1. Introduction
Wavefront sensor (WFS) is one of the key parts in adaptive optics system, and its measurement accuracy decides the wavefront controlling ability of the system [
1J. W. Hardy, “Adaptive optics: a progress review,” Proc. SPIE 1542, 2–17 (1991). [CrossRef]
]. The phase diversity wavefront sensor (PD WFS) captures two images, which are on the conventional focal plane and on a diversity plane with a known defocused distance. The images are used to estimate unknown wavefront aberration and object by phase diversity reconstructing algorithm (PD RA). Since the PD WFS was proposed firstly by Gonsalves and Chidlaw in 1979, simple requirement and high accuracy make PD WFS into an attractive candidate as the WFS in adaptive optics [
2R. A. Gonsalves and R. C. Hidlaw, “Wavefront sensing by phase retrieval,” in Applications of Digital Image Processing, Proc. SPIE 207, 32–39 (1979).
]. During the past decades, many authors have used the PD WFS to estimate wavefront aberrations and improve image quality [
3J. H. Seldin, R. G. Paxman, V. G. Zarifis, L. Benson, and R. E. Stone, “Closed-loop wavefront sensing for a sparse-aperture, phased-array telescope using broadband phase diversity,” in Imaging Technology and Telescopes, SPIE 4091, 48–63 (2000).
–
6H. I. Campbell, S. Zhang, A. H. Greenaway, and S. Restaino, “Generalized phase diversity for wave-front sensing,” Opt. Lett. 29(23), 2707–2709 (2004). [CrossRef] [PubMed]
]. In 1999 and 2000, Blanchard
et al described a novel PD WFS comprising a distorted diffraction grating and a single camera, so that series of focal and defocused images can be collected by one camera [
4P. M. Blanchard and A. H. Greenaway, “Simultaneous multiplane imaging with a distorted diffraction grating,” Appl. Opt. 38(32), 6692–6699 (1999). [CrossRef] [PubMed]
,
5P. M. Blanchard, D. J. Fisher, S. C. Woods, and A. H. Greenaway, “Phase diversity wavefront sensing with a distorted diffraction grating,” Appl. Opt. 39(35), 6649–6655 (2000). [CrossRef] [PubMed]
]. In 2004, Campbell
et al introduced a quadratically distorted diffraction grating to image multiple object planes onto a single camera, and proposed an algorithm by a pair of images to reconstruct the wavefront aberration [
6H. I. Campbell, S. Zhang, A. H. Greenaway, and S. Restaino, “Generalized phase diversity for wave-front sensing,” Opt. Lett. 29(23), 2707–2709 (2004). [CrossRef] [PubMed]
].
When the PD WFS works under the monochromatic point source, the wavefront aberrations, especially the high-spatial-frequency components, could cause the energy spread around on the focal and defocused planes. The dispersed intensity distribution contains the wavefront phase information with high-spatial-frequency, and some intensity information will be submerged by the CCD camera’s noise. Then, the measurement accuracy of the intensity images will be degraded, so the measurement ability of the conventional phase diversity wavefront sensor (C-PDWFS) is limited. In other words, if we could increase the precision of the collected images’ information, the accuracy of the reconstructed wavefront must be improved. We employed a modified phase diversity wavefront sensor with a diffraction grating (G-PD WFS) to improve the measurement ability. The diffraction grating is placed before the imaging lens, and it split the incidence beam into a number of beams with different light energy. The different diffraction order spots are output to the CCD camera. The image stitching technology is employed to calculate the intensity distribution on the focus and defocus plane with two or more diffraction spots. The calculated spots contain more information in the lower light level part of original image, which are submersed in noise. In this case, the random wavefront phase can be reconstructed from the new images, and the measurement accuracy can be improved.
In this paper, we build an experimental setup to study the performance of G-PD WFS and compare with C-PD WFS.
2. Principle of the grating phase diversity wavefront sensor
When an object is illuminated with spatially coherent monochromatic light and imaged by a linear shift-invariant system, the image can be approximated by the Fourier transform. Assume that the noise at each detector element is modeled as an additive random variable. The intensity distribution can be represented by
Eq. (1).
where
p is the amplitude of generalized pupil function;
φ is the wavefront aberration to be measured;
φd is the defocused phase function;
FFT{·} is Fourier transform;
n is the additive detector noise;
I’f and
I’d are the intensity distribution on focal and defocused plan without detector noise;
If and
Id are intensity distributions captured by the CCD camera.
In this letter, we adopt the phase diversity reconstructed algorithm (PD RA) which is presented by Naoshi Baba and Kohta Nutoh in 2001, and the error metric can be written as
Eq. (2) [
7N. Baba and K. Mutoh, “Measurement of telescope aberrations through atmospheric turbulence by use of phase diversity,” Appl. Opt. 40(4), 544–552 (2001). [CrossRef] [PubMed]
].
The optical layout of G-PD WFS is shown in
Fig. 1
.
Fig. 1 Schematic diagram of the G-PD WFS. d: defocused distance, B.S.: beam splitter
In experiment, an one-dimensional diffraction grating is employed to divide the incidence beam into a number of beams with the same phase and different intensities. An imaging lens images beams to the focal and defocused planes. A set of diffraction spots, which have different intensities but have the same distribution, are formed. Finally, these images are captured by the CCD cameras.
The shape of the one-dimensional diffraction grating is rectangle with 45
mm width and 60
mm length, and its transmission function can be written as
Eq. (3).
where
Lx,
Ly are the width and length of grating;
rect(
x/2
Lx)
rect(
y/2
Ly) is a two-dimensional rectangular function with a shape function of grating;
f0 is the grating-spatial-frequency and
m is the ratio of transmission function’s peak to valley.
According to the Fraunhofer diffraction formula, the intensity distribution
Ig on the image plane can be approximately as
Eq. (4).
where (
u,
v) is the Cartesian coordinate on the image plane;
λ is the wavelength;
f is the focal length of the imaging lens;
I is the intensity distribution without the diffraction grating;
f0 is the grating-spatial-frequency;
η0 is the ratio of 0th order diffraction spot’s energy to total energy;
η ± 1 is the ratio of ± 1st order diffraction spot’s energy to total energy. From the
Eq. (3), the shape of 0th and ± 1st order spots are the same, while the spots’ center position and energy are different. The ratio of 0th order spot peak value to ± 1st order depends on grating parameters, and denoted by
η (
η =
η0/
η ± 1).
Figure 2
shows the G-PD WFS’ focused image with a uniform plane wavefront. The central and brighter spot is the 0th order diffraction spot, denoted by
Ig0, and the bilateral spots are the ± 1st order diffraction spots. We add the ± 1st order diffraction spots together, then multiplied by
η/2, and the result denoted by
Ig1. Comparing the
Ig0 and
Ig1, Some pixels of the
Ig0 are saturated, so these pixels can’t exactly express the intensity distribution. But the pixels in the surrounding part of the
Ig0 are clearer than
Ig1, and these pixels contain many details of intensity distribution. We use the corresponding pixels in
Ig1 to replace the saturation pixels in
Ig0, and the new image is denoted by
Ig. Obviously,
Ig contains more detailed information.
3. Experiment
3.1 Experimental setup
The experimental setup, which is used to validate the measurement ability of G-PD WFS, is shown in
Fig. 3
. If the diffraction grating is moved out, this experimental setup can be used as the C-PD WFS.
Fig. 3 Experimental setup of G-PD WFS. Lenses are denoted by L prefix, M: reflective mirror, S.F.: spatial filter, Aperture: circle iris, B.S.: beam splitter, LC-SLM: liquid-crystal spatial light modulator, Grating: one-dimensional diffraction grating
The He-Ne laser beam (wavelength: 632.8 nm) is focused by a 40 × microscope objective onto a 10μm diameter pinhole, which is a point source in this system. The diameter of circle iris is 4.6mm. The focal length of L1, L2, L3 are 200mm and the L4 is 250mm.
The LC-SLM can be actuated to introduce a wavefront aberration into the system. The coherent point source is collimated by L1 and incident on the LC-SLM. The reflected light from the LC-SLM contains the wavefront aberration. The incident beam is divided into a number of beams by the diffraction grating, and then imaged onto the CCD camera by lens L4. The CCD camera (Cascade 650) is a 16 bits camera, with a 653 × 492 array of 7.4 μm pixels. Its exposure time for each image are set by integrating until the signal in the brightest pixel of ± 1st order diffraction spots is nearly 50000.
The defocus is the chosen phase diversity function, and the relationship between the diversity distance (
d) and peak-to-valley (
PV) of defocused aberration in wavefront is given by
Eq. (5).
where
λ is the wavelength;
F# is the image space f-number which is 45 is this experiment setup. In our experiment, the CCD camera is fixed on the focal plane. A defocused aberration is added on the LC-SLM to capture the defocused image. The pupil sampling size is calculated by focal length, wavelength, physical size of pupil and CCD camera’s pixel.
Conditional upon the physical size of photosensitive plane, only three diffraction spots (0th order diffraction spot and ± 1st order diffraction spots) can be captured. The energy of 0th order and ± 1st order diffraction spots is stronger than other order spots. Considering the capability of the CCD camera (such as the value of the CCD camera’s gain and the exposure time) and the incident intensity, we decide to collect the intensity image of the 0th order and ± 1st order diffraction spots. The ratio η is determined by the parameters of the diffraction grating. In this experimental setup, the ratio η is 16, which is obtained by a laser power meter. The energy of the 0th order diffraction spot and ± 1st order diffraction spots are measured by the laser power meter separately. Then, the ratio η could be computed.
According to the image processing method of G-PD WFS, the intensity distribution can be obtained from collection data. For processing in PD RA, each intensity distribution is background subtracted.
3.2 Experimental results
In order to validate the usefulness of the diffraction grating for measurement ability, two experiments are performed. The conditions for these two experiments are the same, as following:
where
N2 is the number of image pixels,
∆Ф is the residual wavefront between
Ф and
Ф0.
Fig. 4 Random wavefront aberration Ф0. (a) Phase distribution, (b) The coefficients of Zernike polynomials
The focal and defocused image, which are captured by CCD camera with the diffraction grating, are shown in
Fig. 5(a)
and
Fig. 5(b). The intensity distributions, which are calculated by image processing method, are shown in
Fig. 5(c) and
Fig. 5(d). The images, which are captured by CCD camera when the diffraction grating is moved out, are shown in
Fig. 6(a)
and
Fig. 6(b).
Figure 5(c),
Fig. 5(d) and
Fig. 6 only show the central regions (128 × 128 pixels) in logarithmic scale, and their peak value is normalized to 1 in each image. Applying the PD RA, the measured wavefront (
Fig. 4(a), for 0.3
λ RMS and 2.16
λ PV) can be estimated based on the focal and defocused images.
Fig. 5 Experimental images of G-PD WFS. (a) Captured focal image, (b) Captured defocused image, (c) Calculated focal image, (d) Calculated defocused image
Fig. 6 Experimental images of C-PD WFS. (a) Focal image, (b) Defocused image
Figure 7
shows the estimate wavefront aberrations and residual wavefront with respect to G-PD WFS and C-PD WFS, and
Table 1
lists the associated parameters.
Fig. 7 Experimental results. (a) The estimated wavefront of G-PD WFS, (b) The residual aberration ∆ФG, (c) The estimated wavefront of C-PD WFS. (d) The residual aberration ∆ФC, (e) The Zernike coefficients of ФG and Ф0, (f) The Zernike coefficients of ФC and Ф0, (g) The Zernike coefficients of ∆ФG and ∆ФC
Table 1 Experimental Results of G-PD WFS and C-PD WFS
| G-PD WFS | C-PD WFS |
|---|
Measured Wavefront
| RMS(λ)
| 0.3
|
PV(λ)
| 2.16
|
Estimated Wavefront
| RMS(λ)
| 0.289
| 0.213
|
PV(λ)
| 2.08
| 1.50
|
| Residual Wavefront | RMSE(λ)
| 0.0308
| 0.106
|
| PV(λ) | 0.220 | 0.891 |
Figure 7(a) is the estimated wavefront of G-PDWFS, denoted by
ФG.
Figure 7(b) is the residual aberration between
ФG and
Ф0, denoted by
∆ФG.
Figure 7(c) is the estimated wavefront of C-PD WFS, denoted by
ФC.
Figure 7(d) is the residual wavefront between
ФC and
Ф0, denoted by
∆ФC.
Figure 7(e) is the 65 order Zernike coefficients of
ФG and
Ф0.
Figure 7(f) is the 65 order Zernike coefficients of
ФC and
Ф0.
Figure 7(g) is the differences between the Zernike coefficients of
Ф0 and estimated wavefront
ФG and
ФC.
As can be seen from the estimated wavefront
ФG shown in
Fig. 7(a), it is much better approximate to
Ф0. Comparing the residual aberrations shown in
Fig. 7(b) and
Fig. 7(d),
∆ФG is much smaller. According to the experimental results in
Fig. 7 and
Table 1, as expected, the measurement accuracy of G-PD WFS is improved with the diffraction grating, and it is much better than that of C-PD WFS.
4. Conclusion
In conclusion, a modified PD WFS with the diffraction grating is proposed to improve measurement accuracy. The basic principle of the proposed method and the processing of PD RA are described. The experimental setup of G-PD WFS is also illustrated in detail. It is shown that the diffraction grating is in front of the image lens, and the structural is simple. Under the same conditions, the experiments are done to validate the measurement accuracy of G-PD WFS and compare with C-PD WFS. According to the experimental results, it can be seen that the modified wavefront technology has better measurement accuracy, especially for the wavefront aberration with larger amplitude. It can be use as the WFS in an adaptive optics system.