CN112378427A - Method for establishing reference optical axis of large-caliber optical system - Google Patents

Method for establishing reference optical axis of large-caliber optical system Download PDF

Info

Publication number
CN112378427A
CN112378427A CN202110030206.9A CN202110030206A CN112378427A CN 112378427 A CN112378427 A CN 112378427A CN 202110030206 A CN202110030206 A CN 202110030206A CN 112378427 A CN112378427 A CN 112378427A
Authority
CN
China
Prior art keywords
target ball
interferometer
reticle
optical axis
optical system
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.)
Granted
Application number
CN202110030206.9A
Other languages
Chinese (zh)
Other versions
CN112378427B (en
Inventor
李金鹏
毕勇
杨永兴
王鑫蕊
赖新华
潘森
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.)
Nanjing Astronomical Instruments Co Ltd
Original Assignee
Nanjing Astronomical Instruments Co Ltd
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 Nanjing Astronomical Instruments Co Ltd filed Critical Nanjing Astronomical Instruments Co Ltd
Priority to CN202110030206.9A priority Critical patent/CN112378427B/en
Publication of CN112378427A publication Critical patent/CN112378427A/en
Application granted granted Critical
Publication of CN112378427B publication Critical patent/CN112378427B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01DMEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D5/00Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable
    • G01D5/26Mechanical means for transferring the output of a sensing member; Means for converting the output of a sensing member to another variable where the form or nature of the sensing member does not constrain the means for converting; Transducers not specially adapted for a specific variable characterised by optical transfer means, i.e. using infrared, visible, or ultraviolet light
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01DMEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D11/00Component parts of measuring arrangements not specially adapted for a specific variable
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/62Optical apparatus specially adapted for adjusting optical elements during the assembly of optical systems

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Telescopes (AREA)

Abstract

The invention discloses a method for establishing a reference optical axis of a large-caliber optical system. The method comprises the following steps: the laser tracker scans the primary mirror to model and calculate the virtual central axis; adjusting the position of the target ball to meet the virtual central axis space equation; the interferometer marks the central position of the target ball; adjusting the center of the reticle to coincide with the center of a converged light spot of the interferometer to complete the marking of a space point on the virtual central axis; repeating the above operations to finish marking another space point on the virtual central axis; the theodolite is aligned with the centers of the two reticles to determine a reference optical axis. The method can quickly and accurately establish the installation and adjustment reference optical axis for the optical system, provides a reliable and accurate installation and adjustment reference for subsequent installation and adjustment detection work, and is suitable for various optical systems.

Description

Method for establishing reference optical axis of large-caliber optical system
Technical Field
The invention belongs to the technical field of optical detection, relates to an optical telescope adjustment technical method, and particularly relates to a large-caliber optical system reference optical axis establishing method adopting laser tracker-interferometer combined measurement.
Background
In the field of large optical system development, after parts required in devices such as a large-aperture telescope, a large-aperture collimator and the like are processed, a specific optical assembly and adjustment technology is required to carry out system assembly and adjustment, and the optical system after assembly and adjustment can normally work. The telescope is adjusted to install each optical element to a specific spatial position according to the optical design requirement, so that the system achieves the optical performance required by the design. If the telescope has a misalignment amount, the conditions of aberration increase, imaging quality reduction, target detail loss and the like can be caused, so that the optical system can reach the design standard through a reasonable installation and adjustment process.
In the common optical system installation and adjustment schemes such as a telescope and the like, the main mirror and mechanical positioning are relied on, and the optical axis marking process is avoided. The method uses the primary mirror as a system to establish the whole adjusting reference, uses the wave aberration of the system as a judgment basis, and realizes the adjustment of the optical system by adjusting the secondary mirror. In the other scheme, two cross lines are drawn by taking the edge of the primary mirror as a reference, and a cross wire is used as the center of the vertex of the primary mirror to establish the reference. The two schemes can not accurately find the main optical axis of the main mirror, so that the pointing direction of the optical system, the off-axis visual field image quality and the design are deviated.
Disclosure of Invention
Aiming at the defects in the prior art, the invention provides a large-caliber optical system reference optical axis establishing method based on laser tracker-interferometer combined measurement, which can quickly establish the installation and adjustment reference optical axes of optical systems such as a telescope. The method has strong universality, is suitable for the adjustment of various types of main mirrors, and particularly has good applicability to the annular main mirror which cannot be adjusted by the traditional method.
In order to achieve the purpose, the invention provides the following technical scheme:
a method for establishing a reference optical axis of a large-aperture optical system, comprising:
step 1: placing the target ball (2) at the edge of the main mirror (7), recording the spatial position of the target ball (2), moving the target ball (2) at the edge of the main mirror (7) to obtain n target ball (2) coordinates
Figure 366284DEST_PATH_IMAGE001
Wherein x isn,yn,znIs the space position coordinate of the target ball;
step 2: establishing the outer contour of the primary mirror (7) according to the coordinates obtained in the step (1)
Figure 608390DEST_PATH_IMAGE002
And calculating to obtain a space linear equation of the virtual central axis
Figure 653707DEST_PATH_IMAGE003
Wherein
Figure 580075DEST_PATH_IMAGE004
The position coordinates of the known points on the virtual central axis are shown, and m, n and p are direction vectors S = (m, n and p) of a space linear equation;
and step 3: placing the target ball (2) on a high-precision translation table (3), adjusting the position of the target ball (2) in space, and monitoring the position coordinate of the target ball (2) in real time until the coordinate of the target ball (2)
Figure 722343DEST_PATH_IMAGE005
Satisfy the space linear equation
Figure 810385DEST_PATH_IMAGE003
The central point of the target ball (2) is positioned on the central shaft;
and 4, step 4: aligning the interferometer (4) to the measurement target ball (2), adjusting the position of the interferometer (4) along the direction of the virtual central axis until interference fringes appear in the visual field of the interferometer (4), finely adjusting the position of the interferometer (4) to reduce the number of the interference fringes in the visual field, indicating that the lens focus of the interferometer (4) is near the spherical center of the target ball (2), continuously finely adjusting the position of the interferometer (4) until the number of the interference fringes in the visual field is minimum, and indicating that the lens focus of the interferometer (4) is coincided with the spherical center of the target ball (2);
and 5: removing the target ball (2), finely adjusting the position of the first reticle (5) until the intersection point of the convergent light spot of the interferometer (4) and the cross line of the first reticle (5) is superposed, namely the first reticle (5) is adjusted in place, fixing the first reticle (5) in the space, wherein the position of the first reticle (5) is
Figure 405314DEST_PATH_IMAGE006
Step 6: replacing the position of the target ball (2), repeating the steps 3-5, determining the position of another point on the central shaft, and marking by using a second reticle (6), wherein the position of the second reticle (6) is
Figure 135373DEST_PATH_IMAGE007
And 7: and (3) removing the target ball (2) and the interferometer (4), and respectively aligning the cross intersection points of the first reticle (5) and the second reticle (6) by using a theodolite (8) to establish a reference optical axis of the primary mirror (7).
Further, the spatial position of the target ball is recorded using a laser tracker.
Furthermore, software in the laser tracker is utilized to establish the outline of the primary mirror, and the position coordinates of the target ball are monitored in real time in the laser tracker software.
Further, the first reticle position was fine-tuned using a micrometer microscope.
Compared with the prior art, the invention has the advantages that:
the method for establishing the assembling and adjusting reference axis of the optical system such as the telescope can quickly and accurately establish the assembling and adjusting reference optical axis for the optical system, provide reliable and accurate assembling and adjusting reference for subsequent assembling and adjusting detection work, and ensure that the performance of the optical system meets the design requirement. The invention has strong adaptability, and can be applied to various optical systems: the optical system of various traditional telescopes, collimator tubes and annular primary mirrors. The optical-mechanical system established by the invention has the advantages of high assembly and adjustment reference axis precision, high digitization degree, high establishment speed of the reference, and simple and efficient overall scheme.
Drawings
FIG. 1 is a schematic diagram of primary mirror optical axis modeling;
FIG. 2 is a schematic view of a target ball positioning light path;
FIG. 3 is a schematic view of a reticle positioning optical path;
FIG. 4 is a schematic illustration of the main optical axis positioning;
FIG. 5 is a front view of a 2m ring primary mirror;
FIG. 6 is a cross-sectional view of a 2m ring primary mirror;
fig. 7 is a measurement flowchart.
The labels in the figure are: 1. a laser tracker; 2. a target ball; 3. a high-precision translation stage; 4. an interferometer; 5. a first reticle; 6. a second reticle; 7. a primary mirror; 8. a theodolite; 9. a micrometric microscope; 10. a central axis.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
The method for establishing the reference optical axis of the large-aperture optical system in the embodiment uses a laser tracker 1, a target ball 2, a three-dimensional high-precision translation 3, an interferometer 4, a first reticle 5, a second reticle 6, a primary mirror 7, a theodolite 8 and a micrometering microscope 9 to establish the reference optical axis. The embodiment can quickly establish the installation and adjustment reference optical axis of an optical system such as a telescope. The following embodiment exemplifies a 2m ring-shaped primary mirror.
Step 1 (shown in fig. 1): placing the target ball (2) at the edge of a main mirror (7), recording the space position of the target ball (2) by using a laser tracker (1), moving the target ball (2) at the edge of the main mirror (7) to obtain the coordinates of n target balls (2)
Figure 69831DEST_PATH_IMAGE001
Wherein x isn,yn,znIs the spatial position coordinate of the target ball in the laser tracker (1) software;
step 2: coordinates obtained from step 1 in a laser tracker (1)) An equation of the outer contour cylindrical surface or the middle hole cylindrical surface of the main mirror (7) is established in software
Figure 391091DEST_PATH_IMAGE008
And calculating to obtain a space linear equation of the virtual central axis
Figure 7404DEST_PATH_IMAGE003
Wherein
Figure 72312DEST_PATH_IMAGE004
The position coordinates of known points on a virtual central axis in the laser tracker (1) are shown, and m, n and p are direction vectors S = (m, n and p) of a space linear equation;
step 3 (shown in fig. 2): placing the target ball (2) on a high-precision translation table (3), adjusting the position of the target ball (2) in space, and monitoring the position coordinate of the target ball (2) in real time in the software of the laser tracker (1) until the coordinate of the target ball (2)
Figure 126856DEST_PATH_IMAGE005
Satisfy the space linear equation
Figure 822279DEST_PATH_IMAGE009
The central point of the target ball (2) is positioned on the central shaft;
and 4, step 4: aligning the interferometer (4) to the measurement target ball (2), adjusting the position of the interferometer (4) along the direction of the virtual central axis until interference fringes appear in the visual field of the interferometer (4), finely adjusting the position of the interferometer (4) to reduce the number of the interference fringes in the visual field, indicating that the lens focus of the interferometer (4) is near the spherical center of the target ball (2), continuously finely adjusting the position of the interferometer (4) until the number of the interference fringes in the visual field is minimum, and indicating that the lens focus of the interferometer (4) is coincided with the spherical center of the target ball (2);
step 5 (shown in fig. 3): removing the target ball (2), and finely adjusting the position of the first reticle (5) by using a micrometer microscope (9) until the convergence light spot of the interferometer (4) is superposed with the cross line intersection of the first reticle (5) to indicate that the first reticle (5) is adjusted in placeA first reticle is fixed in the space (5)
Figure 391801DEST_PATH_IMAGE006
Step 6: replacing the position of the target ball (2), repeating the steps 3-5, and determining the position of another point on the central shaft
Figure 932504DEST_PATH_IMAGE007
And is identified by a second reticle (6);
step 7 (shown in fig. 4): the laser tracker (1), target ball (2) and interferometer (4) are removed and aligned with the first reticle (5) using theodolite (8)
Figure 903871DEST_PATH_IMAGE010
And a second reticle (6)
Figure 770196DEST_PATH_IMAGE007
Thereby establishing a reference optical axis of the primary mirror (7).
Fig. 5-6 are schematic structural views of the 2m ring-shaped primary mirror 7. Fig. 7 is a measurement flowchart.
In summary, the method for establishing the reference optical axis of the large-aperture optical system comprises a laser tracker, a target ball, a three-dimensional high-precision translation stage, an interferometer, a primary mirror, a reticle, a micrometering microscope and a theodolite. The method mainly comprises the following steps: (1) the laser tracker scans the primary mirror to model and calculate the virtual central axis; (2) adjusting the position of the target ball to meet the virtual central axis space equation; (3) the interferometer marks the central position of the target ball; (4) adjusting the center of the reticle to coincide with the center of a converged light spot of the interferometer to complete the marking of a space point on the virtual central axis; (5) repeating the steps 2-4 to finish marking another space point on the virtual central axis; (6) the theodolite is aligned with the centers of the two reticles to determine a reference optical axis. The method can realize the quick and accurate establishment of the installation and adjustment reference optical axis of optical systems such as a telescope and the like in the installation and adjustment stage, and provides accurate and reliable installation and adjustment reference for the subsequent installation and adjustment process.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the present invention. Those skilled in the art will appreciate that the details of the invention not described in detail in the specification are within the skill of those skilled in the art. Any modification, equivalent replacement, and improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (4)

1. A method for establishing a reference optical axis of a large-aperture optical system, comprising:
step 1: placing the target ball (2) at the edge of the main mirror (7), recording the spatial position of the target ball (2), moving the target ball (2) at the edge of the main mirror (7) to obtain n target ball (2) coordinates
Figure DEST_PATH_IMAGE002AAA
Wherein x isn,yn,znIs the space position coordinate of the target ball;
step 2: establishing the outer contour of the primary mirror (7) according to the coordinates obtained in the step (1)
Figure DEST_PATH_IMAGE004AAA
And calculating to obtain a space linear equation of the virtual central axis
Figure DEST_PATH_IMAGE006AAA
Wherein
Figure DEST_PATH_IMAGE008AAAAA
The position coordinates of the known points on the virtual central axis are shown, and m, n and p are direction vectors S = (m, n and p) of a space linear equation;
and step 3: placing the target ball (2) on a high-precision translation table (3), adjusting the position of the target ball (2) in space, and monitoring the position coordinate of the target ball (2) in real time until the coordinate of the target ball (2)
Figure DEST_PATH_IMAGE010AAA
Satisfy the space linear equation
Figure DEST_PATH_IMAGE006AAAA
The central point of the target ball (2) is positioned on the central shaft;
and 4, step 4: aligning the interferometer (4) to the measurement target ball (2), adjusting the position of the interferometer (4) along the direction of the virtual central axis until interference fringes appear in the visual field of the interferometer (4), finely adjusting the position of the interferometer (4) to reduce the number of the interference fringes in the visual field, indicating that the lens focus of the interferometer (4) is near the spherical center of the target ball (2), continuously finely adjusting the position of the interferometer (4) until the number of the interference fringes in the visual field is minimum, and indicating that the lens focus of the interferometer (4) is coincided with the spherical center of the target ball (2);
and 5: removing the target ball (2), finely adjusting the position of the first reticle (5) until the intersection point of the convergent light spot of the interferometer (4) and the cross line of the first reticle (5) is superposed, namely the first reticle (5) is adjusted in place, fixing the first reticle (5) in the space, wherein the position of the first reticle (5) is
Figure DEST_PATH_IMAGE012AAA
Step 6: replacing the position of the target ball (2), repeating the steps 3-5, determining the position of another point on the central shaft, and marking by using a second reticle (6), wherein the position of the second reticle (6) is
Figure DEST_PATH_IMAGE014AAA
And 7: and (3) removing the target ball (2) and the interferometer (4), and respectively aligning the cross intersection points of the first reticle (5) and the second reticle (6) by using a theodolite (8) to establish a reference optical axis of the primary mirror (7).
2. The method for establishing the reference optical axis of the large-aperture optical system according to claim 1, wherein the spatial position of the target ball (2) is recorded by using a laser tracker (1).
3. The method for establishing the reference optical axis of the large-aperture optical system according to claim 2, characterized in that the outer contour of the main mirror (7) is established by software in the laser tracker (1), and the position coordinates of the target ball (2) are monitored in real time in the software of the laser tracker (1).
4. The method for establishing the reference optical axis of the large-caliber optical system according to claim 1, wherein the position of the first reticle (5) is finely adjusted by using a micrometer microscope (9).
CN202110030206.9A 2021-01-11 2021-01-11 Method for establishing reference optical axis of large-caliber optical system Active CN112378427B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202110030206.9A CN112378427B (en) 2021-01-11 2021-01-11 Method for establishing reference optical axis of large-caliber optical system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202110030206.9A CN112378427B (en) 2021-01-11 2021-01-11 Method for establishing reference optical axis of large-caliber optical system

Publications (2)

Publication Number Publication Date
CN112378427A true CN112378427A (en) 2021-02-19
CN112378427B CN112378427B (en) 2021-04-06

Family

ID=74590025

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202110030206.9A Active CN112378427B (en) 2021-01-11 2021-01-11 Method for establishing reference optical axis of large-caliber optical system

Country Status (1)

Country Link
CN (1) CN112378427B (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103557791A (en) * 2013-11-08 2014-02-05 中国科学院光电技术研究所 Device and method for measuring secondary constant of large-caliber aspheric primary mirror
CN103926058A (en) * 2014-03-27 2014-07-16 中国科学院长春光学精密机械与物理研究所 Method for measuring optical axis in aspheric surface detection by means of self-aligning plane mirror
US20150019130A1 (en) * 2013-07-09 2015-01-15 Rosemount Aerospace Inc. Dual Function Focal Plane Array Seeker
KR20150071420A (en) * 2013-12-18 2015-06-26 국방과학연구소 LASER Tracking and Pointing Optical System having Pluralized Optical Telescopes
CN104964648A (en) * 2015-06-30 2015-10-07 中国科学院西安光学精密机械研究所 Off-axis parabolic mirror key parameter calibration system and method
CN105547344A (en) * 2015-12-08 2016-05-04 武昌船舶重工集团有限公司 Test equipment calibration device and calibration method thereof
CN106767403A (en) * 2016-12-09 2017-05-31 中国科学院长春光学精密机械与物理研究所 A kind of optical axis position error detection method of many optical axis optical systems

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150019130A1 (en) * 2013-07-09 2015-01-15 Rosemount Aerospace Inc. Dual Function Focal Plane Array Seeker
CN103557791A (en) * 2013-11-08 2014-02-05 中国科学院光电技术研究所 Device and method for measuring secondary constant of large-caliber aspheric primary mirror
KR20150071420A (en) * 2013-12-18 2015-06-26 국방과학연구소 LASER Tracking and Pointing Optical System having Pluralized Optical Telescopes
CN103926058A (en) * 2014-03-27 2014-07-16 中国科学院长春光学精密机械与物理研究所 Method for measuring optical axis in aspheric surface detection by means of self-aligning plane mirror
CN104964648A (en) * 2015-06-30 2015-10-07 中国科学院西安光学精密机械研究所 Off-axis parabolic mirror key parameter calibration system and method
CN105547344A (en) * 2015-12-08 2016-05-04 武昌船舶重工集团有限公司 Test equipment calibration device and calibration method thereof
CN106767403A (en) * 2016-12-09 2017-05-31 中国科学院长春光学精密机械与物理研究所 A kind of optical axis position error detection method of many optical axis optical systems

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
劳达宝等: "飞秒激光跟踪仪跟踪光路的优化设计与分析", 《中国激光》 *
庞哲等: "利用激光跟踪仪测量大口径非球面几何参数", 《航天返回与遥感》 *

Also Published As

Publication number Publication date
CN112378427B (en) 2021-04-06

Similar Documents

Publication Publication Date Title
CN107796329B (en) A kind of convex aspheric surface reflecting mirror surface shape detection device and detection method
CN101858735B (en) Large-caliber off-axis aspheric surface measuring and calibrating system
CN110631477A (en) Optical imaging unit and system for measurement techniques
CN113588082B (en) High-precision quick assembling and adjusting method for off-axis prism dispersion type hyperspectral imager
CN111338390A (en) Cemented lens centering control method and system and full-automatic cementing equipment
CN115166932B (en) Optical axis adjusting method of large-caliber long-focus off-axis optical system
CN110716321B (en) Off-axis two-mirror system assembling and adjusting method
CN115290006A (en) System and method for alignment of optical axis and detection of surface curvature of reflection light path
CN114488498B (en) Off-axis multi-reflection optical system precise adjustment method based on spherical reflector
CN110989188B (en) K mirror optical system adjusting method
CN115202061A (en) Main optical system assembling, adjusting and aligning method of large-aperture telescope
CN116242315A (en) Mounting and adjusting method of double-sided array off-axis three-reflector mapping camera
CN113739719B (en) Surface shape detection system and method of high-precision Schmidt correction plate
West et al. Alignment and use of the optical test for the 8.4-m off-axis primary mirrors of the Giant Magellan Telescope
CN112378427B (en) Method for establishing reference optical axis of large-caliber optical system
CN113267195A (en) Spacecraft cabin butt joint assembly relative pose measurement method
CN110567392B (en) Method for testing surface shape of convex free-form surface reflector
CN109099871B (en) Interference detection alignment method based on circular target
CN114755818B (en) Device and method for adjusting large-aperture telescope garage light path
CN115164775A (en) Large-caliber convex aspheric reflector surface shape detection device and detection method thereof
CN109437599A (en) A kind of spacecrafts rendezvous sensor superhigh precision mirror integral formula processing method
CN113126272B (en) Method for assembling and adjusting large-view-field off-axis three-mirror optical system
CN212749412U (en) Be used for accurate debugging and detecting system of Fery prism subassembly
CN110764271B (en) Method for adjusting position precision among lenses in conjugate optical system
CN108507488B (en) System and method for detecting surface shape of conical mirror based on axial scanning

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