CN109656013A - A kind of large aperture telescope primary mirror cell assembly method based on laser tracker - Google Patents

A kind of large aperture telescope primary mirror cell assembly method based on laser tracker Download PDF

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Publication number
CN109656013A
CN109656013A CN201811541725.6A CN201811541725A CN109656013A CN 109656013 A CN109656013 A CN 109656013A CN 201811541725 A CN201811541725 A CN 201811541725A CN 109656013 A CN109656013 A CN 109656013A
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primary mirror
large aperture
aperture telescope
mirror cell
laser tracker
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CN109656013B (en
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宿馨文
王建立
吴小霞
孙敬伟
李剑锋
邵亮
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Changchun Institute of Optics Fine Mechanics and Physics of CAS
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Changchun Institute of Optics Fine Mechanics and Physics of CAS
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    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B23/00Telescopes, e.g. binoculars; Periscopes; Instruments for viewing the inside of hollow bodies; Viewfinders; Optical aiming or sighting devices
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B23/00Telescopes, e.g. binoculars; Periscopes; Instruments for viewing the inside of hollow bodies; Viewfinders; Optical aiming or sighting devices
    • G02B23/16Housings; Caps; Mountings; Supports, e.g. with counterweight
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B7/00Mountings, adjusting means, or light-tight connections, for optical elements
    • G02B7/02Mountings, adjusting means, or light-tight connections, for optical elements for lenses

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

Abstract

Large aperture telescope primary mirror cell assembly method provided by the invention based on laser tracker, establishes the large aperture telescope primary mirror two-dimensional coordinate system using laser tracker;It is positioned according to position of the large aperture telescope primary mirror two-dimensional coordinate system to primary mirror support pad;Large aperture telescope primary mirror cell two-dimensional coordinate system is established using laser tracker;It is positioned according to position of the large aperture telescope primary mirror cell two-dimensional coordinate system to primary mirror cell's support construction;Corresponding primary mirror support pad and the connection of primary mirror cell's support construction are compared, position differ by more than flexible link can deviation range then primary mirror cell's support construction is adjusted, large aperture telescope primary mirror cell assembly method provided by the invention based on laser tracker, the step of specific tooling is processed in conventional method is abandoned, the installation site of large aperture telescope primary mirror support pad and large aperture telescope primary mirror cell support construction is positioned using laser tracker, it reduces costs and avoids waste, effectively increase positioning accuracy.

Description

A kind of large aperture telescope primary mirror cell assembly method based on laser tracker
Technical field
The present invention relates to Systems for optical inspection technical field, in particular to a kind of heavy caliber based on laser tracker is looked in the distance Mirror primary mirror cell assembly method.
Background technique
Optical telescope is that scientist detects the essential tool of tera incognita, with the detection of farther apparent target The bore of demand, telescope is also gradually increased.The installation step of traditional optical telescope primary mirror cell are as follows: (1) using special fixed Primary mirror is supported pad bonding, such as customization and the big aluminium sheet tooling of primary mirror by the tooling of system, and it is viscous that supporting pad is reserved in tooling Position is connect, positioning bonding is carried out to supporting pad;(2) flexible support structure anchor point is gone out by machine tooling;(3) by special Primary mirror is put into mirror cell by hoisting tool, while guaranteeing that supporting pad is aligned with support construction.It is traditional but with the increase of bore The shortcomings that primary mirror cell's assembly method is more prominent: (1) the tooling size customized is big, the lathe of processing is required to increase, support Pad bonding location positioning accuracy is difficult to ensure;(2) tooling customized only uniquely can be used the identical supporting way primary mirror of identical bore, Do not have versatility, causes the increase of cost and the waste of resource;(3) for entirely supporting for adjustment process, this side Method serious forgiveness is low and goes wrong and is not easy to check, once there is mistake, the bonding location and support knot of supporting pad in machine tooling The position of structure can then malfunction, and lead to the mistake of entire support system, due to the increase of primary mirror size, supporting pad and support construction Quantity is consequently increased, and also increases difficulty to the investigation of mistake.
Measurement efficiency higher measuring tool when laser tracker is a kind of high measurement accuracy, measurement range Datong District, its benefit With matched target ball and target seat acquisition space characteristics point position and the relative positional relationship for measuring each point.It is answered extensively In the industry for aircraft manufacturing assembly, auto manufacturing etc. with large scale high-precision requirement, but laser tracker is answered For positioning the assembly of large aperture telescope primary mirror cell there is not yet similar report.
Summary of the invention
Have in view of that, it is necessary in view of the defects existing in the prior art, provide it is a kind of be applied to using laser tracker it is big The installation site of Aperture Telescope primary mirror support pad and large aperture telescope primary mirror cell support construction, reduces costs and avoids wave Take and effectively increase the large aperture telescope primary mirror cell assembly method of positioning accuracy.
To achieve the above object, the present invention adopts the following technical solutions:
A kind of large aperture telescope primary mirror cell assembly method based on laser tracker, the large aperture telescope primary mirror cell It is inside provided with large aperture telescope primary mirror, the back side of the large aperture telescope primary mirror cell is connected with several primary mirror cells support knot Structure, the back side of the large aperture telescope primary mirror are provided with several primary mirror support pads, a mutual primary mirror support pad And primary mirror cell's support construction is connected by a flexible link, which is characterized in that is included the following steps:
The large aperture telescope primary mirror two-dimensional coordinate system is established using laser tracker;
It is positioned according to position of the large aperture telescope primary mirror two-dimensional coordinate system to the primary mirror support pad;
Large aperture telescope primary mirror cell two-dimensional coordinate system is established using laser tracker;
Determined according to position of the large aperture telescope primary mirror cell two-dimensional coordinate system to primary mirror cell's support construction Position;
The corresponding primary mirror support pad and the connection of primary mirror cell's support construction are compared, position difference is super Cross the flexible link can deviation range then primary mirror cell's support construction is adjusted.
In some preferred embodiments, the large aperture telescope primary mirror two-dimensional coordinate is being established using laser tracker In the step of being, include the following steps:
Several described primary mirror support pads are numbered one by one, are denoted as supporting pad A1, A2 ... An respectively;
Using the laser tracker as reference, using the back side of the large aperture telescope primary mirror as datum level P, target is utilized If mark ball detects the P1 that does of the datum level P, the coordinate of P2 ... Pn is denoted as Pi (xi, yi, zi), to obtain the datum level P Equation ax+by+cz+d=0 and normal vector N (a, b, c), a, b, c are not 0 simultaneously;
If the aperture edge for acquiring the large aperture telescope primary mirror centre bore does C1, C2 ... Cn each point coordinate is denoted as Ci (xi, yi, zi), Ci is projected on the benchmark P optimized using least square method and obtained center of circle O1 coordinate (x0, y0, z0);
Choose any point M1 on the datum level P, x-axis be denoted as with O1M1 line, on the datum level P perpendicular to The line of O1N1 is denoted as y-axis, establishes the large aperture telescope primary mirror two-dimensional coordinate system.
In some preferred embodiments, large aperture telescope primary mirror cell two dimension seat is being established using laser tracker In the step of mark system, include the following steps:
Several described axial support structures are numbered one by one, are denoted as B1, B2 ... Bn respectively;
Using the laser tracker as reference, using the back side of the large aperture telescope primary mirror cell as datum level R, utilize If target ball detects the R1 that does of the datum level R, the coordinate of R2 ... Rn is denoted as Ri (xi, yi, zi), to obtain the benchmark Face R equation ax+by+cz+d=0 and normal vector N (a, b, c), a, b, c are not 0 simultaneously;
If the aperture edge for acquiring large aperture telescope primary mirror cell centre bore does C1, C2 ... Cn each point coordinate, note For Ci (xi, yi, zi), Ci is projected on the datum level R and obtains center of circle O1 coordinate (x0, y0, z0);
Choose any point M2 on the datum level R, x-axis be denoted as with O2M2 line, on the datum level R perpendicular to The line of O2N2 is denoted as y-axis, establishes the two-dimensional coordinate system of the large aperture telescope primary mirror cell.
In some preferred embodiments, it is tied by two corresponding primary mirror support pads and primary mirror cell support The connection of structure compares, position differ by more than the flexible link can deviation range then to primary mirror cell's support construction carry out In the step of adjustment, include the following steps:
The corresponding primary mirror support is padded into A1, A2 ... the position coordinates (ai, di, mi) of An and the primary mirror cell support The position coordinates (bi, si, ti) of structure B1, B2 ... Bn carry out position and seek difference i.e. When position differ by more than the flexible link can deviation range, then Primary mirror cell's support construction is adjusted.
The present invention by adopting the above technical scheme the advantages of be:
Large aperture telescope primary mirror cell assembly method provided by the invention based on laser tracker, utilizes laser tracker Establish the large aperture telescope primary mirror two-dimensional coordinate system;According to the large aperture telescope primary mirror two-dimensional coordinate system to the master The position of mirror supporting pad is positioned;Large aperture telescope primary mirror cell two-dimensional coordinate system is established using laser tracker;Root It is positioned according to position of the large aperture telescope primary mirror cell two-dimensional coordinate system to primary mirror cell's support construction;It will be corresponding The primary mirror support pad and the connection of primary mirror cell's support construction compare, position differs by more than the flexible link can be inclined Poor range is then adjusted primary mirror cell's support construction, and the heavy caliber provided by the invention based on laser tracker is looked in the distance Mirror primary mirror cell assembly method, has abandoned the step of specific tooling is processed in conventional method, positions heavy caliber using laser tracker The installation site of telescope primary mirror support pad and large aperture telescope primary mirror cell support construction, reduces costs and avoids waste, And effectively increase positioning accuracy.
In addition, the large aperture telescope primary mirror cell assembly method provided by the invention based on laser tracker, laser tracking Instrument can also feed back the bonding and large aperture telescope primary mirror of large aperture telescope primary mirror support pad while positioning each position The position of room support construction understands the deviation of each actual position and ideal position, checks convenient for the later period.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this Some embodiments of invention for those of ordinary skill in the art without creative efforts, can be with Other attached drawings are obtained according to these attached drawings.
Fig. 1 is the structural schematic diagram of primary mirror support pad provided by the invention and primary mirror cell's support construction
Fig. 2 is that the back support of the large aperture telescope primary mirror provided in an embodiment of the present invention pads distribution map.
Fig. 3 is the back support structure distribution figure of the large aperture telescope primary mirror cell provided in an embodiment of the present invention.
Fig. 4 is the step of the large aperture telescope primary mirror cell assembly method provided in an embodiment of the present invention based on laser tracker Rapid flow chart.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts all other Embodiment shall fall within the protection scope of the present invention.
Referring to Fig. 1, for the present invention provides a kind of assembly side, large aperture telescope primary mirror cell based on laser tracker Primary mirror support pad and the structural schematic diagram of primary mirror cell's support construction involved in method, wherein the large aperture telescope primary mirror cell It is inside provided with large aperture telescope primary mirror, the back side of the large aperture telescope primary mirror cell is connected with several primary mirror cells support knot Structure 110, the back side of the large aperture telescope primary mirror are provided with several primary mirror support pads 120, a mutual primary mirror Supporting pad and primary mirror cell's support construction 110 are connected by a flexible link 130.
Referring to Fig. 2, the back support pad distribution of the large aperture telescope primary mirror provided for one embodiment of the invention Scheme, primary mirror support pad 120 is distributed in the back side of the large aperture telescope primary mirror in Fig. 2, can be with the large aperture telescope master Mirror is pasted.
Referring to Fig. 3, the back support structure of the large aperture telescope primary mirror cell provided for one embodiment of the invention Distribution map, the primary mirror cell Tu2Zhong support construction 110 are distributed in the back side of the large aperture telescope primary mirror cell, the primary mirror support Pad 120 and primary mirror cell's support construction 110 are connected by a flexible link.
Large aperture telescope primary mirror cell assembly method provided by the invention based on laser tracker described further below Flow chart of steps.
Referring to Fig. 4, for the large aperture telescope primary mirror cell assembly provided in an embodiment of the present invention based on laser tracker The step flow chart of method, includes the following steps:
Step S110: the large aperture telescope primary mirror two-dimensional coordinate system is established using laser tracker;
In some preferably embodiments, the large aperture telescope primary mirror two-dimensional coordinate is established using laser tracker System, specifically include the following steps:
Step S111: several described primary mirror support pads are numbered one by one, are denoted as supporting pad A1 respectively, A2 ... An please join Read Fig. 3.
Step S112: using the laser tracker as reference, using the back side of the large aperture telescope primary mirror as benchmark Face P, if detecting the P1 that does of the datum level P using target ball, the coordinate of P2 ... Pn is denoted as Pi (xi, yi, zi), to obtain The datum level P equation ax+by+cz+d=0 and normal vector N (a, b, c), a, b, c are not 0 simultaneously;
Step S113: if the aperture edge for acquiring the large aperture telescope primary mirror centre bore does C1, C2 ... Cn each point Coordinate is denoted as Ci (xi, yi, zi), and Ci is projected to and optimizes to obtain center of circle O1 coordinate using least square method on the benchmark P (x0, y0, z0);
Step S114: choosing any point M1 on the datum level P, is denoted as x-axis with O1M1 line, in the datum level P On perpendicular to the line of O1N1 be denoted as y-axis, establish the large aperture telescope primary mirror two-dimensional coordinate system.
It is appreciated that since large aperture telescope primary mirror is, selection institute centrosymmetric for center of circle O1 on datum level P Any point M1 on datum level P is stated, x-axis is denoted as with O1M1 line, the line on the datum level P perpendicular to O1N1 is denoted as y Axis establishes the large aperture telescope primary mirror two-dimensional coordinate system.
Step S120: it is carried out according to position of the large aperture telescope primary mirror two-dimensional coordinate system to the primary mirror support pad Positioning;
It is appreciated that due to establishing the large aperture telescope primary mirror two-dimensional coordinate system, it can be according to the primary mirror support pad It is positioned in the position of the large aperture telescope primary mirror two-dimensional coordinate system, and according to positioning result to each primary mirror support pad It is adjusted bonding.
Step S130: large aperture telescope primary mirror cell two-dimensional coordinate system is established using laser tracker;
In some preferred embodiments, large aperture telescope primary mirror cell two dimension seat is being established using laser tracker In the step of mark system, include the following steps:
Step S131: several described axial support structures are numbered one by one, are denoted as B1, B2 ... Bn respectively;
Step S132: using the laser tracker as reference, using the back side of the large aperture telescope primary mirror cell as base Quasi- face R, if detecting the R1 that does of the datum level R using target ball, the coordinate of R2 ... Rn is denoted as Ri (xi, yi, zi), to obtain The datum level R equation ax+by+cz+d=0 and normal vector N (a, b, c), a, b are taken, c is not 0 simultaneously;
Step S133: if the aperture edge for acquiring large aperture telescope primary mirror cell centre bore does C1, C2 ... Cn is each Point coordinate, is denoted as Ci (xi, yi, zi), and Ci is projected to and optimizes to obtain center of circle O1 seat using least square method on the datum level R It marks (x0, y0, z0);
Step S134: choosing any point M2 on the datum level R, is denoted as x-axis with O2M2 line, in the datum level R On perpendicular to the line of O2N2 be denoted as y-axis, establish the two-dimensional coordinate system of the large aperture telescope primary mirror cell.
Step S140: according to large aperture telescope primary mirror cell two-dimensional coordinate system to the position of primary mirror cell's support construction It sets and is positioned;
It is appreciated that due to establishing large aperture telescope primary mirror cell two-dimensional coordinate system, it can be according to primary mirror cell's branch Support structure is positioned in the position of large aperture telescope primary mirror cell two-dimensional coordinate system, and according to positioning result to each master Mirror cell's support construction is adjusted.
Step S150: the corresponding primary mirror support pad and the connection of primary mirror cell's support construction are compared, Position differ by more than the flexible link can deviation range then primary mirror cell's support construction is adjusted.
In some preferred embodiments, it is tied by two corresponding primary mirror support pads and primary mirror cell support The connection of structure compares, position differ by more than the flexible link can deviation range then to primary mirror cell's support construction carry out In the step of adjustment, include the following steps:
The corresponding primary mirror support is padded into A1, A2 ... the position coordinates (ai, di, mi) of An and the primary mirror cell support The position coordinates (bi, si, ti) of structure B1, B2 ... Bn carry out position and seek difference i.e. When position differ by more than the flexible link can deviation range, then Primary mirror cell's support construction is adjusted.
Large aperture telescope primary mirror cell assembly method provided by the invention based on laser tracker, utilizes laser tracker Establish the large aperture telescope primary mirror two-dimensional coordinate system;According to the large aperture telescope primary mirror two-dimensional coordinate system to the master The position of mirror supporting pad is positioned;Large aperture telescope primary mirror cell two-dimensional coordinate system is established using laser tracker;Root It is positioned according to position of the large aperture telescope primary mirror cell two-dimensional coordinate system to primary mirror cell's support construction;It will be corresponding The primary mirror support pad and the connection of primary mirror cell's support construction compare, position differs by more than the flexible link can be inclined Poor range is then adjusted primary mirror cell's support construction, and the heavy caliber provided by the invention based on laser tracker is looked in the distance Mirror primary mirror cell assembly method, has abandoned the step of specific tooling is processed in conventional method, positions heavy caliber using laser tracker The installation site of telescope primary mirror support pad and large aperture telescope primary mirror cell support construction, reduces costs and avoids waste, And effectively increase positioning accuracy.
In addition, the large aperture telescope primary mirror cell assembly method provided by the invention based on laser tracker, laser tracking Instrument can also feed back the bonding and large aperture telescope primary mirror of large aperture telescope primary mirror support pad while positioning each position The position of room support construction understands the deviation of each actual position and ideal position, checks convenient for the later period.
Certain large aperture telescope primary mirror cell assembly method of the invention based on laser tracker can also have a variety of changes It changes and retrofits, it is not limited to the specific structure of above embodiment.In short, protection scope of the present invention should include those for It obviously converts or substitutes and retrofit for those of ordinary skill in the art.

Claims (4)

1. a kind of large aperture telescope primary mirror cell assembly method based on laser tracker, in the large aperture telescope primary mirror cell It is provided with large aperture telescope primary mirror, the back side of the large aperture telescope primary mirror cell is connected with several primary mirror cells support knot Structure, the back side of the large aperture telescope primary mirror are provided with several primary mirror support pads, a mutual primary mirror support pad And primary mirror cell's support construction is connected by a flexible link, which is characterized in that is included the following steps:
The large aperture telescope primary mirror two-dimensional coordinate system is established using laser tracker;
It is positioned according to position of the large aperture telescope primary mirror two-dimensional coordinate system to the primary mirror support pad;
Large aperture telescope primary mirror cell two-dimensional coordinate system is established using laser tracker;
It is positioned according to position of the large aperture telescope primary mirror cell two-dimensional coordinate system to primary mirror cell's support construction;
The corresponding primary mirror support pad and the connection of primary mirror cell's support construction are compared, position differs by more than institute State flexible link can deviation range then primary mirror cell's support construction is adjusted.
2. the large aperture telescope primary mirror cell assembly method based on laser tracker as described in claim 1, which is characterized in that In the step of establishing the large aperture telescope primary mirror two-dimensional coordinate system using laser tracker, include the following steps:
Several described primary mirror support pads are numbered one by one, are denoted as supporting pad A1, A2 ... An respectively;
Using the laser tracker as reference, using the back side of the large aperture telescope primary mirror as datum level P, target ball is utilized If detecting the P1 that does of the datum level P, the coordinate of P2 ... Pn is denoted as Pi (xi, yi, zi), to obtain the datum level P equation Ax+by+cz+d=0 and normal vector N (a, b, c), a, b, c are not 0 simultaneously;
If the aperture edge for acquiring the large aperture telescope primary mirror centre bore does C1, C2 ... Cn each point coordinate is denoted as Ci Ci is projected to and is optimized to obtain center of circle O1 coordinate (x0, y0, z0) using least square method on the benchmark P by (xi, yi, zi);
Any point M1 on the datum level P is chosen, x-axis is denoted as with O1M1 line, perpendicular to O1N1's on the datum level P Line is denoted as y-axis, establishes the large aperture telescope primary mirror two-dimensional coordinate system.
3. the large aperture telescope primary mirror cell assembly method based on laser tracker as claimed in claim 2, which is characterized in that In the step of establishing the large aperture telescope primary mirror cell two-dimensional coordinate system using laser tracker, include the following steps:
Several described axial support structures are numbered one by one, are denoted as B1, B2 ... Bn respectively;
Using the laser tracker as reference, using the back side of the large aperture telescope primary mirror cell as datum level R, target is utilized If ball detects the R1 that does of the datum level R, the coordinate of R2 ... Rn is denoted as Ri (xi, yi, zi), to obtain the datum level side R Journey ax+by+cz+d=0 and normal vector N (a, b, c), a, b, c are not 0 simultaneously;
If the aperture edge for acquiring large aperture telescope primary mirror cell centre bore does C1, C2 ... Cn each point coordinate is denoted as Ci Ci is projected to and is optimized to obtain center of circle O1 coordinate (x0, y0, z0) using least square method on the datum level R by (xi, yi, zi);
Any point M2 on the datum level R is chosen, x-axis is denoted as with O2M2 line, perpendicular to O2N2's on the datum level R Line is denoted as y-axis, establishes the two-dimensional coordinate system of the large aperture telescope primary mirror cell.
4. the large aperture telescope primary mirror cell assembly method based on laser tracker as claimed in claim 3, which is characterized in that It is compared by two corresponding primary mirror support pads and the connection of primary mirror cell's support construction, position differs by more than The flexible link can deviation range the step of being then adjusted to primary mirror cell's support construction in, include the following steps:
The corresponding primary mirror support is padded into A1, A2 ... the position coordinates (ai, di, mi) of An and primary mirror cell's support construction The position coordinates (bi, si, ti) of B1, B2 ... Bn carry out position and seek difference i.e. When position differ by more than the flexible link can deviation range, then Primary mirror cell's support construction is adjusted.
CN201811541725.6A 2018-12-17 2018-12-17 Large-aperture telescope primary mirror chamber assembly method based on laser tracker Active CN109656013B (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110109242A (en) * 2019-05-08 2019-08-09 中国科学院国家天文台南京天文光学技术研究所 Hydraulic trussing for primary mirror of astronomical telescope
CN111399210A (en) * 2020-04-22 2020-07-10 中国科学院长春光学精密机械与物理研究所 Coarse alignment method, device, equipment and storage medium for large-caliber large-field telescope
CN111644822A (en) * 2020-07-02 2020-09-11 德阳市瑞祥机械厂 Method for processing box body of primary mirror chamber of 4m telescope

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101532821A (en) * 2009-04-24 2009-09-16 北京航空航天大学 Global calibration method of laser tracking visual guidance measurement system
CN103412391A (en) * 2013-08-14 2013-11-27 中国科学院光电技术研究所 Method for realizing through-axis centering of optical system based on laser tracker
CN103512511A (en) * 2013-09-26 2014-01-15 南京航空航天大学 Large face automatic measurement method based on laser tracker
CN103753151A (en) * 2014-01-27 2014-04-30 哈尔滨飞机工业集团有限责任公司 Method for increasing location holes on part of tool
CN104374317A (en) * 2014-11-06 2015-02-25 北京工业大学 Machine tool error calibration method based on multi-point measurement technology of laser tracker
CN105091746A (en) * 2015-05-19 2015-11-25 北京星航机电装备有限公司 Space coordinate system calibration method for spacecraft cabin ground docking
CN105388585A (en) * 2015-12-04 2016-03-09 中国科学院长春光学精密机械与物理研究所 Bonding method for supporting pad of large-aperture reflector and application of bonding method
CN106840023A (en) * 2016-07-25 2017-06-13 中国科学院长春光学精密机械与物理研究所 The complex-curved optical parametric of heavy caliber is accurately tested and caliberating device and method
CN107065123A (en) * 2017-06-09 2017-08-18 中国科学院长春光学精密机械与物理研究所 The side support pad fine adjustment positioner of large caliber reflecting mirror
KR20180071130A (en) * 2016-12-19 2018-06-27 경북대학교 산학협력단 Servo Mismatch Compensation Method of Multi-axis Control Machine Using Laser Tracker

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101532821A (en) * 2009-04-24 2009-09-16 北京航空航天大学 Global calibration method of laser tracking visual guidance measurement system
CN103412391A (en) * 2013-08-14 2013-11-27 中国科学院光电技术研究所 Method for realizing through-axis centering of optical system based on laser tracker
CN103512511A (en) * 2013-09-26 2014-01-15 南京航空航天大学 Large face automatic measurement method based on laser tracker
CN103753151A (en) * 2014-01-27 2014-04-30 哈尔滨飞机工业集团有限责任公司 Method for increasing location holes on part of tool
CN104374317A (en) * 2014-11-06 2015-02-25 北京工业大学 Machine tool error calibration method based on multi-point measurement technology of laser tracker
CN105091746A (en) * 2015-05-19 2015-11-25 北京星航机电装备有限公司 Space coordinate system calibration method for spacecraft cabin ground docking
CN105388585A (en) * 2015-12-04 2016-03-09 中国科学院长春光学精密机械与物理研究所 Bonding method for supporting pad of large-aperture reflector and application of bonding method
CN106840023A (en) * 2016-07-25 2017-06-13 中国科学院长春光学精密机械与物理研究所 The complex-curved optical parametric of heavy caliber is accurately tested and caliberating device and method
KR20180071130A (en) * 2016-12-19 2018-06-27 경북대학교 산학협력단 Servo Mismatch Compensation Method of Multi-axis Control Machine Using Laser Tracker
CN107065123A (en) * 2017-06-09 2017-08-18 中国科学院长春光学精密机械与物理研究所 The side support pad fine adjustment positioner of large caliber reflecting mirror

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
周维虎 等: ""基于激光跟踪仪的天基望远镜安装测量技术"", 《红外与激光工程》 *
安其昌 等: ""TMT tertiary mirror axis calibration with laser tracker"", 《OPTOELECTRONICS LETTERS》 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110109242A (en) * 2019-05-08 2019-08-09 中国科学院国家天文台南京天文光学技术研究所 Hydraulic trussing for primary mirror of astronomical telescope
CN111399210A (en) * 2020-04-22 2020-07-10 中国科学院长春光学精密机械与物理研究所 Coarse alignment method, device, equipment and storage medium for large-caliber large-field telescope
CN111644822A (en) * 2020-07-02 2020-09-11 德阳市瑞祥机械厂 Method for processing box body of primary mirror chamber of 4m telescope

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