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Fig. 2 shows a typical layout used for testing large-aperture mirrors with a CGH as the null lens. The surface shape of the equivalent element is obtained by scaling a large-aperture mirror along the optical axis.
First, the surface shape of the large-aperture mirror is discretized to obtain the point set, P. Next, each point in P is transformed in its normal direction to obtain the point set, Q, at the position of the equivalent element. The mathematical description of this transformation is as follows. For concave mirrors, the equivalent transformation factor, d, is inversely proportional to the aperture size of the equivalent element, expressed as
$$ \begin{array}{l}P\left(x,y,{\textit z}\right):\text{ }{\textit z}=f\left(x,y\right),\text{ }\left(x,y\right)\in D\text{.}\\ Q=P\left(x,y,{\textit z}\right)-d\stackrel{\wedge }{n},\text{ with }n=\left(\dfrac{\partial f}{\partial x},\dfrac{\partial f}{\partial y},-1\right),\text{ }\stackrel{\wedge }{n}=\dfrac{n}{\left|n\right|}\end{array} $$ (1) where x, y, and z are the three-dimensional coordinates of the O-XYZ coordinate system, f (x, y) is the surface shape formula of the large-aperture mirror, P is the point set of the surface shape of the mirror, D is the effective aperture area, Q is the set of surface shape points of the equivalent element, n is the direction vector, and d is the equivalent transformation factor.
The surface shape T of the equivalent element is obtained by fitting the point set, Q. A general expression of the surface-fitting formula, which consists of a base function and an optimization polynomial, is expressed as
$$ T{\text{(}}x',y',{\textit z}'{\text{)}}:{\textit z}' = g(x',y') + \sum {{h_i}(x',y')} $$ (2) where x', y', and z' are the three-dimensional coordinates of the fitted surface shape in the O'-X'Y'Z' coordinate system, T is the mathematical expression of the equivalent element fitted by point set Q, g is the base function, and hi is the optimization polynomial.
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An equivalent element of a 3.5 m aspheric concave mirror was designed to verify the accuracy of its CGH. The surface shape of the 3.5 m mirror was defined as
$$ {\textit z}\left( {x,y} \right) = \frac{{\left( {{x^2} + {y^2}} \right)/R}}{{1 + \sqrt {1 - (k+1 )\left( {{x^2} + {y^2}} \right)/R^2} }} + \sum\limits_i^n {{A_i} \cdot {{\left( {{x^2} + {y^2}} \right)}^i}} $$ (3) where x, y, and z are the three-dimensional coordinates of the O-XYZ coordinate system, z (x, y) is the surface shape formula of the large-aperture mirror, R is the vertex curvature radius, k is the conic constant, and Ai is the aspheric coefficient.
Based on the equivalent principle described in the previous section, point set P was first obtained by selecting points at an interval on the ideal surface shape of the 3.5 m mirror. Next, according to Eq. 1, point set P was transformed in the normal direction of each point. During this process, the most crucial step was to determine the value of the equivalent transformation factor, d. Fig. 3 shows the linear relationship between the aperture of the equivalent element and the equivalent transformation factor, d. As shown in Fig. 3, the aperture of the equivalent element decreased as d increased. The equivalent element was positioned 150 mm from the CGH in the optical axis direction to reduce the aperture and reserve space for adjustment.
Fig. 3 Linear relationship between the aperture of the equivalent element and the equivalent transformation factor d.
The equivalent element had an effective aperture of 281 mm, which was approximately 1/12 that of the 3.5 m mirror. The sag of the designed surface shape was approximately 15 mm, which was significantly steeper than that of the 3.5 m mirror. Therefore, a spherical basis function combined with aspheric terms was used to perform surface fitting. The vertex curvature radius, R, was determined to be 660 mm. The aspheric coefficients were calculated using the damped least-squares method, and the first nine even-order aspheric terms were used for surface fitting. The fitting residual was 0.6 nm (RMS), which fully satisfied the subsequent accuracy verification requirements. Based on the design parameters of the equivalent element, a DTM was manufactured with a surface accuracy of RMS λ/60@λ = 632.8 nm, which was equal to that of the 3.5 m mirror.
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The consistency between the error maps obtained using the CGH and LUPHOScan was evaluated based on their surface error compositions. Accordingly, the error maps in Fig. 6a, b were fitted using Zernike standard polynomials. The RMS values of the first ten terms are shown in Fig. 7. The maximum RMS values obtained from the CGH and LUPHOScan tests occurred in the fourth term, indicating satisfactory consistency between the two error maps. “Delta” in Fig. 7 represents the RMS subtraction of the corresponding Zernike terms. The maximum RMS subtraction was 0.78 nm, which corresponded to the sixth term, whereas the other RMS subtractions were all lower 1 nm, further demonstrating the consistency between the two error maps. The RMS subtraction values corresponding to the terms beyond the tenth term (not shown in Fig. 7) were all lower than 1 nm.
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Spatial frequency domain analysis is another effective method for evaluating consistency. Power spectral density (PSD) was initially used to analyze the surface shape error in the frequency domain25. However, the problem with this technique is that the surface shape error over various spatial wavelengths cannot be recognized, limiting an intuitive consistency analysis.
RMSD is a more effective approach for representing the PSD of a two-dimensional isotropic surface because it can intuitively and quantitatively express the surface shape error over various spatial wavelengths26. Eq. 4 is widely used to define the RMSD and expresses its relationship with the PSD.
$$ RMS {D^2}(\alpha ): = 2\pi \cdot \ln 10 \cdot {f^2}(\alpha ) \cdot PS {D_{2Diso}}\left[ {f(\alpha )} \right] $$ (4) where α is the decadic number.
The first ten terms (the zeroth to the third orders of the standard Zernike terms) in Fig. 6a, b were all removed to evaluate the consistency more intuitively. Fig. 8a, b show the residual error maps of the fourth and higher orders of the Zernike terms obtained using CGH and LUPHOScan, with RMS values of 7.9 and 7.5 nm, respectively. Fig. 8c shows the pointwise deviation map of Figs. 8a, b, with an RMS value of 5.5 nm.
Fig. 8 Residual error maps of the fourth and higher orders of Zernike terms obtained using the (a) CGH and (b) LUPHOScan. (c) Their pointwise deviation map.
Fig. 9 shows the RMSD curves of the error maps presented in Fig. 8. “Delta” represents the RMSD curve of the pointwise deviation shown in Fig. 8c. The two error maps demonstrated favorable consistency over the entire frequency band, particularly for the low- to mid-frequency bands below 0.16 mm-1, with an average value of 4 nm. A relatively significant deviation only occurred in the high-frequency band ranging from 0.16 to 0.36 mm−1, with a maximum deviation of 6.8 nm.
Fig. 9 RMSD curves of the error maps shown in Fig. 8.
The high-frequency bands ranging from 0.16 to 0.36 mm−1 in the error maps shown in Fig. 8 were filtered out to investigate this inconsistency. As shown in Fig. 10a, the ring characteristics were assumed to have been introduced via diamond turning. However, in addition to the ring characteristics, spoke-shaped errors were observed along the radial axis, as shown in Fig. 10b. These errors were more significant, as shown in Fig. 10c. The estimated RMS values of the surface errors were used to determine the cause of inconsistencies in the high-frequency bands, as described in the following section.
Fig. 10 High-frequency bands ranging from 0.16 to 0.36 mm−1 in the error maps shown in Fig. 8.
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The RMS values of the surface errors were estimated using the two error maps obtained using CGH and LUPHOScan to reveal the inconsistencies shown in Fig. 10c. This is based on the orthogonality hypothesis, which states that the actual surface shape error, S, and the instrument measurement error, A, are linearly independent27. The orthogonality hypothesis is defined as
$$ \begin{gathered} {T_i} = S + {A_i},{\text{ with }}i = 1,2,...,n. \\ \left\langle {S|{A_i}} \right\rangle = \left\langle {{A_i}|{A_j}} \right\rangle = 0,{\text{ with }}i,j = 1,2,...,n \\ \end{gathered} $$ (5) where T represents each single-sample test map, i and j represent each sequence of test results, and n is the total sampling count.
The RMS value s of the actual surface shape error was then obtained using
$$ s \approx 0.7 \times \sqrt {t_1^2 + t_2^2 - t_{1 - 2}^2} ,{\text{ with }}t_{1 - 2}^2 = \left\langle {{T_1} - {T_2}|{T_1} - {T_2}} \right\rangle $$ (6) Fig. 11 shows the estimated RMSD curve of the surface errors calculated using Eq. 6. Theoretically, the estimated curve did not contain measurement errors27. This curve was consistent with the CGH curve in the frequency band above 0.065 mm. However, the LUPHOScan error map contained additional characteristic peaks. In particular, the differences between the estimated and LUPHOScan curves were more significant in the frequency band ranging from 0.16 to 0.36 mm−1. Moreover, the repeatability curve (LPS-2 in Fig. 11) of LUPHOScan showed that the repeatability worsened in this frequency band, indicating that LUPHOScan could not accurately measure high-frequency surface errors.
Accuracy verification methodology for computer-generated hologram used for testing a 3.5-meter mirror based on an equivalent element
- Light: Advanced Manufacturing 5, Article number: (2024)
- Received: 26 December 2023
- Revised: 13 April 2024
- Accepted: 13 April 2024 Published online: 15 May 2024
doi: https://doi.org/10.37188/lam.2024.025
Abstract: Interferometry with computer-generated holograms (CGHs) is a unique solution for the highly accurate testing of large-aperture aspheric mirrors. However, no direct testing method for quantifying the measurement accuracy of CGHs has been developed. In this study, we developed a methodology for verifying CGH accuracy based on an element that is functionally equivalent to a large-aperture mirror in terms of accuracy verification. The equivalent element decreased the aperture by one or higher orders of magnitude, implying that the mirror could be replaced by a non-CGH technology in a comparison test. In this study, a 281 mm diamond-turned mirror was fabricated as the equivalent element of a 3.5 m aspheric mirror and measured using CGH and LUPHOScan profilometers. Surface error composition and root-mean-square (RMS) density analyses were performed. The methodology verification accuracy of the CGH was 4 nm (RMS) in the low- to mid-frequency bands, with a measured surface accuracy of approximately 10 nm (RMS). This methodology provides a feasible solution for CGH accuracy verification, ensuring high-accuracy and reliable testing of large-aperture aspheric mirrors.
Research Summary
Accuracy verification methodology for computer-generated holograms
Interferometry with computer-generated holograms (CGHs) is a unique solution for the highly accurate testing of large-aperture aspheric mirrors. However, no direct testing method for quantifying the measurement accuracy of CGHs has been developed. In this study, we developed a methodology for verifying CGH accuracy based on an element that is functionally equivalent to a large-aperture mirror in terms of accuracy verification. A 281 mm diamond-turned mirror was fabricated as the equivalent element of a 3.5 m aspheric mirror and measured using CGH and LUPHOScan profilometers. Surface error composition and root-mean-square (RMS) deviation analyses were performed. The methodology verification accuracy of the CGH was 4 nm (RMS) in the low- to mid-frequency bands, with a measured surface accuracy of approximately 10 nm (RMS). This proposed methodology provides a feasible solution for CGH accuracy verification.
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