机5,在所述激光接收相机5中成像,经所述分光镜8透射的光束后发送给卡式天线14。The structure of the sub-optical path described in this embodiment is shown in FIGS. On one side, after the laser emitting unit 11 transmits the light beam to the infrared beam splitter 10, the light beam transmitted by the infrared beam splitter 10 and the infrared beam refracted by the infrared beam splitter 10 form a beam of light that is emitted to the swing mirror 9, so The deflection mirror 9 reflects the incident light and sends it to the beam splitter 8, the beam reflected by the beam splitter 8 is sent to the laser receiving mirror 7, and the beam reflected by the laser receiving mirror 7 is sent to the laser receiving camera 5 , imaged in the laser receiving camera 5 , and the light beam transmitted by the beam splitter 8 is sent to the card antenna 14 .

上述激光接收相机5、激光接收反射镜7、分光镜8、偏摆镜9、红外分光镜10、激光发射单元11和红外发射单元12均固定在安装框架23上,其中激光接收相机5的激光接收镜头6朝向激光接收反射镜7的反射面。The above-mentioned laser receiving camera 5, laser receiving reflector 7, beam splitter 8, deflection mirror 9, infrared beam splitter 10, laser emitting unit 11 and infrared emitting unit 12 are all fixed on the mounting frame 23, wherein the laser receiving camera 5 The receiving lens 6 faces the reflection surface of the laser receiving mirror 7 .

实施方式九.本实施方式是对实施方式八所述的一种基于双经纬仪的自准直动态靶标光学装校方法中步骤的举例说明,本实施方式中所述的对激光接收单元整体进行装校方法为:Embodiment 9. This embodiment is an example of the steps in the method of self-collimating dynamic target optical installation based on double theodolite described in Embodiment 8. The overall assembly of the laser receiving unit described in this embodiment The school method is:

调整所述激光接收单元整体的姿态,使所述平行光管3出射的光束的在激光接收相机5中的成像光斑位于视场中心位置;Adjust the overall posture of the laser receiving unit so that the imaging spot of the light beam emitted by the collimator 3 in the laser receiving camera 5 is located at the center of the field of view;

调整所述激光接收相机5的焦面,使其与激光接收镜头6的镜头焦面重合,即完成激光接收单元的装校。Adjust the focal plane of the laser receiving camera 5 so that it coincides with the lens focal plane of the laser receiving lens 6, that is, complete the calibration of the laser receiving unit.

实施方式十.本实施方式是对实施方式八所述的一种基于双经纬仪的自准直动态靶标光学装校方法中步骤的举例说明,本实施方式中,所述红外发射单元12和红外分光镜10的装校方法为:Embodiment 10. This embodiment is an illustration of the steps in a self-collimating dynamic target optical calibration method based on a double theodolite described in Embodiment 8. In this embodiment, the infrared emitting unit 12 and the infrared spectroscopic The calibration method of mirror 10 is as follows:

调整所述红外发射单元12的姿态,使得其发射的光束在平行光管相机24中形成成像光斑,保持所述红外发射单元12与红外分光镜10的相对位置不变;Adjust the posture of the infrared emitting unit 12 so that the beam it emits forms an imaging spot in the collimator camera 24, keeping the relative position of the infrared emitting unit 12 and the infrared beam splitter 10 constant;

调整红外发射单元12与红外分光镜10整体姿态,使得所述成像光斑移动到平行光管相机24视场中心位置,完成红外发射单元12与红外分光镜10的装校。Adjust the overall posture of the infrared emitting unit 12 and the infrared beam splitter 10, so that the imaging spot moves to the center of the field of view of the collimator camera 24, and complete the installation and calibration of the infrared emitting unit 12 and the infrared beam splitter 10.

Claims (5)

1. The method is characterized in that the method adopts the double theodolites to realize the coaxial alignment of the guide mirror and the sub-optical path of the auto-collimation dynamic target, and the alignment method comprises the following steps:
fixing a rotating optical axis (15) through an auto-collimation dynamic target calibration tool (26), and completing optical axis consistency calibration of a test reference reflector (16) and the rotating optical axis (15) by adopting a first theodolite (17) in combination with the test reference reflector (16), wherein the posture of the first theodolite (17) is A;
step two, adjusting the first theodolite (17) to rotate 45 degrees to change the attitude C; adjusting and determining the position and initial attitude B of the second theodolite (20);
step three, installing a first guide mirror (21), adjusting the gesture of the first guide mirror (21) through a second theodolite (20), and calibrating the included angle between the first guide mirror (21) and a rotating optical axis (15), thereby completing the installation and calibration of the first guide mirror (21); the second theodolite (20) has a posture D at this time;
step four, detaching the first guide mirror (21) and the test reference mirror (16);
fifthly, integrally mounting the sub-optical path (13) and the card antenna (14) at the left end of the rotating optical axis (15), adjusting the posture of the first theodolite (17) to be recovered to the posture A, and calibrating the postures of the sub-optical path (13) and the card antenna (14) through the first theodolite (17) to finish the assembly and calibration of the sub-optical path (13) and the card antenna (14);
step six, taking down the reference reflector (2); the first guide mirror (21) is installed to an original position and fixed through an installation positioning pin;
step seven, installing a second guide mirror (19), and adjusting the posture of the second guide mirror (19) through the combination of the first theodolite (17) and the second theodolite (20), so as to finish the installation and calibration of the second guide mirror (19);
the specific method of the first step is as follows:
fixing the rotating optical axis (15) on an auto-collimation dynamic target assembling and calibrating tool (26);
a test reference mirror (16) is fixed on a boss (25) of the fixed test reference mirror (16) arranged inside the rotating optical axis (15);
the first theodolite (17) is arranged on the right side of the rotating optical axis (15) and kept in a horizontal posture, and then the position and the posture of the first theodolite are adjusted so that a light beam emitted by the first theodolite (17) is reflected by the test reference reflector (16) and then is incident into the first theodolite (17) again to form an imaging cross light spot;
controlling the rotation of the rotating optical axis (15) until an imaging cross light spot in the first theodolite (17) moves to the center position of a cross line of the imaging cross light spot, and completing the optical axis consistency calibration of the test reference reflector (16) and the rotating optical axis (15); marking the attitude of the first theodolite (17) at the moment as A, and recording the azimuth and pitching values of the attitude A;
the specific method of the second step is as follows:
the azimuth of the first theodolite (17) is rotated 45 degrees to form an attitude C, the second theodolite (20) is adjusted to be in a horizontal attitude, the light emitted by the first theodolite (17) enters the second theodolite (20) and forms an imaging cross light spot by adjusting the position and the attitude of the second theodolite (20), the imaging cross light spot is moved to the center position of a cross line of the second theodolite (20), and at the moment, the attitude of the second theodolite (20) is an initial attitude B, and the azimuth and pitching values under the attitude are recorded;
the specific method of the third step is as follows:
adjusting the azimuth rotation of the second theodolite (20) by 45 degrees to lead the second theodolite to point to the installation position of the first guide mirror (21);
-mounting a first guiding mirror (21) at the mounting position;
controlling the second theodolite (20) to emit light beams, enabling the light beams reflected by the first guide mirror (21) to be incident to the second theodolite (20) to form imaging cross light spots, adjusting the gesture of the first guide mirror (21) until the cross light spots move to the center position of a center cross line of the second theodolite (20), and completing the calibration of the included angle between the first guide mirror (21) and the rotating optical axis (15); at this time, the posture D of the first guide mirror (21);
the specific method of the fifth step is as follows:
integrally mounting the sub-optical path (13) and the card antenna (14) to the left end of the rotating optical axis (15);
the attitude of a first theodolite (17) is adjusted to be an attitude A, and then a light beam is emitted, so that the light beam is reflected by a reference reflector (2) on a card antenna (14) and an imaging cross light spot is formed in the first theodolite (17);
the integral postures of the sub-optical path (13) and the clamp antenna (14) are adjusted until the imaging cross light spot moves to the center position of the cross line of the first theodolite (17), so that the optical axis of the sub-optical path (13) is calibrated with the optical axis of the rotating optical axis (15), and the assembly and calibration of the sub-optical path (13) are completed;
the specific method of the step seven is as follows:
the reference reflector (2) is taken down, and the second guide mirror (19) is arranged at the mounting position of the first guide mirror of the rocker arm (18);
rotating the first theodolite (17) by 60 degrees to become a posture F;
adjusting the posture of a second theodolite (20) so that an imaging cross light spot received by the second theodolite (20) is positioned at the center of a cross line of the second theodolite (20), and at the moment, the position and the posture of the second theodolite (20) are E;
rotating the angle of the second theodolite (20) by 120 degrees to form a posture H, so that the emitted light beam is aligned with a second guide mirror (19);
the sub-optical path (13) emits a light beam, the light beam is reflected by the first guide mirror (21) and then emitted to the second guide mirror (19), the light beam is reflected by the second guide mirror (19) and then enters the second theodolite (20), and an imaging cross light spot is formed in the second theodolite (20);
and adjusting the posture of the second guide mirror (19) to enable the imaging cross light spot to move to the center position of a cross line in the second theodolite (20), and fixing the second guide mirror (19) through a locating pin to finish the assembly and calibration of the second guide mirror (19).
2. A method of auto-collimation dynamic target optical calibration based on dual theodolites according to claim 1, characterized in that the sub-optical path (13) and the card antenna (14) are fixed together to form a whole, said whole being calibrated by the following method:
integrally mounting an auto-collimation dynamic target sub-optical path (13) and a card antenna (14) on a sub-optical path calibration tool (1), wherein the calibration tool (1) is fixed on a horizontal optical platform (4);
installing a reference reflector (2) at a reserved position of a secondary mirror of the card antenna (14);
controlling the collimator (3) to emit light beams to be incident to the reference reflector (2), reflecting the light beams back to the collimator (3) through the reference reflector (2), and then entering the collimator (3) to the collimator camera (24) to form imaging light spots;
adjusting the posture of the sub-optical path assembling and correcting tool (1) to enable the imaging light spot to be located at the center of the view field of the collimator camera (24), and finishing the optical axis calibration of the card type antenna (14) and the collimator (3);
and (3) carrying out assembly correction on the internal structure of the sub-optical path (13).
3. The method for calibrating the auto-collimation dynamic target optical based on the double theodolites according to claim 2, wherein the method for calibrating the internal structure of the sub-optical path (13) is as follows:
the postures of the laser receiving reflector (7) and the spectroscope (8) are respectively adjusted, so that light beams emitted by the collimator (3) are respectively positioned at the central positions of the laser receiving reflector (7) and the spectroscope (8);
the method comprises the steps of installing a deflection mirror (9) and an infrared spectroscope (10), and respectively adjusting the postures of the deflection mirror and the infrared spectroscope, so that light beams emitted by a collimator (3) are positioned in the center of a lens when reaching the installation deflection mirror (9) and the infrared spectroscope (10) respectively;
assembling and correcting the whole laser receiving unit, and determining the posture of the whole laser receiving unit;
installing an infrared emission unit (12), adjusting the posture of the infrared emission unit (12) and the integral posture of the infrared emission unit and an infrared spectroscope (10), and finishing the assembly and calibration of the infrared emission unit (12) and the infrared spectroscope (10);
installing and adjusting the posture of the laser emission unit (11), and performing assembling and calibrating to finish assembling and calibrating the inside of the sub-optical path (13); the process for adjusting the posture of the laser emission unit (11) comprises the following steps: the posture of the collimator is adjusted so that the emitted light beam is incident into the collimator camera (24) through the sub-light path (13) and the card antenna (14) to form an imaging light spot which is positioned at the center of the field of view of the collimator camera (24), and the posture adjustment is completed.
4. The method for calibrating the auto-collimation dynamic target optics based on the dual theodolites according to claim 3, wherein the method for calibrating the whole laser receiving unit is as follows:
adjusting the integral posture of the laser receiving unit to enable an imaging facula of a light beam emitted by the collimator (3) in the laser receiving camera (5) to be positioned at the center of a field of view;
and adjusting the focal plane of the laser receiving camera (5) to enable the focal plane to coincide with the lens focal plane of the laser receiving lens (6), and thus completing the assembly and calibration of the laser receiving unit.
5. A method for calibrating an auto-collimation dynamic target optical system based on a dual theodolite according to claim 3, wherein the method for calibrating the infrared emission unit (12) and the infrared spectroscope (10) comprises the following steps:
adjusting the posture of the infrared emission unit (12) so that the emitted light beam forms an imaging light spot in the collimator camera (24), and keeping the relative position of the infrared emission unit (12) and the infrared spectroscope (10) unchanged;
and adjusting the integral postures of the infrared emission unit (12) and the infrared spectroscope (10) to enable the imaging light spot to move to the center position of the view field of the collimator camera (24), and completing the assembly and calibration of the infrared emission unit (12) and the infrared spectroscope (10).
CN202210431438.XA 2022-04-23 2022-04-23 Optical calibration method of autocollimating dynamic target based on double theodolite Active CN114967022B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202210431438.XA CN114967022B (en) 2022-04-23 2022-04-23 Optical calibration method of autocollimating dynamic target based on double theodolite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202210431438.XA CN114967022B (en) 2022-04-23 2022-04-23 Optical calibration method of autocollimating dynamic target based on double theodolite

Publications (2)

Publication Number Publication Date
CN114967022A CN114967022A (en) 2022-08-30
CN114967022B true CN114967022B (en) 2023-08-22

Family

ID=82979417

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202210431438.XA Active CN114967022B (en) 2022-04-23 2022-04-23 Optical calibration method of autocollimating dynamic target based on double theodolite

Country Status (1)

Country Link
CN (1) CN114967022B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115356089B (en) * 2022-10-21 2022-12-27 长春理工大学 Image quality detection device, method, apparatus and medium for optical system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0386925A (en) * 1989-08-29 1991-04-11 Asahi Optical Co Ltd Optical axis aligning method and jig for optical system for optical information recording and reproducing device
CN103063227A (en) * 2012-12-25 2013-04-24 中国科学院长春光学精密机械与物理研究所 Pointing device assisting in light path butt joint of theodolite and target and light path butt joint method
CN106247998A (en) * 2016-08-16 2016-12-21 江苏北方湖光光电有限公司 A kind of laser axis and the calibration method of reflecting mirror normal parallel
CN110595280A (en) * 2019-09-18 2019-12-20 中国科学院合肥物质科学研究院 A high-efficiency target calibration mirror axis consistency verification device and method
CN111083470A (en) * 2019-12-30 2020-04-28 中国科学院西安光学精密机械研究所 Array camera visual axis adjusting device and adjusting method
CN114266807A (en) * 2021-12-06 2022-04-01 长春理工大学 Detection method and system for device with tracking and pointing function

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0386925A (en) * 1989-08-29 1991-04-11 Asahi Optical Co Ltd Optical axis aligning method and jig for optical system for optical information recording and reproducing device
CN103063227A (en) * 2012-12-25 2013-04-24 中国科学院长春光学精密机械与物理研究所 Pointing device assisting in light path butt joint of theodolite and target and light path butt joint method
CN106247998A (en) * 2016-08-16 2016-12-21 江苏北方湖光光电有限公司 A kind of laser axis and the calibration method of reflecting mirror normal parallel
CN110595280A (en) * 2019-09-18 2019-12-20 中国科学院合肥物质科学研究院 A high-efficiency target calibration mirror axis consistency verification device and method
CN111083470A (en) * 2019-12-30 2020-04-28 中国科学院西安光学精密机械研究所 Array camera visual axis adjusting device and adjusting method
CN114266807A (en) * 2021-12-06 2022-04-01 长春理工大学 Detection method and system for device with tracking and pointing function

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
红外跟踪测量系统动态精度偏置检测方法研究;李桂芝;郑重;吕瑶;钟辉;;红外技术(第07期);561-564 *

Also Published As

Publication number Publication date
CN114967022A (en) 2022-08-30

Similar Documents

Publication Publication Date Title
CN109787686B (en) A satellite optical communication terminal on-orbit calibration and transceiver coaxiality correction device and method
CN104142579B (en) A kind of prestige formula of diving is caught and is debug method with mechanism's speculum
CN105157578B (en) System and method for measuring off-axis quantity and off-axis angle of off-axis paraboloid main reflector
CN110554512B (en) High-precision secondary off-axis ellipsoid mirror optical axis extraction method and optical system
CN112526489B (en) Optical axis calibration system and method of laser range finder and laser parameter measurement method
CN104048620B (en) A kind of Radio Telescope Antenna face shape absolute calibration apparatus and method
CN111006855B (en) Method and device for calibrating optical axis of large-caliber off-axis reflective vacuum parallel light tube
CN111982467B (en) Device and method for aligning the optical axis of the collimator with the optical axis of the optomechanical system in the stray light test
CN111811782A (en) A detection device and method for a space debris ranging imaging composite optical system
CN109100733A (en) Laser radar apparatus error detecting facility, method and device
CN112596258A (en) Debugging method for two-dimensional turntable folded optical assembly
CN108955537A (en) System and method capable of realizing accurate measurement of high and low point positions of off-axis reflector
CN208833907U (en) Lidar equipment error detection equipment
CN114967022B (en) Optical calibration method of autocollimating dynamic target based on double theodolite
CN106066239A (en) Detection device and method is debug at large telescope scene based on guiding
CN207439442U (en) A kind of laser pick-off emission element commissioning device
CN104748945B (en) System and method for detecting optical axis pointing consistency of corner reflector or corner reflector array
CN114279687B (en) Measuring device and measuring method for relative deflection of primary mirror and secondary mirror
CN112129319A (en) Incident optical axis calibration method of satellite-borne double-grating modulation type imaging instrument
CN112532969B (en) Adjustable focal plane assembly position calibration method for collimator
CN114266807A (en) Detection method and system for device with tracking and pointing function
CN110824459B (en) Intelligent optical axis adjustment system based on interference fringes and adjustment method thereof
CN211698179U (en) Intelligent optical axis installation and adjustment system based on interference fringes
CN112098050B (en) A system and method for testing the two-axis orthogonality of a coarse pointing mechanism
CN114264279B (en) Detection method and device for devices with tracking and variable beam angle pointing functions

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
GR01 Patent grant
GR01 Patent grant