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Profilometry with compact single-shot low-coherence time-domain interferometry
Molly Subhash Hrebesh *, Yuuki Watanabe, Manabu Sato
Graduate School of Science and Engineering, Yamagata University, 4-3-16 Jonan, Yonezawa, Yamagata 992-8510, Japan
a r t i c l e i n f o
Article history:
Received 2 February 2008
Received in revised form 19 May 2008
Accepted 4 June 2008
Keywords:
Interferometry
Profilometry
Height measurement
Optical instrument
Metrology
Polarization
Low-coherence
Shape measurement
a b s t r a c t
We describe the performance of a compact single-shot low-coherence interferometric scheme that can be
capable of measuring three-dimensional surface profiles and shape. This technique utilizes a polarizing
Michelson interferometer and a four-channel polarization phase-stepper optics, which is based on a
paired wedge prism, a combined wave plate and a Wollaston prism. The coherence gated surface image
can be calculated by the simultaneous acquisition of two interferograms and a DC image on a single CCD
camera. The image calculation is based on a novel algorithm to calibrate the imbalanced intensity as well
as the deviated arbitrary relative phase of each of the imaging channels. The system can display the trans-
verse cross-sectional images in real-time. To demonstrate the feasibility of this system, a Japanese coin is
presented as a 3-D shape measurement example with an image size of 4 mm (horizontal) 4 mm (ver-
tical)160 lm (depth).
2008 Elsevier B.V. All rights reserved.
1. Introduction
Optical interferometric schemes can allow a variety of surface
measurements from optical elements such as mirrors to highly
scattering biological specimens with very high resolution. Numer-
ous type of interferometric techniques have been reported using
many kinds of light sources coupled to the interferometer, and
the way to analyze the interference patterns [1,2]. Laser based
phase-shifting interferometry (PSI)[3] can perform three-dimen-
sional (3-D) surface measurements with subnanometer resolution
by analysis of a few sequences of phase-shifted monochromatic
interferograms. PSI can be accomplished either by sequentially
introducing a temporal phase-shifting method or by spatially split-
ting the beam into parallel channels for simultaneous phase-shift-
ing method. In conventional temporal phase-shifting
interferometry, the interferometers have an element to introduce
three or more known phase shifts in the path of the reference light.
Measuring the interference image at each of these phase shifts and
by analyzing, the phase distribution of signal lights can be quanti-
tatively calculated. However, the interferometer using temporal
phase-shifting method is very sensitive to vibration, because the
various phase-shifted frames of interferometric data are taken at
different times and vibration causes the phase shift between the
data frames to be different from the desired value. Instead, in
simultaneous phase-shifting interferometry, the spatially phase-
shifted three or four interferograms were simultaneously acquire
in a time several order of magnitude less than temporal phase-
shifting, thus eliminates the measurement errors caused by the
sample vibrations or movements.
Several types of simultaneous phase-shifting method have been
developed over the years and these techniques utilize conventional
beam splitters and polarization optics to produce three or four
phase-shifted images on a single or multiple charge coupled device
(CCD) for simultaneous acquisition [4,5]. Most of these methods re-
quire relatively complex optical and electronic arrangements and
have had limited practical applications. Recently, novel simulta-
neous PSIs that uses diffractive elements to simultaneously image
three or more interferograms on to a single CCD sensor have been
reported by several authors[68]. These techniques are consider-
ably more compact and less expensive compare to the multi-cam-
era arrangement. However, the diffractive elements are available
only over a small spectral band due to dispersion and chromatic
distortion inherent in their design. Thus they are not capable of
working with white light or short coherence length source interfer-
ometers [9]. More recently, single-shot PSI based on pixellated
phase mask was introduced in which micropolarizers were used
to spatially multiplex the phase-shifted interferograms [10,11]
and which works well over a large wavelength band. However,
such type of phase mask is difficult to manufacture accurately
and need highly sophisticated technologies[9].
The monochromatic PSI technique using coherent light source
degrades the accuracy for rough and discontinuous surfaces be-
cause of the occurrence of speckle and phase ambiguity problem,
0030-4018/$ - see front matter 2008 Elsevier B.V. All rights reserved.doi:10.1016/j.optcom.2008.06.004
* Corresponding author.
E-mail address: [email protected](M.S. Hrebesh).
Optics Communications 281 (2008) 45664571
Contents lists available at ScienceDirect
Optics Communications
j o u r n a l h o m e p a g e : w w w . e l s e v i e r . c o m / l o c a t e / o p t c o m
mailto:[email protected]://www.sciencedirect.com/science/journal/00304018http://www.elsevier.com/locate/optcomhttp://www.elsevier.com/locate/optcomhttp://www.sciencedirect.com/science/journal/00304018mailto:[email protected]7/24/2019 Hrebesh_Jurnal
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respectively. Scanning white light interferometry (WLI) [12,13]
overcomes this limitation and which is one of the most commonly
used method for 3-D shape measurement. In WLI the interference
patterns can be treated by two ways in order to get the surface and
subsurface information of a sample. The first way processes inter-
ferograms by phase calculation algorithm to provide a resolution
better than 1 nm[14,15]. The second way consists of analyzing
the fringe visibility, and this technique named optical coherencetomography (OCT) is widely used for getting depth resolved infor-
mation from highly scattering biological specimens[16]with spa-
tial resolutions of the order of 10 lm. In OCT the depth or height
information are given by the position of the reference mirror. How-
ever, each measurement techniques has its own unique
advantages.
Recently, there is considerable interest in wide-field (full-field)
coherence gated imaging by means of light source with short
coherence length for many applications, which can acquire trans-
verse cross-sectional (en-face) images of biological tissues and
materials with high resolution. Wide-field (full-field) OCT consist
of 2D interferometer with CCD camera were used to obtain en-face
sectional image. A single-shot phase-stepped wide-field OCT utiliz-
ing simultaneous phase-shifting optics and a single CCD camera
has been reported[17], which can allow the reconstruction of 3-
D depth resolved object profiles and shape with high time resolu-
tion. Using this technique the measurement of optical phase distri-
bution is also demonstrated. The temporal resolution of the system
depends only on the frame rate of the CCD camera. However, the
four-channel phase-stepper optics in the proposed system is quite
complicated for practical implementation. Moreover, the image
reconstruction algorithm requires geometric (image position and
magnification) correction and non-uniformity compensation
parameters for the accurate reconstruction of theen-face OCT im-
age, and this correction parameters were determined by manually.
In this paper, we describe the performance of a compact low-
coherence single-shot spatial phase-stepping interferometeric
technique for 3-D shape measurement. The technique is based on
a polarizing Michelson interferometer and a four-channel polariza-
tion stepper optics, which uses a paired wedge prism (PWP) and a
combined wave plate (CWP) for capturing 4 images simultaneously
on a single CCD camera. The fundamental characteristics of this
system such as shifted relative phase, intensity ratio and spatial
resolutions have already been reported [18]. The main objective
of this paper is to demonstrate the feasibility of this single-shotlow-coherence interferometer for practical applications such as
profilometry and 3-D shape measurement. This technique need
only two quadraturely phase-stepped interferograms and a DC im-
age for extracting the interferometric component. Moreover, this
technique is simple, compact and more robust than that of the pre-
viously reported studies.
2. Basic principle of single-shot interferometry
2.1. Optical scheme
Fig. 1 shows the schematic of the experimental setup. The
experimental setup consists of a 2D polarizing Michelson interfer-
ometer followed by four-channel phase stepper optics. The light
from an LED (Hitachi, HE8404SG) with a central wavelength (k0)
of 846 nm and a spectral bandwidth (Dk) of 46 nm (FWHM) is par-
tially collimated using lens L1 (focal length 12 mm). The calculated
coherence length [lc= 0.44(k0)2/Dk] of the source was around
6.9 lm. Using a polarizer (P-1), the light is linearly polarized at
+45 and is coupled to the polarization interferometer. The inter-
ferometer is based on a free-space Michelson configuration with
a nonpolarizing beam splitter (NPBS), which splits the incoming
light into two. After the round-trip transmission through the pola-
rizer (P-2) in the sample arm, the signal light is linearly polarized
at an angle of +45 at the output of the interferometer. Similarly,
at the reference arm the reference light becomes right circularly
polarized after the round-trip transmission through the polarizer
Fig. 1. Experimental setup: P1P3: polarizers, L1L3: lenses, QWP: quarter wave plate, HWP: half-wave plate, RM: reference mirror, PWP: paired wedge prism, WP:Wollaston prism and CWP: combined wave plate. Inset shows the CCD image acquired with a USAF test chart as object.
M.S. Hrebesh et al./ Optics Communications 281 (2008) 45664571 4567
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(P-3) and the quarter wave plate (QWP) with its fast axis oriented
at 0with respect to thex-axis, then at the out put of the interfer-
ometer the polarization state become left circular because of the
reflection by the nonpolarizing beam splitter.
At the output of the interferometer, a four-channel phase-step-
per optics is constructed, which consists of a relay optic with lens
L2 (focal length 125 mm) and L3 (focal length 75 mm), a PWP, a
CWP, and a Wollaston prism (aperture 1515 mm
2
, separationangle 4.8). The PWP is fabricated using two wedge prisms with
a deviation angle of 1, as shown inFig. 1, which perform the ver-
tical splitting of the incoming beam inxzplane. The distance be-
tween the sample and the objective lens L2 is the focal length of
the lens L2. The PWP is aligned with L2 at a distance of 162 mm
to obtain uniform images.
The CWP consists of two-quarter wave plates, QWP1 (size
1020 mm2) and QWP2 (1010 mm2) with their fast axis ori-
ented at 0and t45, respectively, with respect to thex-axis, and
a half-wave plate (HWP, 1010 mm2) with its fast axis oriented
at 22.5with respect to thex-axis, as shown inFig. 1. The distance
between the CWP and L3 is 118 mm. The distance between L2 and
L3 is kept at 300 mm.
The light exiting from the interferometer is then collimated
onto the input plane of the four-channel phase stepper optics.
The PWP splits the incoming light into up-down direction in the
xz plane, then the up-directed beam from the PWP passed
through QWP 1, and the down-directed beam passes through the
QWP 2 and the HWP 1. The Wollaston prism then splits the incom-
ing beam into two orthogonally polarized components. Finally the
four phase-stepped channels are projected on the CCD (Hamama-
tsu Photonics, C4880-80, 656494 pixels, pixel size
9.99.9 lm2, resolution 12 bit, frame rate 28 frames/s) camera
by the imaging lens L3.
2.2. Principle of phase stepper optics
We analyzed the polarization states of the lights to calculate the
intensities of four spatially splitted images using the Jones matrixand vectors. The electric fields of the signal and reference lights
that enter the phase-stepper can be expressed as:
Signal light (linear + 45),
ESES0ej/Sffiffiffi2
p 11
ES0ej/SJS 1
Reference light (left circular),
ERER0ej/Rffiffiffi2
p 1j
ER0ej/RJR 2
whereES0, ER0, /S, /Rare the amplitudes and phases of signal
and reference lights, respectively. JS and JR represent the corre-
sponding Jones vector for sample and reference arm signals. After
L3, the electric fields of the signal and reference lights for Beam
1 and Beam 2 are given by:
For beam-1 through QWP 1 at 0
EB1S12ES0e
j/SJB1S1
2ES0e
j/S1ffiffiffi
2p 1j
3
EB1R12ER0 e
j/RJB1R1
2ER0e
j/R1ffiffiffi
2p 11
4
For beam-2 through QWP 2 at 45
EB2S12ES0e
j/SJB2S1
2ES0e
j/S1ffiffiffi
2p 1
1
5
EB2R
1
2ER0 e
j/RJB2R
1
2ER0e
j/R1
ffiffiffi2p
1 j
0
6
For beam-2 through HWP 1 at 22.5
E0B2S1
2ES0e
j/SJ0B2S1
2ES0e
j/S1
0
7
E0B2R1
2ER0 e
j/RJ0B2R1
2ER0e
j/R1
2
1 j1 j
8
HereJB1S,JB1R,JB2S,JB2R,J0B2S and J
0B2Rare the Jones vectors of sig-
nal and reference lights for Beam 1 and Beam 2, which can be writ-ten as:
JB1STQWP1JS; JB1RTQWP1JR;JB2STQWP2JS; JB2RTQWP2JR;J
0B2STHWP1JS; J0B2RTHWP1JR 9
where TQWP1, TQWP2 and THWP1 are Jones matrixes for QWP 1
(fast axis at 0 to the x-direction), QWP 2 (fast axis at 45 to the
x-direction) and HWP 1 (fast axis at 22.5 to the x-direction),
respectively, which can be expressed as follows:
TQWP-1 1 0
0 j
; TQWP-21
2
1 j 1 j1 j 1 j
; THWP-1 1
ffiffiffi2
p 1 11 1
10
The Wollaston prism, which laterally separates the incoming
beam into two orthogonal polarization components with a separa-
tion angle. Thus the interferograms of images A to D are calculated
using Jones vector and matrix are represented by
IAE2S
4E
2R
4ESER2
Cos /S/R 11
IBE2S
4E
2R
4ESER
2 Cos/S/R 90
12
ICE2S
8E
2R
8 13
ID3E2S
8 3E
2R
8 1
ffiffiffi2p ESERCos/S/R 45
14
The relative phase of images A and 90, and that of images A andD is 45, and the image C corresponds to the DC intensity of both
the reference and signal lights.
2.3. Image reconstruction
For extracting the interferometric component, we use the two
quadraturely phase-stepped images (image A and image B) and
the DC image C. The basic equation to extract the interference com-
ponents S is given by
Sffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi ffiffiffiffiffiffiffiffiffiffiffiffiIA 2IC2 IB 2IC2
q 15
The intensity ration of the phase-shifted images at the output of
the phase-stepper optics was not exactly same as that of the theo-
retical ration. This unbalanced intensity of each phase-stepped
images will introduce a residual dc-offset intensity in the recon-
structed image. In order to compensate this residual intensity,
we introduce three intensity compensation parameters. Moreover,
a phase calibration parameter is also introduced to compensate the
slight relative phase deviation from 90between image A and im-
age B. Thus the modified algorithm with compensation parameters
is as below:
SMffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi ffiffiffiffiffiffiffiffiffiffiffiACPIA 2CCPIC2 ACPIA 2CCPIC
Sing :Cosg BCPIB 2CCPIC
Sing
2s ;
16whereACP, BCP and CCP are the parameters used to calibrate the
intensities of image A, B and C, respectively. For calculating thesecalibration parameters, after capturing the 3 phase-stepped
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images, the mean intensity of each images were measured and
then the least mean valuehIibetween image A and image B is cal-
culated first. Using this least mean value, the calibration parame-
ters for image A and image B can be obtained as follows;
ACP hIi=hAi; BCP hIi=hBi; 17
After calibrating the intensity of image A and image B, the cal-
ibration parameter for image C is obtained as follows:
CCP hIi=2hCi 18wherehi denote the mean value. Theg in Eq.(16)is the practi-
cal relative phase between image A and B. Our custom software
developed in LabVIEW-IMAQ domain can calculate these intensity
coefficients in real-time. The real-time calculation and compensa-
tion is very essential for practical application, because the mean
intensity of each phase-stepped images should vary during depth
scan. The relative phase parameterg can be feed manually duringmeasurement to reduce the residual fringe in the reconstructed
image. The Image acquisition, calculations of mean image intensi-
ties, image processing of Eq. (16)and the real-time display of the
obtained en-face images can be done with a frame rate of
28 frames/s.
3. Performances
3.1. Basics parameters
For optimizing the system performance, first we aligned to split
the image using a USFA 1951 test target with field of view
33 mm2, the magnification was measured around 0.67, which
is almost corresponded to the calculated value of 0.68 (85 mm/
125 mm). The distance between lens L3 and CCD camera is
85 mm. The horizontal image separation distance on the CCD plane
depends upon the deviation angle of the Wollaston prism and its
distance from the CCD plane. Similarly, the vertical separation dis-
tance depends upon the wedge deviation angle and lens positions.Using a USAF test targetthe relative phasesbetween image A and
B, and between A and D were measured at 88and 37, respectively
by the cross-correlations of intensity profiles of the interferograms.
For a particular alignment condition, the mean pixel intensities for
image A to D were measured at 1540, 1571, 994, and 2242, respec-
tively, and this intensity rations are not exactly same as that of the
theoretical ratio of 1:1:0.5:1.5, in order to compensatethis intensity
unbalance, the corresponding intensity calibration parametersACP,
BCP and CCP were calculated at 1, 0.98 and 0.77, respectively. The
main reason of this intensity imbalance and slight discrepancies in
thephase is dueto theimperfect designof PWPand thetilted optical
beam path through the CWP, respectively.
The axial resolution calculated using the central wavelength
and spectral bandwidth was around 6.9lm, and the measuredone was 10 lm [18]. This incongruity is due to the dispersion
imbalance between the reference and signal lights. For the mea-
surement of lateral resolution en-face image of a standard USAF
1951 test target was taken and could be distinguish the 5th groups
6th elements, which correspond to a lateral resolution of 35 lm.
The lateral resolution is limited by the CCD pixel size and the
low magnification of the optical system.Fig. 2shows the four spa-
tially splitted phase-stepped images A to D of a Japanese 5-yen
coin as the test sample.
3.2. Imaging of rough surface
To demonstrate the imaging capability of this system, we mea-
sured the depth resolveden-faceimages of the surface imprint of a5-yen Japanese coin. The coin is made of 70% of Cu and 30% of Zn.
The measured kanji imprint is marked (44 mm2) inFig. 3. The
irradiation power was nearly 120 lW at the sample surface and
the exposure time set was 7 ms. The input relative phasegwas ad-justed at 88to obtain residual fringe free image. For verifying the
influence of the implemented intensity compensation algorithm,
we obtain the coherence gated image of the bottom surface of
the coin with and without the intensity parameters.Fig. 4a and b
shows the coherence gated bottomen-facesurfaces and its profiles
of a coin with and without the intensity parameters, respectively.
By using the intensity compensation algorithm the dc-offset inten-sity could be reduced by a factor of 10 times.
Fig. 5a and b shows coherence gated en-face surface profile
images of the top and bottom surface of the coin, respectively.
The size of the field of view was 44 mm2 (200200 pixels) as
shown by white square mark in Fig. 2 with a magnification of
0.5. For measuring the 3-D volumetric image, eachen-face images
were sequentially acquired by scanning the reference mirror along
the optical axis with a high precision motorized translation stage.
Fig. 6shows the 3-D volumetric image of the kanji imprint recon-
structed by a stack of 160en-faceimages with a depth scan interval
of 1 lm. When the coherence gate is above the top surface, ideally
the measured image must be null. However, due to the depolariza-
Fig. 2. Four spatially splitted image of a 5-yen Japanese coin with a field of view of
44 mm2 and the pixel size of each channel is 200 200 pixels.
Fig. 3. (a) Image of a Japanese 5-yen coin. The black rectangular mark shows themeasured area and (b) shows the enlarged image.
M.S. Hrebesh et al./ Optics Communications 281 (2008) 45664571 4569
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tion and specular reflection at the rough surface, there was an
influence of background image and which exist constantly through
out the scanning range. In order to alleviate this problem, thatbackground image was subtracted from all of calculated images.
The measured height between top and bottom was 80 lm. The
accuracy of the measurement is mainly depends upon the orienta-
tion and alignment condition of CWP and PWP, pixel match of the
phase-shifted interferograms and g, the practical relative phase be-tween image A and B. Once the alignment conditions were opti-
mized, a 3-D shape measurement can be performed with the
same accuracy and repeatability without any vibration control.
4. Summary
We have presented a compact surface measurement system
using the simultaneous capture of two phase-shifted interfero-
grams and a DC image. We measured the axial and lateral resolu-tion at 10 lm and 35 lm, respectively using an LED with a central
wavelength of 846 nm. Compared to the previously reported sim-
ilar techniques, this technique needs only three images for extract-
ing the interferometric components and it uses relatively more
simple image reconstruction algorithm. Moreover, it presents the
advantages of more compactness and robustness. The system is
also compactable for using cheap thermal sources. The feasibility
of imaging rough surfaces has been demonstrated with an expo-
sure time of 7 ms, a frame rate of 28 frames/s and a field of view
of 44 mm2 (200200 pixels). Furthermore, the better optical
design of CWP and PWP, and the use of high power broadbandoptical source may improve the sensitivity of this system for appli-
Fig. 4. Reconstructed surface images and its profiles of the bottom surface of the coin: (a) without intensity compensation parameter and (b) with intensity compensation
parameters. The intensity profiles are corresponding to the black solid lines in the figures.
Fig. 5. (a) and (b) are the reconstructed depth resolved images of top and bottom
surfaces, respectively.
Fig. 6. The reconstructed 3-D volume rendered image of a set of 160 en-faceplanes
measured.
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cations such as optical ranging or full-field OCT (FF-OCT) with high
time resolution.
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