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The principle of the large-aperture laser differential confocal-interferometric measurement system (LLDCIMS) is illustrated in Fig. 1. We use the Fizeau horizontal interferometric light path configuration,which has several advantages, including a simple structure, fewer accessories, and good applicability and flexibility for testing. Light from a point source passes through a large-aperture beam-expanding system (LBES), which includes a small-aperture collimator (SAC), a beam expander (BE), and a large-aperture collimator (LAC), and is then transformed into a large-aperture parallel beam. A portion of this beam serves as the reference beam, which is reflected by the back surface of the reference lens (RL) and then passes through the beam-expansion system, reflected by beam splitter1 (BS1), transmitted by beam splitter2 (BS2), and reflected by mirror R2 before entering the imaging system. This serves as the reference beam for the rotating ground glass. Another portion of the light serves as the measurement beam, which is transmitted through the reference lens and enters the tested lens (TL). After being reflected by the tested lens, it passes through the reference lens and beam-expansion system, and is then reflected by beam splitter1 (BS1), transmitted by beam splitter2 (BS2), and reflected by mirror R2 before entering the imaging system. This serves as the measurement beam for the rotating ground glass (RG). The reference and measurement beams interfere with the ground glass of the imaging module, and the interference pattern is recorded by the interference charge-coupled device (CCD) after passing through the imaging lens. During the large-aperture interference measurement process, a high-precision phase-shifting function is derived using a large-aperture mechanical phase-shifting system (LAMPS) with a heavy-load reference lens. The air-bearing slider (ABS) supports the large-aperture heavy-load reference lens and its precise adjustment mechanism (PAM) to counteract gravity loads. Phase shifting is driven by a three-channel piezoelectric ceramics (PZT) drive structure via the piezoelectric effect, whereas the elastic deformation of the flexible hinge (FH) enables the gapless micro-displacement of the heavy-load reference lens mechanical phase-shifting system. This setup enables the high-precision measurement of the surface profiling parameters of large-aperture optical elements.
Fig. 1 Principle diagram of large-aperture differential confocal-interferometric measurement system. a large-aperture laser differential confocal-interferometric measurement path; b large-aperture beam-expansion system; c large-aperture mechanical phase-shifting system; d laser differential confocal signal-processing module; e interference signal-processing module; f ultra-long focal length; g convex spherical ultra-large curvature radius; h concave spherical ultra-large curvature radius; i concave spherical interference; j convex spherical interference.
Replacing the reference lens with a large-aperture spherical standard lens enables the measurement of the surface profile, ultra-large curvature radius, and ultra-long focal length of large-diameter spherical optical elements. Acquisition of laser differential confocal signals through virtual pinholes (VP) for measurement of optical component parameters. Moreover, using a system-switching device (SSD) allows one to achieve common baseline measurements of multiple parameters, such as the surface profile, curvature radius/ultra-large curvature radius, and focal length/ultralong focal length of optical elements with small apertures.
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When using the large-aperture differential confocal-interferometric measurement system for large-aperture surface-profiling measurements, the tested lens is placed in the path of the collimated beam behind the reference lens. The interference pattern of the reference beam reflected from the reference lens and the measurement beam reflected from the surface of the tested lens can be expressed as
$$ I(x,y,{t_n}) = {I_d}(x,y) + {I_a}(x,y)\cos [\varphi (x,y) + \delta ({t_n})] $$ (1) where, Id(x,y) represents the background beam intensity of the interference fringes, Ia(x,y) the amplitude of the interference fringes, φ(x,y) = 2kw(x,y) the wavefront phase distribution of the reflected measurement beam from the tested lens, and δ(tn) the phase shift introduced by the reference lens. Specifically, x and y denote the horizontal and vertical coordinates of the pixel points of the i phase-shifting interferogram, respectively, and tn denotes the time required for each phase-shift step.
Additionally, δ(tn) is obtained using the mechanical phase shifter of the heavy-load reference lens, as shown in Fig. 1c. Designing a mechanical structure that combines high-frequency response and high-resolution flexible hinges (FH) with piezoelectric ceramics allows the mechanical phase-shifting system to achieve sub-nanometer-level phase shifting without gaps in the reference lens. Meanwhile, integrating a high-stability, low-ripple piezoelectric ceramic drive power supply and a phase-shifting mechanism in the circuit control allows the mechanical phase-shifting system to achieve high-resolution and low-error phase shifting. By establishing a spatial in-situ monitoring model that combines high-precision, high-resolution capacitive sensors (HCS) with phase control, the interference measurement system can achieve a sub-nanometer-level precision spatial translation of the reference lens. Meanwhile, establishing calibration algorithms for the pitch and yaw errors of the reference lens during mechanical phase shifting allows the system to suppresses phase-shifting errors. Ultimately, high-precision measurement of δ(tn) is achieved in the interference measurement system.
The large-aperture mechanical phase-shifting system model is depicted in Fig. 2, which can be simplified as a mass–spring-damping second-order system28. Under the action of the force at the input end, the deformation is generated at the output end by the interaction of seven straight circular flexible hinges A-G. Based on the equilibrium of the forces in the x, y, and z directions as well as the equilibrium of the forces Fx, Fy, and Fz and the moments Mx, My, and Mz of each hinge, the mechanical phase-shifting actuator of the heavy-load reference lens is designed. The large-aperture mechanical phase-shifting system is driven by a piezoelectric ceramic. If the input displacement is denoted as x, then the output displacement of the mechanical phase-shifting guide rail, denoted as pd, can be expressed by the motion differential equation established based on the large-aperture mechanical phase-shifting system model as follows
$$ M{\ddot p_d} + \mu {\dot p_d} + \left( {{K_t} + K} \right){p_d} = {K_t}x $$ (2) where K is the stiffness of the mechanical phase-shifting guide rail for the heavy-load reference lens, M the total weight of the mechanical phase-shifting system, µ the damping coefficient, and Kt the stiffness of the mechanical phase-shifting transmission mechanism.
Based on the system transfer function, the open-loop transfer function of a large-aperture mechanical phase-shifting system can be derived as follows
$$ G\left( s \right) = \frac{{\alpha {K_v}{K_s}\omega _n^2}}{{\left( {{R_i}{C_p}s + 1} \right)\left( {{s^2} + 2\xi {\omega _n}s + \omega _n^2} \right)}} $$ (3) where $ {K_s} = {{{K_t}}}/({{K + {K_t}}}) $ is the amplification factor, Kv the amplification ratio of the direct current high-voltage power supply, $ {\omega _n} = \sqrt {({{K + {K_t}}})/{M}} $ the undamped natural frequency of the system, $ \xi = {\mu }/{{2M{\omega _n}}} $ the damping ratio of the system, Ri the internal resistance of the PZT drive power supply, and Cp the equivalent capacitance of the PZT.
Using the open-loop transfer function of the large-aperture mechanical phase-shifting system allows one to achieve high-precision and high-stability control of the heavy-load reference lens and thus the actual value of δ(tn). The relationship between the displacement amount pd of the reference lens obtained via the mechanical phase shifting of the heavy-load reference lens and the phase shift amount δ(tn) introduced by the reference lens can be expressed as3
$$ \delta \left( {{t_n}} \right) = {p_d}\frac{{4{\text π} }}{\lambda } $$ (4) where λ represents the wavelength of the laser light source.
Subsequently, a five-step equal-step phase-shifting algorithm is employed, as shown in Fig. 1e. By obtaining five interferograms with phase shifts of δ(tn) = 0, π/2, π, 3π/2, and 2π, the phase distribution φ(x,y) can be extracted as follows
$$ \varphi \left( {x,y} \right) = \arctan \left[ {\frac{{2\left( {{I_4} - {I_2}} \right)}}{{2{I_3} - {I_1} - {I_5}}}} \right] $$ (5) Next, phase unwrapping is performed, followed by Zernike fitting and removal processing, thus resulting in the actual surface profiling of the tested lens.
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When utilizing the large-aperture differential confocal-interferometric measurement system (LDCMS) for ultra-long focal-length measurements, RL is the large-aperture spherical reference lens, and the tested lens is placed in the collimated beam path between the large-aperture spherical RL and the large-aperture collimating lens, as illustrated in Fig. 3.
By precisely correlating the zero points QB of the axial intensity response curves IB(u, uM) of the differential confocal system with the combined focal point B. Then, remove the tested lens and move the reflector to reach A to obtain the differential confocal response signal IA(u, uM), the distance l of the change in focal position with/without the tested lens with an XL-80 Renishaw interferometric (DMI). Subsequently, based on the focal length fR′ of the reference lens and the mirror separation distance d0, the posterior vertex focal distance fTBFD′ of the tested lens is obtained. Utilizing the curvature radius of the tested lens, the vertex focal distance fTBFD′ is converted into the focal length fT′, thereby achieving the measurement of ultra-long focal length lenses37.
Based on geometric imaging theory, the effective focal length fcom′ of the combined lens system, the focal length fT′ of the tested lens, the focal length fR′ of the reference lens, the posterior vertex focal distance fTBFD′ of the tested lens, and the axial distance d from the principal plane of the test lens image side to the principal plane of the reference lens object side, one can calculate the effective focal length value fT′ of the tested lens by converting from the posterior vertex focal distance fTBFD′ of the tested lens as follows
$$\begin{split} {f_T}' = \;&d - {f_R}' + \frac{{{f_R}{'^2}}}{l} = {d_0} - {f_R}' + \frac{{{f_R}{'^2}}}{l} +\\& \frac{{r{}_{12}{b_1}}}{{{n_1}(r{}_{12} - {r_{11}}) + ({n_1} - 1){b_1}}} + \frac{{r{}_{12}{b_1}}}{{{n_1}(r{}_{12} - {r_{11}}) + ({n_1} - 1){b_1}}} \end{split}$$ (6) where b1 is the center thickness of the tested lens, n1 is the refractive index of the material, and r11 and r12 are the radii of curvature of the left and right surfaces, respectively.
Small-aperture tested lenses can be placed in the measurement beam path of small optical elements. This measurement method is consistent with that for a large-aperture ultra-long focal length. The laser differential confocal signals are precisely focused at points A′ and B′ to achieve accurate focusing, thus enabling the measurement of small-aperture tested lenses with ultra-long focal lengths.
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When utilizing the large-aperture differential confocal-interferometric measurement system (LDCMS) for the ultra-large curvature radius, RL is the large-aperture spherical reference lens, and the tested lens is positioned in the converging light path of the large-aperture spherical reference lens, as illustrated in Fig.4. After passing through the large-aperture spherical reference lens, the light converges to cat's eye position of the measured lens, i.e., A. The differential confocal light intensity response curve IA(u, uM) at the cat’s eye position of the measured surface is used to accurately determine the focus of the cat’s eye position. Subsequently, the tested lens is shifted such that the measurement beam is reflected off the surface of the tested lens and converges at position D the back surface of the reference lens. At this point, surface D the back surface of the reference lens is focused precisely using the differential confocal-intensity response curve IC(u, uM) at position C. Finally, the position difference LT between points A and C is measured using a DMI, and the curvature radius r of the tested lens is obtained using ray-tracing algorithms in conjunction with the posterior vertex focal length fRBFD′ of the reference lens38.
The zero-crossing points Q1 and Q2 of the laser differential confocal-intensity response curves IA(u, uM) accurately correspond to cat's eye position A of the tested lens. The difference in the positions of the tested lens at points A and C, which is denoted as LT here, can be precisely measured using a DMI.
$$ \left\{ \begin{gathered} \theta = \arctan \left( {\frac{{\rho D}}{{2{f_{RBFD}}^\prime }}} \right) \\ \tan\frac{{{\theta _1}}}{2} = \frac{{2{f_{RBFD}}^\prime {r_\rho }\left( {1 - \cos{\theta _1}} \right)}}{{\rho D\left[ {{L_T} - {r_\rho }\left( {1 - \cos{\theta _1}} \right)} \right]}} \\ {r_\rho } = \frac{{\left( {{f_{RBFD}}^\prime - {L_T}} \right)\sin \left( {\theta - 2{\theta _1}} \right)}}{{\sin \left( {\theta - {\theta _1}} \right) - \sin \left( {\theta - 2{\theta _1}} \right)}} \\ \end{gathered} \right. $$ (7) Here, D is the aperture of the reference lens, ρ the normalized aperture of the beam, θ the angle between the outgoing light rays from the reference lens and the optical axis of the reference lens. The curvature radius of the tested lens, which was calculated based on imaging from point A to point D by the light ray at aperture ρ, is denoted as rρ. Meanwhile, θ1 represents the angle between rρ and the optical axis m of the reference lens.
The curvature radius value r of the tested lens can be expressed as
$$ r = \frac{{\displaystyle\int_0^1 {2{\text π} \rho {r_\rho }d\rho } }}{{\displaystyle\int_0^1 {2{\text π} \rho d\rho } }} = 2\displaystyle\int_0^1 {\rho {r_\rho }d\rho } $$ (8) Small-diameter tested lenses can be placed on small-aperture measurement optical paths. This measurement method is consistent with that for a large-aperture curvature radius. By precisely focusing at points A' and C' based on laser differential confocal signals, one can accurately measure small-diameter tested lenses with an ultra-large curvature radius.
In summary, the large-aperture laser differential confocal-interferometric measurement system can achieve high-precision, multiple parameters, common baseline measurement for optical elements of large, medium, and small diameters.
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Based on the schematic diagram of the measurement system shown in Fig. 1, a large-aperture laser differential confocal-interferometric measurement system was designed and developed, as shown in Fig. 5.
This system consists of several main components: the interferometer main machine (IMM), which is used to complete the measurement data acquisition, and the controller and computer (CAC); the large-aperture beam-expanding system, which is used to expand the point light source into a parallel beam with an aperture of 820 mm; the heavy-load reference lens mechanical phase-shifting mechanism, which is used to realize the mechanical phase-shifting function of the heavy-load reference lens; the small-aperture multiparameter measurement system, which is used to realize the multiparameter measurement of small-aperture optical elements, including a precision five-dimensional adjustment mechanism (FDAM) for adjusting the posture of the tested lens, a precision rail screw mechanism (HPGS) for the precise positioning of the tested lens, and an XL-80 Renishaw interferometric displacement measurement mechanism (DMI) for obtaining the displacement of the tested lens; and the main control system, which is used to control the entire system and process the acquired data, including the processing of interference signals and laser differential confocal signals. In addition, the mainframe of the interferometric measurement system, the large-aperture beam-expanding system, the large-aperture precision-adjustment mechanism, and the mechanical phase-shifting mechanism are designed on the same air-floating vibration isolation instrument base. Switching measurements of different apertures can be achieved through a conversion mechanism to satisfy the requirements of multiple extreme-parameters common baseline measurements.
The optical system is the most crucial component of a large-aperture laser differential confocal interferometric measurement system. The precision of an optical system determines the measurement accuracy of the entire instrument. To satisfy the requirements for high-precision measurements, an optical system for a large-aperture laser differential confocal-interferometric system was designed, as shown in Fig. 6. To ensure the stability of interference fringes while satisfying the spatial and temporal coherence requirements of the light source, a He-Ne laser light source with the following parameters was selected: wavelength of 632.8 nm, power stability of <2.5%; spot diameter of 0.6 mm and divergence angle of 1.4 mrad. The combined focal length of the beam-expander system, fZ, was 8155 mm.
The design results of the optical system are shown in Fig.7. For the large-aperture laser differential confocal interferometric system, the transmitted wavefront of the system with a PV value of 0.0074λ for the transmitted wavefront was adopted. The distortion aberration of the imaging system was less than 0.011%, and the MTF of the system was > 0.6@22lp/mm. The spot radius of the system is 0.3 μm, which was smaller than the Airy disk radius of 2.2 μm. The pixel size of the differential confocal signal acquisition camera was 8.3 μm × 8.3 μm, which met the measurement requirements for differential confocal ultra-long focal lengths and ultra-large radii of curvature.
Fig. 7 Design results of large-aperture laser differential confocal-interferometric measurement optical system. (a) the transmitted wavefront of the system; (b) the MTF of the system. (c) The distortion aberration system. (d) The spot radius of the system.
In a large-aperture laser differential confocal-interferometric measurement system, the hardware components, under the coordination of the host computer and measurement control software, perform functions such as phase-shifting drive control, high-resolution interferometric image acquisition, precise surface-profile computation, phase-shifting monitoring signal acquisition, pose signal decoupling and computation, tilt-error separation compensation, phase-shifting interferometric calculation and processing, and differential confocal signal acquisition and computation.
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(1) Optical Quality of Large-Aperture Interferometer
The optical quality of the large-aperture interferometer, which is based on the results of the cavity calibrations of the reference lens and the tested lens performed by the Standardization and Testing Center of the Laser Fusion Research Center, is the standard deviation of the measurement result expressed as
$$ {u_{B1}} = \left( {0.073\lambda + 0.002\lambda \times 3} \right)/3 = 0.0265\lambda $$ (9) (2) Errors Introduced by Mechanical Phase Shifting
The mechanical phase-shifting errors include calibration and nonlinear errors. Using nonlinear voltage drive and compensation methods can reduce the mechanical phase-shifting error to 2.01 × 10−4 rad. This introduces a standard deviation of λ/500 for the wavefront measurement error. The standard deviation is
$$ {u_{B2}} = 0.002\lambda $$ (10) (3) Detection Error of Photodetector CCD and Quantization Error of Interference Image
The CCD detection errors can be classified into two categories. The first is the nonlinearity of the response at each point on the target surface of the CCD. The other is the unevenness in the geometric distribution of the CCD target surface, which can introduce errors during the conversion to a digital image. The standard deviation of the introduced wavefront error is λ/10039.
$$ {u_{B3}} = 0.01\lambda $$ (11) (5) Effect of Stray Fringes
Owing to the addition of stray light from the reflection of various optical surfaces in the optical system, the standard deviation of the introduced wavefront error due to stray fringes is λ/800.
$$ {u_{B4}} = 0.00125\lambda $$ (12) (6) Stability of Light Source
The frequency stability of the laser affects the accuracy of the interferometer test. The standard deviation of the light source is
$$ {u_{B5}} = 0.002\lambda $$ (13) (7) Calculation of Uncertainty
The combined uncertainty (u) is calculated using the root-sum-square method by combining the various components of uA and uB as follows
$$ U = k{\left[ {\sum {u_i^2} } \right]^{1/2}} = k \times {\left[ {u_{B1}^2 + u_{B2}^2 + u_{B3}^2 + u_{B4}^2 + u_{B5}^2} \right]^{1/2}} $$ (14) Therefore, according to the uncertainty analysis, it can be seen that the expanded uncertainty of the large-aperture interferometer based on the mechanical phase shift of the heavy-load reference lens is λ/29, that is, 22.0 nm. The current interferometer surface profiling accuracy is λ/10, so the achieved accuracy of 22.0 nm is advanced compared with the accuracy of other optical metrology designs for similar optical elements. We have effectively suppressed the phase shift error and improved the measurement accuracy of the system by using a high-precision, heavy-load reference lens mechanical phase shift method. In addition, the detection error of the photodetector CCD and the quantization error of the interference image are the main sources of error. This error can be reduced by replacing the device and optimizing the algorithm to improve the accuracy of the system.
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(1) Uncertainty caused by d0
According to the literature40, that the relative measurement error of the axial space is less than 0.02%. Therefore, the stand uncertainty of d0 can be described based on a uniform distribution as follows
$$ u\left( {{d_0}} \right) = \frac{{0.02\% \times {d_0}}}{{\sqrt 3 }} $$ (15) (2) Uncertainty caused by fR′
Based on uncertainty analysis, the combined stand uncertainty of fR′ can be expressed as1
$$ u\left( {f_R^{'}} \right) = \sqrt {{{\left( {\frac{{{\sigma _{axial}}}}{{\sqrt 3 }}} \right)}^2} + {{\left( {\frac{{{\sigma _{offset}}}}{{\sqrt 3 }}} \right)}^2} + 4\left[ {{{\left( {\frac{{{\sigma _{DMI}}}}{{\sqrt 3 }}} \right)}^2} + {{\left( {\frac{{{\sigma _{\Delta L1}}}}{{\sqrt {20} }}} \right)}^2}} \right]} $$ (16) where σoffset is the detector offset error, σaxial the alignment error, and σDMI the distance measurement error. These errors are discussed in detail in Ref. 40. In addition, σΔL1 is the stand uncertainty of ΔL1 from 10 measurements.
(3) Uncertainty caused by l
The causes of uncertainty in l are the errors caused by two detectors with different offsets, the distance measurement error, and the axis alignment error.
$$ u\left( l \right) = \sqrt {{{\left( {\frac{{{\sigma _M}}}{{\sqrt 3 }}} \right)}^2} + {{\left( {\frac{{{\sigma _{\alpha ,\beta }}}}{{\sqrt 3 }}} \right)}^2} + {{\left( {\frac{{{\sigma _L}}}{{\sqrt 3 }}} \right)}^2} + {\sigma ^2}_l} $$ (17) where σα,β is the measurement error caused by misalignments between axes; σL is the measurement error of the distance between positions A and B, which can be measured using an XL-80 Renishaw interferometer; and σM is the error caused by two detectors with different offsets.
Considering the effects of the three uncertainties, i.e., u(fR′), u(d0), and u(l), the total combined stand uncertainty u(fT′) is
$$ {u_{rel}}(f_T^{'}) = \frac{{\sqrt {{{\left[ {\dfrac{{\partial f_T^{'}}}{{\partial {d_0}}}u\left( {{d_0}} \right)} \right]}^2} + {{\left[ {\dfrac{{\partial f_T^{'}}}{{\partial f_R^{'}}}u\left( {f_R^{'}} \right)} \right]}^2} + {{\left[ {\dfrac{{\partial f_T^{'}}}{{\partial l}}u\left( l \right)} \right]}^2}} }}{{f_T^{'}}} \times 100\% $$ (18) Based on the above uncertainty components, the uncertainty analysis of the lens with focal length of 10452.21 mm has a related standard uncertainty of 0.034%, and the experimental measurement results have a relative standard deviation of 0.019%. Thus, the result of the uncertainty analysis is identical to that of the experiments.
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(1) Uncertainty component u(L1)
Considering the uncertainty components of ultra-large curvature radius, the combined uncertainty u(L1) can be obtained as follows
$$ u\left( {{L_1}} \right) = \sqrt {u\left( {{L_1}} \right)_{axial}^2 + u{{\left( {{L_1}} \right)}^2}_{of f set} + u{{\left( {{L_1}} \right)}^2}_{DMI} + u{{\left( {{L_1}} \right)}^2}_{\sigma 1}} $$ (19) where u(L1)axial is the uncertainty caused by axial-misalignment errors, u(L1)offset the uncertainty caused by two detectors with different offsets, u(L1)DMI the uncertainty caused by position-measurement errors, and u(L1)σ1 the uncertainty observed from repeated measurements.
(2) Uncertainty component u(L2)
The uncertainty u(L2) due to the position difference L2 of reflector can be written as
$$ u\left( {{L_2}} \right) = \sqrt {\frac{1}{2}\left[ {{{\left( {\frac{{{\sigma _{axial}}}}{{\sqrt 3 }}} \right)}^2} + {{\left( {\frac{{{\sigma _{of f set}}}}{{\sqrt 3 }}} \right)}^2} + {{\left( {\frac{{{\sigma _{DMI}}}}{{\sqrt 3 }}} \right)}^2}} \right] + {{\left( {\frac{{{\sigma _{L2}}}}{{\sqrt {10} }}} \right)}^2}} $$ (20) where σoffset is the error caused by two detectors with different offsets, σaxial the alignment error, and σDMI the distance measurement error. These errors are discussed in detail in Ref. 38. In addition, σL2 is the standard deviation of ΔL2 from the careful adjustments and experiments.
Assuming the aforementioned uncertainty components of the radius R for the tested lens measurements are independent of each other, the relative combined measurement uncertainty in large-aperture laser differential confocal interferometry can be obtained using Eq. 22 as follows
$$ {u_{rel}}(R) = \frac{{\sqrt {{{\left[ {{c_1}u\left( {{L_1}} \right)} \right]}^2} + {{\left[ {{c_2}u\left( {{L_2}} \right)} \right]}^2}} }}{R} \times 100\% $$ (21) Where c1 and c2 are the uncertainty transfer coefficients of L1 and L2, respectively.
Based on the above uncertainty components, the relative uncertainty of large-aperture laser differential confocal interferometry is expected to be less than 0.0038% for a tested lens with a radius of approximately −14792.38 mm and a relative standard deviation of 0.0036%. The results of the uncertainty analysis are in good agreement with the experimental results.
Research on high-precision large-aperture laser differential confocal-interferometric optical element multi-parameter measurement method
- Light: Advanced Manufacturing , Article number: (2024)
- Received: 09 March 2024
- Revised: 21 August 2024
- Accepted: 23 August 2024 Published online: 16 October 2024
doi: https://doi.org/10.37188/lam.2024.047
Abstract: To fulfill the requirements of high-precision common baseline measurement for multiple parameters, such as surface profiling and the curvature radius of large-aperture optical elements on the same instrument, this paper proposes a research on a high-precision large-aperture laser differential confocal-interferometric measurement method. This method is based on the principle of laser differential confocal combined with interferometry. It utilizes a Galilean double-reflection collimation system to generate well large-aperture collimated beams and employs mechanical phase-shifting technology for large-aperture and heavy-load reference lenses to overcome the flaws of existing large-aperture wavelength-tuning phase shifting technology in theory, thus achieving high-precision and high-stable phase-shifting interference in large-aperture surface profiling measurements. By utilizing the laser differential confocal method with anti-scattering and anti-interference properties, high-precision common baseline measurements are achieved for the multiple-parameter of optical elements such as ultra-long focal lengths and ultra-large curvature radii. The measurements of large-aperture surface profiles, the mean PV was 46.0 nm. For the ultra-long focal length, the relative standard deviation was 0.019%, whereas for the ultra-large curvature radius, the relative standard deviation was 0.0036%. This method enables high-precision, high-stable, and high-efficient common baseline measurements for the multiple parameters of optical elements with large, medium, and small apertures thereby providing an effective technical approach for improving the detection and machining precision of optical elements.
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