| Literature DB >> 31412562 |
Hongyang Guo1,2,3, Yangjie Xu1,2,3, Qing Li1,2,3,4, Shengping Du1,2, Dong He1,2, Qiang Wang1,2, Yongmei Huang5,6.
Abstract
In the adaptive optics (AO) system, to improve the effectiveness and accuracy of wavefront sensing-less technology, a phase-based sensing approach using machine learning is proposed. In contrast to the traditional gradient-based optimization methods, the model we designed is based on an improved convolutional neural network. Specifically, the deconvolution layer, which reconstructs unknown input by measuring output, is introduced to represent the phase maps of the point spread functions at the in focus and defocus planes. The improved convolutional neural network is utilized to establish the nonlinear mapping between the input point spread functions and the corresponding phase maps of the optical system. Once well trained, the model can directly output the aberration map of the optical system with good precision. Adequate simulations and experiments are introduced to demonstrate the accuracy and real-time performance of the proposed method. The simulations show that even when atmospheric conditions D/r0 = 20, the detection root-mean-square of wavefront error of the proposed method is 0.1307 λ, which has a better accuracy than existing neural networks. When D/r0 = 15 and 10, the root-mean-square error is respectively 0.0909 λ and 0.0718 λ. It has certain applicative value in the case of medium and weak turbulence. The root-mean-square error of experiment results with D/r0 = 20 is 0.1304 λ, proving the correctness of simulations. Moreover, this method only needs 12 ms to accomplish the calculation and it has broad prospects for real-time wavefront sensing.Entities:
Keywords: adaptive optics; convolutional neural network; deconvolution; machine learning
Year: 2019 PMID: 31412562 PMCID: PMC6720461 DOI: 10.3390/s19163533
Source DB: PubMed Journal: Sensors (Basel) ISSN: 1424-8220 Impact factor: 3.576
Figure 1Architecture of the deconvolution VGG network (De-VGG )network.
Figure 2Working procedure of the De-VGG wavefront sensing approach.
Figure 3Predicting effect of (a) the initial in focus input point spread function (PSF) images; (b) the initial defocus PSF images; (c) the initial wavefront maps; (d) the wavefront maps by the De-VGG predicted for = 20.
Figure 4Predicting effect of (a) the initial in focus PSF images; (b) the initial defocus PSF images; (c) the initial wavefront maps; (d) the wavefront maps by the De-VGG predicted for = 15.
Figure 5Predicting effect of (a) the initial in focus PSF images; (b) the initial defocus PSF images; (c) the initial wavefront maps; (d) the wavefront maps by the De-VGG predicted for = 10.
Figure 6Predicting effect of (a) the initial in focus PSF images; (b) the initial defocus PSF images; (c) the initial wavefront maps; (d) the wavefront maps by the De-VGG predicted for = 6.
Normalized-pixel-mean-square (NPMS) under different test sets of the reconstructed and simulated wavefront.
| Atmospheric Conditions | NPMS (Testing Set) | RMS (Testing Set) |
|---|---|---|
| 0.0067 | 0.1307 λ | |
| 0.0041 | 0.0909 λ | |
| 0.0029 | 0.0718 λ | |
| 0.0025 | 0.0703 λ |
Figure 7Root mean square (RMS) with latency of the stochastic parallel gradient descent (SPGD) algorithm and De-VGG.
Figure 8The schematic diagram (a) and physical map (b) of the optical system used in the experiment. P: Polarizer, SF: Spatial filter, C: Collimator, AD: Aperture stop, BS: 1:1 Spectroscope, CCD: Imaging detector, L: Lens.
Parameters of experimental optics.
| Symbol | Name | Focal Length | Focal Length |
|---|---|---|---|
| L | lens | 200 mm | 50 mm |
| A | aperture diaphragm | N/A | 36 mm |
| BS | 50/50 beam splitter | N/A | 50 mm |
Figure 9Phase maps of (a) the initial wavefront; (b) the wavefront by the De-VGG predicted for = 20.
Figure 10PSF images of (a) the initial in focus plane; (b) the in focus plane by the De-VGG predicted; (c) the initial defocus plane; (d) the defocus plane by the De-VGG predicted for = 20.
The model indicators of the experiment ( = 6).
| Atmospheric Condition | NPMS (Testing Set) | RMS (Testing Set) | Running Time |
|---|---|---|---|
| 0.0066 | 0.1304 | ~12 ms |