Abstract Optical Models for Direct Volume Rendering

合集下载

光学遥感图像小样本舰船目标识别

光学遥感图像小样本舰船目标识别

光学遥感图像小样本舰船目标识别光学遥感图像小样本舰船目标识别摘要:舰船识别在海上安全和海洋经济中具有重要意义。

然而,由于舰船外观的差异性和目标数量的复杂性,舰船目标识别存在着一定的难度。

光学遥感图像中舰船目标种类较多,通常需要大量的数据进行训练,但现实中获取大量舰船图像数据的难度很大。

因此,如何在小样本下实现舰船目标识别便成为了研究的热点。

本文提出了一种基于卷积神经网络(CNN)的小样本舰船目标识别方法。

该方法采用了一种基于注意力机制的循环学习机制,用于进一步提高模型的泛化能力。

经过实验验证,本文提出的方法在光学遥感图像中实现小样本舰船目标识别效果较好,方法准确率达到95.86%。

关键词:光学遥感图像,小样本,舰船目标识别,卷积神经网络,注意力机制,循环学习机制Abstract:Ship identification is of great significance in maritime safety and maritime economy. However, due to the differences in the appearance of ships and the complexity of the number of targets, ship identification has certain difficulties. There aremany types of ship targets in optical remote sensing images, and usually a large amount of data is required for training, but it is difficult to obtain a large number of ship image data in reality. Therefore, how to achieve ship target identification under small samples has become a research hotspot. This paper proposes a small sample ship target identification method based on convolutional neural network (CNN). This method uses a cycle learning mechanism based on attention mechanism to further improve the model's generalization ability. After experimental verification, the method proposed in this paper has a good effect in small sample ship target identification in optical remote sensing images, and the method accuracy reaches 95.86%.Keywords: optical remote sensing, small sample, ship target identification, convolutional neural network, attention mechanism, cycle learning mechanismOptical remote sensing has become an important toolfor maritime security and fishery management. However, identifying ships in optical remote sensing images with a small sample size is a challenging task. In order to address this issue, this paper proposes a ship target identification method based on a convolutional neural network (CNN) with attentionmechanism and cycle learning mechanism.First, the CNN is trained with a small number of samples to improve its generalization ability. Then, an attention mechanism is introduced to enable the network to focus on important features and suppress irrelevant noise. The cycle learning mechanism is employed to further enhance the model's ability to generalize by iteratively updating the model with samples from previous iterations.Experimental results demonstrate that the proposed method achieves a high accuracy of 95.86% in ship target identification in optical remote sensing images with a small sample size. Compared with traditional CNN models, the proposed method can effectively improve the identification accuracy and reduce false positives.Overall, the proposed method provides a practical solution for ship target identification in optical remote sensing images with limited training samples. It demonstrates the potential of deep learning techniques in solving challenging problems in remote sensing applicationsIn addition to ship target identification, deep learning techniques have shown promising results in various remote sensing applications such as land use classification, vegetation mapping, and object detection. However, there are still challenges in applying deep learning to remote sensing data, particularly due to the high dimensionality andlimited availability of labeled samples. Therefore, developing effective deep learning algorithms that can handle small sample sizes and exploit domain-specific features is crucial for advancing remote sensing research.One potential direction for future work is to explore transfer learning methods that transfer pre-trained models from other domains to remote sensing datasets. Transfer learning can help overcome the limitations of limited labeled samples by leveraging knowledge learned from other datasets. For example, pre-trained models on natural images can be fine-tuned on the remote sensing data to improve accuracy and reduce training time. Another promising direction is to investigate more advanced network architectures such as attention-based models that can learn to focus on salient regions of the image and reduce noise interference. Additionally, exploring the integration of multi-source information such as radar and LiDARdata, which have complementary strengths to optical remote sensing data can further enhance the performance of deep learning-based methods.Overall, the application of deep learning techniques to remote sensing data has shown great potential for improving various applications. With the continued development of new algorithms and the availability of more high-quality training data, deep learning will play an increasingly important role in facilitating remote sensing research and applicationsOne area where deep learning has demonstrated significant potential in remote sensing is in land cover and land use classification. These applications are particularly important for environmental management and monitoring, as they provide information on changes in land use patterns, which can affect ecosystem health, urbanization, and agricultural production. Deep learning algorithms have been applied to various remote sensing data sources, including optical and synthetic aperture radar (SAR), to extract features and classify land cover and land use types.In addition to land cover and land use classification, deep learning has also been used to estimate biophysical variables, such as leaf area index,vegetation water content, and biomass. These variables are critical for understanding ecosystem health and productivity and are used in various ecological models. Deep learning techniques, such as convolutional neural networks (CNNs) and recurrent neural networks (RNNs), have been shown to outperform traditional approaches, such as linear regression and decision trees, in estimating these biophysical variables from remote sensing data.Another application of deep learning in remote sensing is in object detection and segmentation. These applications are important in various domains,including environmental monitoring, urban planning, disaster response, and military surveillance. Deep learning algorithms such as region-based CNNs andfully convolutional networks (FCNs) have been developed to automatically detect and segment objects, such as buildings, roads, and water bodies, fromaerial imagery and satellite data. These algorithms have demonstrated high accuracy compared totraditional object detection algorithms, making them ideal for large-scale object detection and segmentation tasks.Finally, deep learning has shown promise in enhancing the performance of remote sensing data fusion. Datafusion involves combining data from multiple sensorsto provide more accurate and comprehensive information. Deep learning techniques such as multilayerperceptrons (MLPs) and deep belief networks (DBNs)have been used to fuse data from different remote sensing sources, including optical, SAR, and LiDAR data. The use of deep learning has enhanced the performance of data fusion algorithms, enabling improved accuracy in classification and estimation tasks.In conclusion, the application of deep learning techniques to remote sensing data has shownsignificant potential for enhancing various applications, including land cover and land use classification, estimation of biophysical variables, object detection and segmentation, and data fusion. With the continued development of new algorithms and training data, deep learning will continue to play a critical role in advancing remote sensing research and applications综上所述,将深度学习技术应用于遥感数据显示出显著的潜力,包括地表覆盖和土地利用分类、生物物理变量估算、目标检测和分割以及数据融合等各种应用。

光学模型介绍英文作文

光学模型介绍英文作文

光学模型介绍英文作文英文:Optical model is a mathematical model that describesthe behavior of light in various media, such as air, water, and glass. It is widely used in the field of optics to predict and analyze the propagation, reflection, refraction, and absorption of light.The optical model is based on the principles of geometrical optics and wave optics. Geometrical optics assumes that light travels in straight lines and obeys the laws of reflection and refraction at the interface between two media. Wave optics, on the other hand, considers light as a wave that can diffract, interfere, and undergo polarization.One of the most important parameters in the optical model is the refractive index, which is a measure of how much a material slows down the speed of light. Therefractive index is different for different materials and can be used to calculate the angle of refraction when light passes through a medium.Another important parameter is the absorption coefficient, which measures how much light is absorbed by a material per unit distance. This is important for designing optical devices such as filters and lenses.In addition to these parameters, the optical model also considers factors such as the thickness of the medium, the angle of incidence, and the polarization state of light. By combining all these factors, the optical model can accurately predict the behavior of light in various scenarios.中文:光学模型是一种描述光在各种介质中行为的数学模型,例如空气、水和玻璃。

光纤photo电导位传感器SSF系列资料说明书

光纤photo电导位传感器SSF系列资料说明书

M18 photoelectric sensors for optical fibresSSF seriesfeaturesweb contents• Application notes • Photos•Catalogue / Manuals• Models with sensitivity adjustment by teach-in button • With range of optical fibres are available • LED status indicator for all versions• Complete protection against electrical damages •Approvals: CE and cULus listedM18 sensors for optical fibres/SS F -0N w ar r a n t yw ar r a n t yWH/2BU/3BK/4BN/1load 1000 mA+dark on teachn.c light on- - + WH/2BU/3BK/4BN/1+dark on teachn.c light on+ - -technical specification(1)Protection guaranteed only with plug cable well mountedSSF/0*-**depending on optical fibresred (660 nm)+ 15 %...- 5 %≤ 10 %5 %10...30 Vdc ≤ 10 %100 mA ≤ 20 mA ≤ 10 µA 2 V maxNPN or PNP - LO / DO selectable800 Hz 150 mspolarity reversal, transient short circuit (autoreset)- 25°C...+ 70°C (without freeze)10 % Sr3,000 lux (incandescent lamp)10,000 lux (sunlight)IP67 (EN60529) (1)yellow Teach-InPBT (plastic), nickel-plated brass (metal)depending on optical fibres1 Nm (plastic housing), 25 Nm (metallic housing)plastic version: 30 g connector / 100 g cable metallic version: 70 g connector / 130 g cablenominal sensing distanceemission tolerance differential travel repeat accuracy operating voltageripple load current no-load current leakage current output voltage dropoutput type switching frequency power on delay power supply protections output electrical protectionstemperature range temperature drift external ligth interferenceprotection degreeLEDssensitivity adjustment housing material optic material tightening torque weight (approximate)WHBK BUBN GYPK electrical diagrams of the connectionsPNPNPNwithe black blue brown graypink In case bothe dark on and remote teach in functions are necessary connect a pull up resistor of 2,2 kΩ between Wh/2 and Bn/1.M18 sensors for optical fibres262SSFplugCubic amplifierunit for optical fibres - DCFS1 seriesfeaturesweb contents• Application notes • Photos•Catalogue / Manuals• Extremely reduced dimensions amplifier units (only 49 x 26 x15 mm)• Right angle cable exit or M12 plug cable for reducing the overall dimensions at minimum • Trimmer for sensivity adjustment• NPN or PNP outputs with selectable NO/NC • Red light beam with visible spot• Wide range of optical fibres (plastics and glass)• Complete protection against electrical damage •Fixing with M4 screws (2xM4, 20 mm step)Cubic amplifier unit for optical fibres - DC/-w ar r a n t yw ar r a n t yWH BKBUBN GYPK NPNPNPWH/2+-BK/4BN/1BU/3+-open/= LOn= DOn+-BN/1BK/4BU/3WH/2+= DOnopen/= LOn-technical specification(1)Protection guaranteed only with plug cable well mounted.FS1/0*-*see optical fibres tablered (660 nm)10...30 Vdc ≤ 10 %100 mA 30 mA 1.2 V maxNPN or PNP - NO / NC selectable1 kHz 200 mspolarity reversal, transient short circuit (autoreset)1 turn trimmer- 25°C...+ 70°C (without freeze)3,000 lux (incandescent lamp)10,000 lux (sunlight)IP65 (EN60529) (1)red (output NO energized)Polyammidedepending by optical fibres50 g connector / 120 g cable (20 g mount bracket)sensing distanceemission operating voltagerippleno-load supply currentload current voltage drop output type switching frequency power on delay power supply protections output electrical protections sensitivity adjustment temperature range external ligth interferenceprotection degreeLEDs housing material optic material weight (approximate)electrical diagrams of the connectionswithe blackblue brown graypink Maximum admissible capacity C=0,2μF, for maximum output voltage and current.IndicationsNO and NC are referred to the diffuse reflection optical fibres (on target absence).For retro-reflective and through-beam models the indication NO to be replaced by NC and NC becomes NO.Cubic amplifier unit for optical fibres - DC266FS1M123421432OUTLO / DO teachFS1/0*-CFS1/0*-E1plugdimensions (mm)2.22617.549M32.64.7M315202.22617.549M39.5M12 x 1M3152018Supply (+)Supply (-)Cubic amplifier unit for optical fibres - DC267FS1Photoelectric sensors for DIN-rail mountingF seriesfeaturesweb contents• Application notes • Photos•Catalogue / Manuals• Models with trimmer sensitivity • Models with Teach-In • Double dgital display • High switching frequency •Approvals: CEPhotoelectric sensors for DIN-rail mounting/F 1R 0code descriptionw ar r a n t yw ar r a n t ypower supply protections technical specificationvalue tabelThe values shown in the following tables are measured, by using our CF/CB1 optical fibre, set to obtain an hysteresis of about 15% with all type of amplifier.glass optical fibres CV series (mm)standard high speed digital F1R/0*-0AF2R/0*-0AF6R/0*-0Adepending on fibre used 36 mmred (680 nm)red (650 nm)≤15 %5 %12...24 Vdc≤10 %< 35 mA< 40 mA50 mA max < 10 μA 1 V maxNPN or PNP - LO / DO selectable200 μs maxON: 20 μs OFF:30 μs1ms≤ 200 ms polarity reversal short circuittrimmer (8 giri)Teach-In -25...+55° C (without freeze)-30...+70° C (without freeze)in conformity with the EMC Directive according to EN 60947-5-210.000 lux (incandescent lamp)20.000 lux (sunlight)IP50 (according to: IEC 60529)orange (output active)green (n.4 - received signal level)red (no received signal)orange (output active)8 bits display (n.4 red: incidentsignal;n.4 green: threshold level)PBT (housing); PC (cover)70 g (approx.)nominal sensing distanceemission diffential travel repeat accuracy operating voltagerippleno-load supply currentload current leakage current output voltage dropoutput type responce time power on delay power supply protections output electrical protections sensitivity adjustment operative Temperature rangestorage temperatureEMCinterference by external lightprotection degreeLEDs housing material weight (approximate)models CV-CB1CV-CB3CV-RB4CV-RB6FF1 series F2 seriesF6 series--7090--410500200240800925Photoelectric sensors for DIN-rail mounting270plastic optical fibres cf series (mm)modular fibres for any application AF series (mm)accessories for CV series optical fibres (mm)F1 seriesF2 seriesF6 seriesON 90 %OFF 90 %ON 90 %OFF 90 %ON 90 %OFF 90 %00000040471518100115100130606830035015018070903003454105002002408009254,0004,0002,4002,800> 4.000 EX.G. = 1250582025901153504001902206006902,2002,6001,6001,900> 4,000 EG = 12series F1series F2series F6model fibres Sn Sn Sn CF-RB3-20400200800CF-RB3-201,5001,0003,000CF-RBA-**CF-RCA-20series F1series F2series F6Sn Sn Sn 1,500700 3.0002,2001,0004,5004,5002,0006,000series F1series F2series F6Sn Sn Sn -20-303,0002,0006,0004,0003,0008,00010,0008,00014,000models CF/CA1CF-CA2CF-CA4CF-RA4CF-RA7CF-CB1CF-CB3CF-RB3CF-RB4CF-RB6CF-RB9CF-RBA CF-CC1CF-RC6CF-RC9CF-RCAmodelsAF/ER9ST28modelsAF/ER4AF/ER5AF/ER6AF/ER7modelsAF/FC1AF/FC2AF/ER1AF/ER2AF/ER3accessories for CF series optical fibres (mm)FPhotoelectric sensors for DIN-rail mounting271Photoelectric sensors for DIN-rail mountingFX seriesfeaturesweb contents• Application notes • Photos•Catalogue / Manuals• Fibre-optic amplifier for DIN-rail mounting (DIN/EN 50022)• Distance setting by means of teach in with additional manual fine adjustment (FX4)• Distance setting by means of 12-turn potentiometer with illuminated scale (FX3)• Adjustable pulse delay and stretching (FX4)• High switching frequency: 1,5 kHz• Ideal for stacking, thanks to 10 mm housing width• Teach 1 (background), Teach 2 (target and background) (FX4)•Large setting range of 20...200 mmPhotoelectric sensors for DIN-rail mountingw ar r a n t yw ar r a n t ytechnical specification(1) Protection guaranteed only with plug cable well mountedFX4/0*-0*FX3/0*-0*see optical fibres table20...200 mm≤ 1 mm-10 % typ.100 x 100 mm whitered (660 nm)NO / NC-light ON LEDs; bar graph LED yellowLED green10 ... 30 Vdc≤ 20% V al / UB≤200 mA≤ 2.0 V a / at 200 mAμ25 mA typ. a / at UB = 24 V≤ 15 mA typ. a / at UB = 24 V≤ 0.1 mA≤ 1,500 Hz≤ 330 μsec15 kHz80 ms300 ms5,000 Lux10,000 LuxTeach-In Potentiometer10 ... 150 msec--25 ... +55 °C0.2 % / °Cbuilt-inIEC 60947-5-2 / 7.4300 m max.17 g connector / 68 g cable18 g connector/ 69 g cableIP64 (EN60529) (1)in conformity with the EMC Directive according to EN 60947-5-2ø 2,2 mmPBTPPVC 4 x 0,25 mm2 / 128 x 0,05 mm øM8 4 wiresnominal sensing distancesetting rangeteach incrementhysteresisstandard targetemitter (regulated light power)output (switchable)excess light outputoutput state indicationexcess light indicatorsupply voltage rangemax. ripple contentoutput currentoutput voltage dropno-load supply currentleakage currentswitching frequencyswitching timemodulation frequencypower on delaymax. ambient light, halogenmax. ambient light, sunsensitivity settingpulse delay/stretchingambient temperature rangetemperature drift of snvoltage reversal protectioninduction protectionshort-circuit protectionshocks and vibrationcable lengthweightprotection degreeEMCoptical fibre connectionhousing materialconnection cable (FX*/0*-0A)connector type (FX*/0*-0F) Photoelectric sensors for DIN-rail mounting274FX3421243BN BK PK BU (1)(4)(2)(3)+ UBA1A2OVloadRL1RL2BN BK PK BU (1)(4)(2)(3)+ UBA1A2OVloadRL1RL2BN BK PK BU (1)(4)(2)(3)+ UBTeach AOVload RLBN BK PK BU (1)(4)(2)(3)+ UBTeachAOVloadRL1WH BKBUBN GYPKFX3/0*-0* NPN outputFX3/0*-0* PNP outputelectrical diagrams of the connectionswithe blackblue brown graypink FX4/0*-0* NPN output FX4/0*-0* PNP outputplugA1 Output (Light-ON/Dark-ON switchable)A2 Excess light output Light-ONM8Photoelectric sensors for DIN-rail mounting275FXFX3/0*-0AFX3/0*-0FFX4/0*-0AFX4/0*-0Fdimensions (mm)13ø 4351042.23.210.8136.32.360319813M8 x 1351042,23,210,8136,32,36031988,513ø 4351042.23.210.8136.32.360319813M8 x 1351042.23.210.8136,32.36031988.5Photoelectric sensors for DIN-rail mounting276FX。

2158 IEEE TRANSACTIONS ON ANTENNAS AND PROP

2158 IEEE TRANSACTIONS ON ANTENNAS AND PROP
[12] O. M. Bucci and M. D. Migliore, “A new method for avoiding the truncation error on near-field antenna measurements,” IEEE Trans Antenna Propag., vol. 54, no. 10, pp. 2940–2952, Oct. 2006.
[11] F. D’Agostino, F. Ferrara, C. Gennarelli, R. Guerriero, and G. Riccio, “An effective technique for reducing the truncation error in the nearfield-far-field trnasformation with plane-polar scanning,” Progr. Electromagn. Res., vol. 73, pp. 213–238, 1996.
[3] M. G. Cote an of bistatic electromagnetic scattering measurements by spherical near-field scanning,” in Proc. AMTA Symp., 1993, p. 191.
[13] F. Ferrara, C. Gennarelli, R. Guerriero, G. Riccio, and C. Savarese, “Extrapolation of the outside near-field data in the cylindrical scanning,” Electromagnetics, vol. 28, pp. 333–345, 2008.

基于optisystem光学传感器阵列的仿真设计的国外文献

基于optisystem光学传感器阵列的仿真设计的国外文献

基于optisystem光学传感器阵列的仿真设计的国外文献IntroductionOptical sensors are widely used in various fields, such as environmental monitoring, medical diagnosis, and industrial applications. Optical sensor arrays, which consist of multiple sensor elements, offer significant advantages in terms of sensitivity, selectivity, and multiplexing capabilities. However, designing and optimizing optical sensor arrays can be a challenging task due to the complex interactions between light and the sensor elements.Simulation tools provide an effective way to study the performance of optical sensor arrays without the need for expensive and time-consuming experimental setups. OptiSystem, a comprehensive software package for designing and simulating optical communication systems, offers a powerful platform for simulating optical sensor arrays. In this review, we provide an overview of the simulation design of optical sensor arrays based on OptiSystem, including the key features of the software, the simulation techniques used, and the applications of optical sensor arrays in different fields.Overview of OptiSystemOptiSystem is a versatile software package developed by Optiwave Systems Inc. It provides a range of tools for designing and simulating optical communication systems, including optical sensors. The software enables users to create complex optical systems by combining optical components such as sources, detectors, fibers, and splitters, and simulate the performance of these systems under different conditions.Key features of OptiSystem include a user-friendly graphical interface, a wide range of built-in optical components, advanced simulation algorithms, and comprehensive data analysis tools. The software also supports a variety of measurement and analysis techniques, such as power spectral density analysis, eye diagram analysis, and bit error rate analysis.Simulation techniques for optical sensor arraysSimulation design of optical sensor arrays based on OptiSystem typically involves the following steps:1. System modeling: The first step in designing an optical sensor array is to model the system architecture using OptiSystem's graphical interface. This involves selecting the appropriate optical components, arranging them in the desired configuration, and setting the operating parameters of the system.2. Light propagation simulation: Once the system architecture is defined, the next step is to simulate the propagation of light through the optical sensor array. OptiSystem uses ray tracing and beam propagation techniques to calculate the transmission and reflection of light at each sensor element, taking into account factors such as refractive index, absorption, and scattering.3. Sensor response simulation: After simulating the light propagation, the next step is to model the response of the sensor elements to the incident light. OptiSystem provides a range of models for different types of sensors, such as photodiodes, photoconductors, and photomultipliers, allowing users to accurately predict the output signal of each sensor element.4. Signal processing and analysis: Finally, the simulated output signals from the sensor elements can be processed and analyzed using OptiSystem's data analysis tools. This allows users to extract useful information from the sensor array, such as the intensity of the incident light, the wavelength of the light, and the spatial distribution of the light.Applications of optical sensor arraysOptical sensor arrays have a wide range of applications in various fields, including:1. Environmental monitoring: Optical sensor arrays can be used to detect pollutants in air and water, monitor the quality of soils, and track environmental changes over time. For example, optical sensor arrays have been used to detect heavy metals in water, monitor greenhouse gases in the atmosphere, and measure the concentration of nutrients in soils.2. Medical diagnosis: Optical sensor arrays can be used for non-invasive medical diagnostics, such as monitoring blood glucose levels, detecting cancer cells, and imaging internal organs. For example, optical sensor arrays have been used to analyze blood samples for diseases, monitor the oxygen saturation in tissues, and image the retinal blood vessels in the eye.3. Industrial applications: Optical sensor arrays can be used for quality control, process monitoring, and product inspection in industrial settings. For example, optical sensor arrays have been used to inspect the surface roughness of machined parts, monitor the temperature of manufacturing processes, and detect defects in semiconductor wafers. ConclusionOptical sensor arrays offer significant advantages in terms of sensitivity, selectivity, and multiplexing capabilities, making them an attractive technology for a wide range of applications. Simulation tools such as OptiSystem provide a powerful platform for designing and optimizing optical sensor arrays, allowing users to study the performance of these systems in a virtual environment before implementing them in real-world applications.In this review, we have provided an overview of the simulation design of optical sensor arrays based on OptiSystem, including the key features of the software, the simulation techniques used, and the applications of optical sensor arrays in different fields. By leveraging the capabilities of OptiSystem, researchers and engineers can develop innovative optical sensor arrays that address pressing challenges in environmental monitoring, medical diagnosis, and industrial applications.。

英国大学电力专业介绍

英国大学电力专业介绍

英国大学电力专业排名、地址及教授介绍1 Cambridge 剑桥大学地址:英格兰剑桥镇网址:教授介绍:主要都是电力电子方向Prof Gehan Amaratunga Director of EPECResearch interests include: Nanoscale materials and device design for electronics and energy conversion. Novel materials and device structures for low cost, high efficiently solar cells. Power electronics for optimum grid connection of large photovoltaic electric generation systems. Integrated and discrete semiconductor devices for power switching and control.Dr Richard McMahon Senior LecturerCurrent research focuses on low maintenance generators for wind turbines; linear generators for wave power and energy efficient power conversion for power supplies and electric appliances such as compact fluorescent lights.Dr Timothy Coombs Heads Superconductivity GroupResearch Interests * Electrical Machines * Electromagnetic Modelling * Engineering Applications of Superconductivity * MEMS2 Southampton 南安普顿大学地址:英格兰南部海滨的Hampshire郡,主校区(Highfield Campus)距离南安普敦市中心3英里网址:教授介绍:以下为主要负责人及链接,无法打开Professor Jan SykulskiElectrical Power Engineering3 Imperial College 伦敦大学帝国理工学院地址:帝国理工主校区坐落于伦敦标准的富人区南肯辛顿网址:教授介绍:Dr Balarko ChaudhuriHis areas of interest are power systems dynamics, stability and robust control. He is actively involved with ABB Corporate Research in the area of wide-area monitoring and control of power systemsProf Goran StrbacProf Strbac's research interests include Power system optimisation and economics; Integration of distributed energy resources and Intermittency.Dr Bikash PalPower System Stability; Dynamic Equivalencing and Coherency; State estimation in power distribution system, Robust Control of Power System Oscillations; FACTS Controllers; Distributed and Renewable Energy Modelling; Grid Integration of Marine Wave Generations; and Risk modelling and assessment in distribution system operation.Dr Imad Jaimoukharobust controller design for structured and unstructured uncertainties; controller reduction; model reduction for large-scale systems; hierarchical optimization in robust controller design, robust control design for power system and fault detection and isolation.4 Surrey 萨里大学地址:位于英国伦敦市郊的吉尔福德网址:教授介绍:没有electrical engineering5 Loughborough 拉夫堡大学地址:位于英格兰中部的拉夫堡镇网址:/教授介绍:Professor Philip C EamesHis research focuses on various aspects of renewable energy systems, energy in buildings and thermal energy storage.Professor Ivor R SmithFor several years recently his research interests have been in the pused power area, where he has been concerned with the Generation, Processing and Application of High-Energy pulsed of electrical energy.Dr Murray ThomsonRenewables into existing electrical power systems. Analysis of low-voltage distribution networks and the development of flexible demand as a means of grid balancing in future low-carbon power systems incorporating high penetrations of intermittent wind, marine and solar powerDr Simon J Watson Head of Wind and Water Power ResearchCondition Monitoring of Wind Turbines; Wind Resource Assessment; Wind Power Forecasting; Wake Modelling; Wave Power Device Modelling; Climate Change Impacts.6 Edinburgh 爱丁堡大学地址:位于爱丁堡市中心,爱丁堡则位于苏格兰海滨,是苏格兰首府网址:/教授介绍:Prof Robin Wallacenetwork integration of distributed renewable energy generation and marine energyProf Janusz BialekPower system economics: Transmission pricing; Modelling electricity markets and security of supply; Congestion management.Sustainable power generation and supply: Future Network Technologies; Flexible Network; Asset Management and Performance in Energy Networks; Autonomous Regional Active Network Management System; Smart Grid Oscillation Management for a Changing Generation Mix. Power systems dynamic and stabilityProf Ian BrydenMarine Renewable EnergyDr Markus MuellerThe design of novel generator topologies for direct drive wave energy, wind energy and tidal current energy converters7 Sheffield 谢菲尔得大学地址:谢菲尔得大学位于约克郡南边的谢菲尔得市网址:教授介绍:Emeritus Professor Barry ChambersSmart electromagnetic structures. Target signature management. Passive and active radar absorbing materials. Conducting polymers and composites. Optimisation using evolutionary computing techniques. Automated microwave measurement systems. Radomes and electromagnetic windows.Emeritus Professor David HoweElectrical technologies for aerospace, automotive and marine applications. High integrity electrical drive systems. Novel electromagnetic devices. Multi-physics modelingProfessor Geraint JewellSelf-bearing electrical machines. Power dense electrical machines and actuators for aerospace and marine applications. Valve actuation. Electromagnetic modelling of novel devices8 Bristol 布里斯托大学地址:大学的几个校园分布在极具活力的现代海滨城市-布里斯托市中心,布里斯托是英格兰西南部最大的城市网址:/教授介绍:Dr Dritan KaleshiCommunications and distributed systems performance; connectivity and performance issues in access and local networks. Self-organised systems, service discovery. Specification of distributed systems; specification conformance testing. Small-device networking, and in particular home networking systems. Interoperability: standardisation and autonomic systems. ICT solutions for SmartGrids and distributed energy management.Dr Dave DruryHardware-in-the-Loop and real-time substructuring (hybrid dynamic) testing methods Aircraft generation and power management systems Hybrid automative vehicle traction and generation systems Efficient control of electric machines Distributed control methods, using industrial purpose built networks and standard ethernet9 York 约克大学地址:约克大学位于历史名城约克郡约克市网址:教授介绍:没有electrical engineering10 Essex 埃塞克斯大学地址:埃塞克斯大学位于英国有史以来最古老的市镇科尔切斯特(Colchester)的郊外两英里处,该镇也是英国的第一个首都网址:主校区:/Southend校区:/southendEast 15 校区:教授介绍:没有electrical engineering11 Bath 巴斯大学地址:巴斯市郊网址:/教授介绍:Dr Miles Alexander Redfernthe control and protection of distribution systemsthe connection of embedded generationintegration of renewable energy systems into utility networks.high speed transient based protection schemescommunications for power system control and protectionnon-invasive techniques for the location of buried utilities.Dr Furong Liall aspects of power system planning, operation, analysis and power system economics.Professor Raj AggarwalProfessor Ag garwal’s research interests are in Electrical Power and Energy Systems. His research group focuses on the technology to support the development of a secure and stable electricity supply network that is able to accommodate new and renewable forms of energy generation.12 Glasgow 格拉斯哥大学地址:格拉斯哥市以西3英里网址:教授介绍:Prof. Enrique Achapower systems analysis and power electronics applications in renewable energy systems.Prof. T.J.E. MillerActive in the Power Systems & Power Engineering research areaProf. John O'Reillyfundamental trade-offs between transient stability and oscillation stability in multi-machine power systems, distributed renewable (wind) generation systems, and distribution level energy control and management.13 Queen's, Belfast 贝尔法斯特女王大学地址:学校位于北爱尔兰首府贝尔法斯特的绿树成荫的南部郊外,步行到市中心只要15分钟网址:教授介绍:Professor Brendan FoxHis interests are in power system analysis, modelling and operation. Current interests include system integration aspects of embedded generation, including wind farms, and power system dynamic stability.Professor Haifeng Wangpower systems modelling, analysis and control with power electronics and renewable generation.14 Leeds 利兹大学地址:利兹市是英格兰北部的金融以及工业中心网址:教授介绍:没有electrical engineering15 University College London 伦敦大学学院地址:伦敦市中心的Bloomsbury广场网址:教授介绍:没有electrical engineering=15 Strathclyde 斯特拉斯克莱德大学地址:格拉斯哥是苏格兰最大的城市,地处苏格兰中部,位于克莱德河两岸网址:/教授介绍:Prof James R McDonaldPower system operation, management and control, protection system analysis, design and modelling, artificial intelligence applications in power systems, energy management systems, electricity pricing techniques, power system planning; optical sensing techniques.Prof Stephen McArthurPower engineering applications of Artificial Intelligence: condition monitoring; diagnostics and prognostics for equipment and plant; active network management and Smart Grids; and monitoring and diagnosis of nuclear reactorsIntelligent and automated power system fault analysisIntelligent system methods: knowledge based systems; model based reasoning; case based reasoningMulti-Agent Systems and Intelligent Agents: agent based condition monitoring; agent based power system fault analysis; multi-agent methods, models, techniques and architectures for power engineering applicationsModel and simulation integrationDecision support environmentsProf Kwok L LoPower systems analysis, planning, operation, monitoring and control including the application of expert systems and artificial neural networks;transmission and distribution management systems and privatisation issues.Prof William E LeitheadDynamic analysis, simulation, modelling, control, integrated drive-train design of wind turbines. Analysis and design of multivariable control system. Analysis and simulation of stochastic systems.Prof David InfieldMy research interests are with electricity generation from renewable energy sources, in particular from wind and photovoltaics (PV), and the integration of these sources into electricity systems large and small. Associated with this central challenge I take an interest in energy storage technology and application, and demand side management.Dr Andrew J CrudenHydrogen and Fuel cell systems, electric vehicles, power electronics for fuel cells and rotating machines (e.g. wind turbines), and electrical machine design.Dr Graham AultDr. Ault's research is in the general area of power system planning and operations with particular emphasis on renewables grid integration, distributed energy resources, distribution systems and long-term transitions and scenarios.17 Manchester 曼彻斯特大学地址:曼彻斯特大学位于地理位置优越的曼彻斯特市中心,曼彻斯特市是伦敦以外英国最重要的商业、教育和文化中心,也是英格兰重要的交通枢纽网址:教授介绍:Prof Daniel Kirschen Head of the Electrical Energy and Power Systems Group in the School of Electrical and Electronic Engineering.The introduction of competitive electricity markets has created a whole new set of interesting and challenging problems in the operation and development of power systems.Prof Jovica MilanovicHis research and consultancy work is equally split between the areas of Power System Dynamics and Power Quality with a common, underlying stream of probabilistic / stochastic modelling of uncertainties of events and system parameters.Prof Vladimir TerzijaMy main research interests are application of intelligent methods to power system monitoring, control, and protection, as well as power system plant, particularly switchgears.=17 Heriot-Watt 赫瑞特瓦特大学地址:主校园位于爱丁堡的郊外。

光电系毕业论文外文翻译半导体激光器适用于毕业论文外文翻译+

光电系毕业论文外文翻译半导体激光器适用于毕业论文外文翻译+

毕业设计(论文)英文翻译姓名学号0811122121所在学院理学院专业班级2008级光信1班指导教师日期2012年4月20日英文原文1.5 Experimental Setup Due to the many concepts and variations involved in performing the experimentsin this project and also because of their introductory nature Project 1 will very likelybe the most time consuming project in this kit. This project may require as much as 9hours to complete. We recommend that you perform the experiments in two or morelaboratory sessions. For example power and astigmatic distance characteristics maybe examined in the first session and the last two experiments frequency andamplitude characteristics may be performed in the second session. A Note of Caution All of the above comments refer to single-mode operation of the laser which is avery fragile device with respect to reflections and operating point. One must ensurethat before performing measurements the laser is indeed operating single-mode.This can be realized if a single broad fringe pattern is obtained or equivalently a goodsinusoidal output is obtained from the Michelson interferometer as the path imbalanceis scanned. If this is not the case the laser is probably operating multimode and itscurrent should be adjusted. If single-mode operation cannot be achieved by adjustingthe current then reflections may be driving the laser multimode in which case thesetup should be adjusted to minimize reflections. If still not operating single-modethe laser diode may have been damaged and may need to be replaced. Warning The lasers provided in this project kit emit invisible radiation that can damagethe human eye. It is essential that you avoid direct eye exposure to the laser beam.We recommend the use of protective eyewear designed for use at the laser wavelengthof 780 nm. Read the Safety sections in the Laser Diode Driver Operating Manual and in thelaser diode section of Component Handling and Assembly Appendix A beforeproceeding.1.5.1 Semiconductor Diode Laser Power Characteristics1. Assemble the laser mount assembly LMA-I and connect the laser to its powersupply. We will first collimate the light beam. Connect the laser beam to a videomonitor and image the laser beam on a white sheet of paper held about two to tencentimeters from the laser assembly. Slowly increase the drive current to the laser andobserve the spot on the white card. The threshold drive current rating of the laser issupplied with each laser. Increase the current to about 10-20 mA over the thresholdvalue. With the infrared imager or infrared sensor card observe the spot on the card andadjust the collimator lens position in the laser assembly LMA-I to obtain a bright spoton the card. Move the card to about 30 to 60 centimeters from the lens and adjust thelens position relative to the laser to obtain a spot where size does not vary stronglywith the position of the white card. When the spot size remains roughly constant asthe card is moved closer or further from the laser the output can be consideredcollimated. Alternatively the laser beam may be collimated by focusing it at adistance as far away as possible. Protect fellow co-workers from accidental exposureto the laser beam.2. Place an 818-SL detector on a post mount assembly M818 and adjust its positionso that its active area is in the center of the beam. There should be adequate opticalpower falling on the detector to get a strong signal. Connect the photodetector to thepower meter 815. Reduce the background lighting room lights so that the signalbeing detected is only from the laser. Reduce the drive current to a few milliamperesbelow threshold and again check to see that room light is not the dominantsignal atthe detector by blocking the laser light.3. Increase the current and record the output of the detector as a function of laser drivecurrent. You should obtain a curve similar to Figure 1.2. If desired the diodetemperature may also be varied to observe the effects of temperature on thresholdcurrent. When examining laser diode temperature characteristics the laser diodedriver should be operated in the constant current mode as a safeguard againstexcessive currents that damage the diode laser. Note that as the diode temperature isreduced the threshold decreases. Start all measurements with the diode current off toprevent damage to the laser by preventing drive currents too high above threshold.To prevent destruction of the laser do not exceed the stated maximum drive current ofthe laser.1.5.2 Astigmatic Distance Characteristics The laser diode astigmatic distance is determined as follows. A lens is used tofocus the laser beam at a convenient distance. A razor blade is then incrementallymoved across the beam to obtain data for total optical power passing the razor edge vs.the razor blade position. A plot of this data produces an integrated power profile of thelaser beam Figure 1.9a which through differentiation exposes the actual powerprofile Figure 1.9b which in turn permits determination of the beam diameter W.A beam diameter profile is obtained by measuring the beam diameter while varyingthe laser position. Figure 1.9c illustrates the two beam diameter profiles of interest:one for razor edge travel in the direction perpendicular to the laser diode junctionplane and the other for travel in the direction parallel to the junction plane. Theastigmatic distance for a laser diode is the displacement between the minima of thesetwo profiles. This method is known as the knife edge technique.1. Assemble the components shown in Figure 1.8 with the collimator lens LC in therotational stage assembly RSA-I placed roughly 1 centimeter away from the laser.The beam should travel along the optic axis of the lens. This is the same lens used incollimating the laser in the previous setup. The approximate placement of all thecomponents are shown in the figure. Make sure that the plane of the diode junctionxz plane in Figure 1.1 is parallel with the table surface.2. Due to the asymmetric divergence of the light the cross-section of the beamleaving the laser and further past the spherical lens is elliptical. The beam thus hastwo distinct focal points one in the plane parallel and the other in the planeperpendicular to the laser diode junction. There is a point between the two focalpoints where the beam cross-section is circular. With the infrared imager and a whitecard roughly determine the position where the beam cross-section is circular. Figure 1.9 – Procedure for finding astigmatic distance.3. Adjust the laser diode to lens distance such that the razor blades are located in thexy plane where the beam cross-section is circular.4. Move the laser diode away from the lens until minimum beam waist is reached atthe plane of razor blades. Now move the laser diode about 200 m further away fromthe lens.5. Move razor blade 1 in the x direction across the beam through the beam spreadθxand record the x position and detected intensity at each increment ≤100 mincrements. The expected output is shown in Figure 1.9. The derivative of this curveyields the intensity profile of the beam in the x direction from which the beamdiameter is determined.6. Repeat with razor blade 2 for θy in the y direction.7. Move the laser closer to the lens in increments ≤50 m through a total of at leastthan 500m. Repeat Steps 5 and 6 at each z increment recording the z position.8. Using the collected data determine the beam intensity profiles in the x and ydirections as a function of the lens position z. This is done by differentiating each dataset with respect to position. Then calculate the beam diameter and plot as a functionof z. The difference in z for the minimum in θx and θy isthe astigmatic distance of thelaser diode. Use of computer software especially in differentiating the data is highlyrecommended. If the laser junction is not parallel to the table surface then for eachmeasurement above you will obtain an admixture of the two beam divergences andthe measurement will become imprecise. If the laser is oriented at 45° to the surfaceof the table the astigmatic distance will be zero. Different laser structures will have different angular beam divergences and thusdifferent astigmatic distances. If you have access to several different laser types gainguided index guided it may be instructive to characterize their astigmatic distances.1.5.3 Frequency Characteristics of Diode Lasers In order to study frequency characteristics of a diode laser we will employ aMichelson interferometer to convert frequency variations into intensity variations. Anexperimental setup for examining frequency and also amplitude characteristics of alaser source is illustrated in Figure 1.10.1. In this experiment it is very possible that light may be coupled back into the laserthereby destabilizing it. An optical isolator therefore will be required to minimizefeedback into the laser. A simple isolator will be constructed using a polarizing beamsplitter cube and a quarterwave plate. We orient the quarterwave plate such that thelinearly polarized light from the polarizer is incident at 45° to the principal axes of thequarterwave plate so that light emerging from the quarterwave plate is circularlypolarized. Reflections change left-circular polarized light into right-circular or viceversa so that reflected light returning through the quarterwave plate will be linearlypolarized and 90° rotated with respect to the polarizer transmission axis. The polarizerthen greatly attenuates the return beam. In assembling the isolator make sure that the laser junction xz plane in Figure1.1 is parallel to the surface of the table the notch on the laser diode case pointsupward and the beam is collimated by the lens. The laser beam should be parallel tothe surface of the optical table. Set the polarizer and quarterwave λ/4 plate in place.Place a mirror after the λ/4 plate and rotate the λ/4 pl ate so that maximum rejectedsignal is obtained from the rejection port of the polarizing beam splitter cube asshown in Figure 1.11. When this signal is maximized the feedback to the laser shouldbe at a minimum.2. Construct the Michelson interferometer as shown in Figure 1.12. Place the beamsteering assembly BSA-II on the optical table and use the reflected beam from themirror to adjust the quarterwave plate orientation. Set the cube mount CM on theoptical breadboard place a double sided piece of adhesive tape on the mount and putthe nonpolarizing beam splitter cube 05BC16NP.6 on the adhesive tape. Next placethe other beam steering assembly BSA-I and the detector mountM818BB inlocation and adjust the mirrors so that the beams reflected from the two mirrorsoverlap at the detector. When long path length measurements are made the interferometer signal willdecrease or disappear if the laser coherence length is less than the two wayinterferometer path imbalance. If this is the case shorten the interferometer until thesignal reappears. If this does not work then check the laser for single-mode operationby looking for the fringe pattern on a card or by scanning the piezoelectric transducerblock PZBin BSA-II and monitoring the detector output which should be sinusoidalwith PZB scan distance. If the laser does not appear to be operatingsingle-moderealign the isolator and/or change the laser operating point by varying the bias current.Additionally to ensure single-mode operation the laser should be DC biased abovethreshold before applying AC modulation. Overdriving the laser can also force it intomultimode operation.3. The Michelson interferometer has the property that depending on the position of themirrors light may strongly couple back toward the laserinput port. In order to furtherreduce the feed-back slightly tilt the mirrors as illustrated in Figure 1.13. If stillunable to obtain single-mode operation replace the laser diode.4. Place a white card in front of the detector and observe the fringe pattern with theinfrared imager. Slightly adjust the mirrors to obtain the best fringe pattern. Try toobtain one broad fringe.5. Position the detector at the center of the fringe pattern so that it intercepts no morethan a portion of the centered peak.6. By applying a voltage to the piezoelectric transducer block attached to the mirrorpart PZB in one arm of the interferometer i.e. BSA-II maximize the outputintensity. The output should be stable over a time period of a minute or so. If it is notverify that all components are rigidly mounted. If they are then room air currents maybe destabilizing the setup. In this case place a box cardboard will do over the setupto prevent air currents from disturbing the interferometer setup.7. Place the interferometer in quadrature point of maximum sensitivity betweenmaximum and minimum outputs of the interferometer by varying the voltage on thePZB.8. The output signal of the interferometer due to frequency shifting of the laser isgiven by I∝φ 2π/c L ν where L is the difference in path length b etween thetwo arms of the interferometer and ν is the frequency sweep of the laser that isinduced by applying a current modulation. Remember that in a Michelsoninterferometer L is twice the physical difference in length between the arms sincelight traverses this length difference in both directions. L values of 3-20 cmrepresent convenient length differences with the larger L yielding higher outputsignals. Before we apply a current modulation to the laser note that the interferometeroutput signal I should be made larger than the detector or laser noise levels byproper choice of L and current modulation amplitude di. Also recall from Section1.3that when the diode current is modulated so is the laser intensity as well as itsfrequency. We can measure the laser intensity modulation by blocking one arm of theinterferometer. This eliminates interference and enables measurement of the intensitymodulation depth. We then subtract this value from the total interferometer output todetermine the true dI/di due to frequency modulation. Apply a low frequency smallcurrent modulation to the laser diode. Note that when the proper range is beingobserved 1 dv 10 5 mA 1 v diand 1 dI 0.2mA 1 I difor the amplitude change only.RecallingdI d(Δφ)2π Δv c dI ∝ΔL 10 5 mA 1 di di cΔi 2πΔLv diordI ΔL 2Kπ mA 1di λ10 -5where K is a detector response constant determined by varying L.9. With the interferometer and detection system properly adjusted vary the drivefrequency of the laser and obtain the frequency response of the laser Figure 1.4 or1.10a.You will need to record two sets of data: i the modulation depth of theinterferometer output as a function of frequency and ii the laser intensitymodulation depth. The difference of the two sets of collected data will provide anestimate of the actual dI/di due to frequency modulation. Also note that if the currentmodulation is sufficiently small and the path mismatch sufficiently large the laserintensity modulation may be negligible. You may need to actively keep theinterferometer in quadrature by adjusting the PZB voltage. Make any necessary function generator amplitude adjustments to keep thecurrent modulation depth of the laser constant as you vary the frequency. This isbecause the function generator/driver combination may not have a flat frequencyresponse. The effect of this is that the current modulation depth di is not constant andvaries with frequency. So to avoid unnecessary calculations monitor the current.。

Secrets of Optical Flow Estimation and Their Principles

Secrets of Optical Flow Estimation and Their Principles

Secrets of Optical Flow Estimation and Their PrinciplesDeqing Sun Brown UniversityStefan RothTU DarmstadtMichael J.BlackBrown UniversityAbstractThe accuracy of opticalflow estimation algorithms has been improving steadily as evidenced by results on the Middlebury opticalflow benchmark.The typical formula-tion,however,has changed little since the work of Horn and Schunck.We attempt to uncover what has made re-cent advances possible through a thorough analysis of how the objective function,the optimization method,and mod-ern implementation practices influence accuracy.We dis-cover that“classical”flow formulations perform surpris-ingly well when combined with modern optimization and implementation techniques.Moreover,wefind that while medianfiltering of intermediateflowfields during optimiza-tion is a key to recent performance gains,it leads to higher energy solutions.To understand the principles behind this phenomenon,we derive a new objective that formalizes the medianfiltering heuristic.This objective includes a non-local term that robustly integratesflow estimates over large spatial neighborhoods.By modifying this new term to in-clude information aboutflow and image boundaries we de-velop a method that ranks at the top of the Middlebury benchmark.1.IntroductionThefield of opticalflow estimation is making steady progress as evidenced by the increasing accuracy of cur-rent methods on the Middlebury opticalflow benchmark [6].After nearly30years of research,these methods have obtained an impressive level of reliability and accuracy [33,34,35,40].But what has led to this progress?The majority of today’s methods strongly resemble the original formulation of Horn and Schunck(HS)[18].They combine a data term that assumes constancy of some image property with a spatial term that models how theflow is expected to vary across the image.An objective function combin-ing these two terms is then optimized.Given that this basic structure is unchanged since HS,what has enabled the per-formance gains of modern approaches?The paper has three parts.In thefirst,we perform an ex-tensive study of current opticalflow methods and models.The most accurate methods on the Middleburyflow dataset make different choices about how to model the objective function,how to approximate this model to make it com-putationally tractable,and how to optimize it.Since most published methods change all of these properties at once, it can be difficult to know which choices are most impor-tant.To address this,we define a baseline algorithm that is“classical”,in that it is a direct descendant of the original HS formulation,and then systematically vary the model and method using different techniques from the art.The results are surprising.Wefind that only a small number of key choices produce statistically significant improvements and that they can be combined into a very simple method that achieves accuracies near the state of the art.More impor-tantly,our analysis reveals what makes currentflow meth-ods work so well.Part two examines the principles behind this success.We find that one algorithmic choice produces the most signifi-cant improvements:applying a medianfilter to intermedi-ateflow values during incremental estimation and warping [33,34].While this heuristic improves the accuracy of the recoveredflowfields,it actually increases the energy of the objective function.This suggests that what is being opti-mized is actually a new and different ing ob-servations about medianfiltering and L1energy minimiza-tion from Li and Osher[23],we formulate a new non-local term that is added to the original,classical objective.This new term goes beyond standard local(pairwise)smoothness to robustly integrate information over large spatial neigh-borhoods.We show that minimizing this new energy ap-proximates the original optimization with the heuristic me-dianfiltering step.Note,however,that the new objective falls outside our definition of classical methods.Finally,once the medianfiltering heuristic is formulated as a non-local term in the objective,we immediately recog-nize how to modify and improve it.In part three we show how information about image structure andflow boundaries can be incorporated into a weighted version of the non-local term to prevent over-smoothing across boundaries.By in-corporating structure from the image,this weighted version does not suffer from some of the errors produced by median filtering.At the time of publication(March2010),the re-sulting approach is ranked1st in both angular and end-point errors in the Middlebury evaluation.In summary,the contributions of this paper are to(1)an-alyze currentflow models and methods to understand which design choices matter;(2)formulate and compare several classical objectives descended from HS using modern meth-ods;(3)formalize one of the key heuristics and derive a new objective function that includes a non-local term;(4)mod-ify this new objective to produce a state-of-the-art method. In doing this,we provide a“recipe”for others studying op-ticalflow that can guide their design choices.Finally,to en-able comparison and further innovation,we provide a public M ATLAB implementation[1].2.Previous WorkIt is important to separately analyze the contributions of the objective function that defines the problem(the model) and the optimization algorithm and implementation used to minimize it(the method).The HS formulation,for example, has long been thought to be highly inaccurate.Barron et al.[7]reported an average angular error(AAE)of~30degrees on the“Yosemite”sequence.This confounds the objective function with the particular optimization method proposed by Horn and Schunck1.When optimized with today’s meth-ods,the HS objective achieves surprisingly competitive re-sults despite the expected over-smoothing and sensitivity to outliers.Models:The global formulation of opticalflow intro-duced by Horn and Schunck[18]relies on both brightness constancy and spatial smoothness assumptions,but suffers from the fact that the quadratic formulation is not robust to outliers.Black and Anandan[10]addressed this by re-placing the quadratic error function with a robust formula-tion.Subsequently,many different robust functions have been explored[12,22,31]and it remains unclear which is best.We refer to all these spatially-discrete formulations derived from HS as“classical.”We systematically explore variations in the formulation and optimization of these ap-proaches.The surprise is that the classical model,appropri-ately implemented,remains very competitive.There are many formulations beyond the classical ones that we do not consider here.Significant ones use oriented smoothness[25,31,33,40],rigidity constraints[32,33], or image segmentation[9,21,41,37].While they deserve similar careful consideration,we expect many of our con-clusions to carry forward.Note that one can select among a set of models for a given sequence[4],instead offinding a “best”model for all the sequences.Methods:Many of the implementation details that are thought to be important date back to the early days of op-1They noted that the correct way to optimize their objective is by solv-ing a system of linear equations as is common today.This was impractical on the computers of the day so they used a heuristic method.ticalflow.Current best practices include coarse-to-fine es-timation to deal with large motions[8,13],texture decom-position[32,34]or high-orderfilter constancy[3,12,16, 22,40]to reduce the influence of lighting changes,bicubic interpolation-based warping[22,34],temporal averaging of image derivatives[17,34],graduated non-convexity[11]to minimize non-convex energies[10,31],and medianfilter-ing after each incremental estimation step to remove outliers [34].This medianfiltering heuristic is of particular interest as it makes non-robust methods more robust and improves the accuracy of all methods we tested.The effect on the objec-tive function and the underlying reason for its success have not previously been analyzed.Least median squares estima-tion can be used to robustly reject outliers inflow estimation [5],but previous work has focused on the data term.Related to medianfiltering,and our new non-local term, is the use of bilateralfiltering to prevent smoothing across motion boundaries[36].The approach separates a varia-tional method into twofiltering update stages,and replaces the original anisotropic diffusion process with multi-cue driven bilateralfiltering.As with medianfiltering,the bi-lateralfiltering step changes the original energy function.Models that are formulated with an L1robust penalty are often coupled with specialized total variation(TV)op-timization methods[39].Here we focus on generic opti-mization methods that can apply to any model andfind they perform as well as reported results for specialized methods.Despite recent algorithmic advances,there is a lack of publicly available,easy to use,and accurateflow estimation software.The GPU4Vision project[2]has made a substan-tial effort to change this and provides executablefiles for several accurate methods[32,33,34,35].The dependence on the GPU and the lack of source code are limitations.We hope that our public M ATLAB code will not only help in un-derstanding the“secrets”of opticalflow,but also let others exploit opticalflow as a useful tool in computer vision and relatedfields.3.Classical ModelsWe write the“classical”opticalflow objective function in its spatially discrete form asE(u,v)=∑i,j{ρD(I1(i,j)−I2(i+u i,j,j+v i,j))(1)+λ[ρS(u i,j−u i+1,j)+ρS(u i,j−u i,j+1)+ρS(v i,j−v i+1,j)+ρS(v i,j−v i,j+1)]}, where u and v are the horizontal and vertical components of the opticalflowfield to be estimated from images I1and I2,λis a regularization parameter,andρD andρS are the data and spatial penalty functions.We consider three different penalty functions:(1)the quadratic HS penaltyρ(x)=x2;(2)the Charbonnier penaltyρ(x)=√x2+ 2[13],a dif-ferentiable variant of the L1norm,the most robust convexfunction;and(3)the Lorentzianρ(x)=log(1+x22σ2),whichis a non-convex robust penalty used in[10].Note that this classical model is related to a standard pairwise Markov randomfield(MRF)based on a4-neighborhood.In the remainder of this section we define a baseline method using several techniques from the literature.This is not the“best”method,but includes modern techniques and will be used for comparison.We only briefly describe the main choices,which are explored in more detail in the following section and the cited references,especially[30].Quantitative results are presented throughout the remain-der of the text.In all cases we report the average end-point error(EPE)on the Middlebury training and test sets,de-pending on the experiment.Given the extensive nature of the evaluation,only average results are presented in the main body,while the details for each individual sequence are given in[30].3.1.Baseline methodsTo gain robustness against lighting changes,we follow [34]and apply the Rudin-Osher-Fatemi(ROF)structure texture decomposition method[28]to pre-process the in-put sequences and linearly combine the texture and struc-ture components(in the proportion20:1).The parameters are set according to[34].Optimization is performed using a standard incremental multi-resolution technique(e.g.[10,13])to estimateflow fields with large displacements.The opticalflow estimated at a coarse level is used to warp the second image toward thefirst at the nextfiner level,and aflow increment is cal-culated between thefirst image and the warped second im-age.The standard deviation of the Gaussian anti-aliasingfilter is set to be1√2d ,where d denotes the downsamplingfactor.Each level is recursively downsampled from its near-est lower level.In building the pyramid,the downsampling factor is not critical as pointed out in the next section and here we use the settings in[31],which uses a factor of0.8 in thefinal stages of the optimization.We adaptively de-termine the number of pyramid levels so that the top level has a width or height of around20to30pixels.At each pyramid level,we perform10warping steps to compute the flow increment.At each warping step,we linearize the data term,whichinvolves computing terms of the type∂∂x I2(i+u k i,j,j+v k i,j),where∂/∂x denotes the partial derivative in the horizon-tal direction,u k and v k denote the currentflow estimate at iteration k.As suggested in[34],we compute the deriva-tives of the second image using the5-point derivativefilter1 12[−180−81],and warp the second image and its deriva-tives toward thefirst using the currentflow estimate by bicu-bic interpolation.We then compute the spatial derivatives ofAvg.Rank Avg.EPEClassic-C14.90.408HS24.60.501Classic-L19.80.530HS[31]35.10.872BA(Classic-L)[31]30.90.746Adaptive[33]11.50.401Complementary OF[40]10.10.485Table1.Models.Average rank and end-point error(EPE)on the Middlebury test set using different penalty functions.Two current methods are included for comparison.thefirst image,average with the warped derivatives of the second image(c.f.[17]),and use this in place of∂I2∂x.For pixels moving out of the image boundaries,we set both their corresponding temporal and spatial derivatives to zero.Af-ter each warping step,we apply a5×5medianfilter to the newly computedflowfield to remove outliers[34].For the Charbonnier(Classic-C)and Lorentzian (Classic-L)penalty function,we use a graduated non-convexity(GNC)scheme[11]as described in[31]that lin-early combines a quadratic objective with a robust objective in varying proportions,from fully quadratic to fully robust. Unlike[31],a single regularization weightλis used for both the quadratic and the robust objective functions.3.2.Baseline resultsThe regularization parameterλis selected among a set of candidate values to achieve the best average end-point error (EPE)on the Middlebury training set.For the Charbonnier penalty function,the candidate set is[1,3,5,8,10]and 5is optimal.The Charbonnier penalty uses =0.001for both the data and the spatial term in Eq.(1).The Lorentzian usesσ=1.5for the data term,andσ=0.03for the spa-tial term.These parameters arefixed throughout the exper-iments,except where mentioned.Table1summarizes the EPE results of the basic model with three different penalty functions on the Middlebury test set,along with the two top performers at the time of publication(considering only published papers).The clas-sic formulations with two non-quadratic penalty functions (Classic-C)and(Classic-L)achieve competitive results de-spite their simplicity.The baseline optimization of HS and BA(Classic-L)results in significantly better accuracy than previously reported for these models[31].Note that the analysis also holds for the training set(Table2).At the time of publication,Classic-C ranks13th in av-erage EPE and15th in AAE in the Middlebury benchmark despite its simplicity,and it serves as the baseline below.It is worth noting that the spatially discrete MRF formulation taken here is competitive with variational methods such as [33].Moreover,our baseline implementation of HS has a lower average EPE than many more sophisticated methods.Avg.EPE significance p-value Classic-C0.298——HS0.38410.0078Classic-L0.31910.0078Classic-C-brightness0.28800.9453HS-brightness0.38710.0078Classic-L-brightness0.32500.2969Gradient0.30500.4609Table2.Pre-Processing.Average end-point error(EPE)on the Middlebury training set for the baseline method(Classic-C)using different pre-processing techniques.Significance is always with respect to Classic-C.4.Secrets ExploredWe evaluate a range of variations from the baseline ap-proach that have appeared in the literature,in order to illu-minate which may be of importance.This analysis is per-formed on the Middlebury training set by changing only one property at a time.Statistical significance is determined using a Wilcoxon signed rank test between each modified method and the baseline Classic-C;a p value less than0.05 indicates a significant difference.Pre-Processing.For each method,we optimize the regu-larization parameterλfor the training sequences and report the results in Table2.The baseline uses a non-linear pre-filtering of the images to reduce the influence of illumina-tion changes[34].Table2shows the effect of removing this and using a standard brightness constancy model(*-brightness).Classic-C-brightness actually achieves lower EPE on the training set than Classic-C but significantly lower accuracy on the test set:Classic-C-brightness= 0.726,HS-brightness=0.759,and Classic-L-brightness =0.603–see Table1for comparison.This disparity sug-gests overfitting is more severe for the brightness constancy assumption.Gradient only imposes constancy of the gra-dient vector at each pixel as proposed in[12](i.e.it robustly penalizes Euclidean distance between image gradients)and has similar performance in both training and test sets(c.f. Table8).See[30]for results of more alternatives. Secrets:Some form of imagefiltering is useful but simple derivative constancy is nearly as good as the more sophisti-cated texture decomposition method.Coarse-to-fine estimation and GNC.We vary the number of warping steps per pyramid level andfind that3warping steps gives similar results as using10(Table3).For the GNC scheme,[31]uses a downsampling factor of0.8for non-convex optimization.A downsampling factor of0.5 (Down-0.5),however,has nearly identical performance Removing the GNC step for the Charbonnier penalty function(w/o GNC)results in higher EPE on most se-quences and higher energy on all sequences(Table4).This suggests that the GNC method is helpful even for the con-vex Charbonnier penalty function due to the nonlinearity ofAvg.EPE significance p-value Classic-C0.298——3warping steps0.30400.9688Down-0.50.2980 1.0000w/o GNC0.35400.1094Bilinear0.30200.1016w/o TA VG0.30600.1562Central derivativefilter0.30000.72667-point derivativefilter[13]0.30200.3125Bicubic-II0.29010.0391GC-0.45(λ=3)0.29210.0156GC-0.25(λ=0.7)0.2980 1.0000MF3×30.30500.1016MF7×70.30500.56252×MF0.3000 1.00005×MF0.30500.6875w/o MF0.35210.0078Classic++0.28510.0078 Table3.Model and Methods.Average end-point error(EPE)on the Middlebury training set for the baseline method(Classic-C) using different algorithm and modelingchoices.Figure1.Different penalty functions for the spatial terms:Char-bonnier( =0.001),generalized Charbonnier(a=0.45and a=0.25),and Lorentzian(σ=0.03).the data term.Secrets:The downsampling factor does not matter when using a convex penalty;a standard factor of0.5isfine. Some form of GNC is useful even for a convex robust penalty like Charbonnier because of the nonlinear data term. Interpolation method and derivatives.Wefind that bicu-bic interpolation is more accurate than bilinear(Table3, Bilinear),as already reported in previous work[34].Re-moving temporal averaging of the gradients(w/o TA VG), using Central differencefilters,or using a7-point deriva-tivefilter[13]all reduce accuracy compared to the base-line,but not significantly.The M ATLAB built-in function interp2is based on cubic convolution approximation[20]. The spline-based interpolation scheme[26]is consistently better(Bicubic-II).See[30]for more discussions. Secrets:Use spline-based bicubic interpolation with a5-pointfilter.Temporal averaging of the derivatives is proba-bly worthwhile for a small computational expense. Penalty functions.Wefind that the convex Charbonnier penalty performs better than the more robust,non-convex Lorentzian on both the training and test sets.One reason might be that non-convex functions are more difficult to op-timize,causing the optimization scheme tofind a poor local(a)With medianfiltering(b)Without medianfilteringFigure2.Estimatedflowfields on sequence“RubberWhale”using Classic-C with and without(w/o MF)the medianfiltering step. Color coding as in[6].(a)(w/MF)energy502,387and(b)(w/o MF)energy449,290.The medianfiltering step helps reach a so-lution free from outliers but with a higher energy.optimum.We investigate a generalized Charbonnier penalty functionρ(x)=(x2+ 2)a that is equal to the Charbon-nier penalty when a=0.5,and non-convex when a<0.5 (see Figure1).We optimize the regularization parameterλagain.Wefind a slightly non-convex penalty with a=0.45 (GC-0.45)performs consistently better than the Charbon-nier penalty,whereas more non-convex penalties(GC-0.25 with a=0.25)show no improvement.Secrets:The less-robust Charbonnier is preferable to the Lorentzian and a slightly non-convex penalty function(GC-0.45)is better still.Medianfiltering.The baseline5×5medianfilter(MF 5×5)is better than both MF3×3[34]and MF7×7but the difference is not significant(Table3).When we perform5×5medianfiltering twice(2×MF)orfive times(5×MF)per warping step,the results are worse.Finally,removing the medianfiltering step(w/o MF)makes the computedflow significantly less accurate with larger outliers as shown in Table3and Figure2.Secrets:Medianfiltering the intermediateflow results once after every warping iteration is the single most important secret;5×5is a goodfilter size.4.1.Best PracticesCombining the analysis above into a single approach means modifying the baseline to use the slightly non-convex generalized Charbonnier and the spline-based bicu-bic interpolation.This leads to a statistically significant improvement over the baseline(Table3,Classic++).This method is directly descended from HS and BA,yet updated with the current best optimization practices known to us. This simple method ranks9th in EPE and12th in AAE on the Middlebury test set.5.Models Underlying Median FilteringOur analysis reveals the practical importance of median filtering during optimization to denoise theflowfield.We ask whether there is a principle underlying this heuristic?One interesting observation is thatflowfields obtained with medianfiltering have substantially higher energy than those without(Table4and Figure2).If the medianfilter is helping to optimize the objective,it should lead to lower energies.Higher energies and more accurate estimates sug-gest that incorporating medianfiltering changes the objec-tive function being optimized.The insight that follows from this is that the medianfil-tering heuristic is related to the minimization of an objective function that differs from the classical one.In particular the optimization of Eq.(1),with interleaved medianfiltering, approximately minimizesE A(u,v,ˆu,ˆv)=(2)∑i,j{ρD(I1(i,j)−I2(i+u i,j,j+v i,j))+λ[ρS(u i,j−u i+1,j)+ρS(u i,j−u i,j+1)+ρS(v i,j−v i+1,j)+ρS(v i,j−v i,j+1)]}+λ2(||u−ˆu||2+||v−ˆv||2)+∑i,j∑(i ,j )∈N i,jλ3(|ˆu i,j−ˆu i ,j |+|ˆv i,j−ˆv i ,j |),whereˆu andˆv denote an auxiliaryflowfield,N i,j is the set of neighbors of pixel(i,j)in a possibly large area andλ2 andλ3are scalar weights.The term in braces is the same as theflow energy from Eq.(1),while the last term is new. This non-local term[14,15]imposes a particular smooth-ness assumption within a specified region of the auxiliary flowfieldˆu,ˆv2.Here we take this term to be a5×5rectan-gular region to match the size of the medianfilter in Classic-C.A third(coupling)term encouragesˆu,ˆv and u,v to be the same(c.f.[33,39]).The connection to medianfiltering(as a denoising method)derives from the fact that there is a direct relation-ship between the median and L1minimization.Consider a simplified version of Eq.(2)with just the coupling and non-local terms,where E(ˆu)=λ2||u−ˆu||2+∑i,j∑(i ,j )∈N i,jλ3|ˆu i,j−ˆu i ,j |.(3)While minimizing this is similar to medianfiltering u,there are two differences.First,the non-local term minimizes the L1distance between the central value and allflow values in its neighborhood except itself.Second,Eq.(3)incorpo-rates information about the data term through the coupling equation;medianfiltering theflow ignores the data term.The formal connection between Eq.(3)and medianfil-tering3is provided by Li and Osher[23]who show that min-2Bruhn et al.[13]also integrated information over a local region in a global method but did so for the data term.3Hsiao et al.[19]established the connection in a slightly different way.Classic-C 0.5890.7480.8660.502 1.816 2.317 1.126 1.424w/o GNC 0.5930.7500.8700.506 1.845 2.518 1.142 1.465w/o MF0.5170.7010.6680.449 1.418 1.830 1.066 1.395Table 4.Eq.(1)energy (×106)for the optical flow fields computed on the Middlebury training set .Note that Classic-C uses graduated non-convexity (GNC),which reduces the energy,and median filtering,which increases it.imizing Eq.(3)is related to a different median computationˆu (k +1)i,j=median (Neighbors (k )∪Data)(4)where Neighbors (k )={ˆu (k )i ,j }for (i ,j )∈N i,j and ˆu (0)=u as well as Data ={u i,j ,u i,j ±λ3λ2,u i,j±2λ3λ2···,u i,j ±|N i,j |λ32λ2},where |N i,j |denotes the (even)number of neighbors of (i,j ).Note that the set of “data”values is balanced with an equal number of elements on either side of the value u i,j and that information about the data term is included through u i,j .Repeated application of Eq.(4)converges rapidly [23].Observe that,as λ3/λ2increases,the weighted data val-ues on either side of u i,j move away from the values of Neighbors and cancel each other out.As this happens,Eq.(4)approximates the median at the first iterationˆu (1)i,j ≈median (Neighbors (0)∪{u i,j }).(5)Eq.(2)thus combines the original objective with an ap-proximation to the median,the influence of which is con-trolled by λ3/λ2.Note in practice the weight λ2on thecoupling term is usually small or is steadily increased from small values [34,39].We optimize the new objective (2)by alternately minimizingE O (u ,v )=∑i,jρD (I 1(i,j )−I 2(i +u i,j ,j +v i,j ))+λ[ρS (u i,j −u i +1,j )+ρS (u i,j −u i,j +1)+ρS (v i,j −v i +1,j )+ρS (v i,j −v i,j +1)]+λ2(||u −ˆu ||2+||v −ˆv ||2)(6)andE M (ˆu ,ˆv )=λ2(||u −ˆu ||2+||v −ˆv ||2)(7)+∑i,j ∑(i ,j )∈N i,jλ3(|ˆu i,j −ˆu i ,j |+|ˆv i,j −ˆv i ,j |).Note that an alternative formulation would drop the cou-pling term and impose the non-local term directly on u and v .We find that optimization of the coupled set of equations is superior in terms of EPE performance.The alternating optimization strategy first holds ˆu ,ˆv fixed and minimizes Eq.(6)w.r.t.u ,v .Then,with u ,v fixed,we minimize Eq.(7)w.r.t.ˆu ,ˆv .Note that Eqs.(3)andAvg.EPE significancep -value Classic-C0.298——Classic-C-A0.30500.8125Table 5.Average end-point error (EPE)on the Middlebury train-ing set is shown for the new model with alternating optimization (Classic-C-A ).(7)can be minimized by repeated application of Eq.(4);weuse this approach with 5iterations.We perform 10steps of alternating optimizations at every pyramid level and change λ2logarithmically from 10−4to 102.During the first and second GNC stages,we set u ,v to be ˆu ,ˆv after every warp-ing step (this step helps reach solutions with lower energy and EPE [30]).In the end,we take ˆu ,ˆv as the final flow field estimate.The other parameters are λ=5,λ3=1.Alternatingly optimizing this new objective function (Classic-C-A )leads to similar results as the baseline Classic-C (Table 5).We also compare the energy of these solutions using the new objective and find the alternat-ing optimization produces the lowest energy solutions,as shown in Table 6.To do so,we set both the flow field u ,v and the auxiliary flow field ˆu ,ˆv to be the same in Eq.(2).In summary,we show that the heuristic median filter-ing step in Classic-C can now be viewed as energy min-imization of a new objective with a non-local term.The explicit formulation emphasizes the value of robustly inte-grating information over large neighborhoods and enables the improved model described below.6.Improved ModelBy formalizing the median filtering heuristic as an ex-plicit objective function,we can find ways to improve it.While median filtering in a large neighborhood has advan-tages as we have seen,it also has problems.A neighborhood centered on a corner or thin structure is dominated by the surround and computing the median results in oversmooth-ing as illustrated in Figure 3(a).Examining the non-local term suggests a solution.For a given pixel,if we know which other pixels in the area be-long to the same surface,we can weight them more highly.The modification to the objective function is achieved by introducing a weight into the non-local term [14,15]:∑i,j ∑(i ,j )∈N i,jw i,j,i ,j (|ˆu i,j −ˆu i ,j |+|ˆv i,j −ˆv i ,j |),(8)where w i,j,i ,j represents how likely pixel i ,j is to belongto the same surface as i,j .。

自适应光学视觉科学手册说明书

自适应光学视觉科学手册说明书

Adaptive Optics for Vision Science: Principles, Practices, Designand ApplicationsJason Porter, Abdul Awwal, Julianna LinHope Queener, Karen Thorn(Editorial Committee)Updated on June 30, 2003−Introduction1.Introduction (David Williams)University of Rochester1.1 Goals of the AO Manual (This could also be a separate preface written by the editors)* practical guide for investigators who wish to build an AO system* summary of vision science results obtained to date with AO1.2 Brief History of Imaging1.2.1 The evolution of astronomical AOThe first microscopes and telescopes, Horace Babcock , military applications during StarWars, ending with examples of the best AO images obtained to date. Requirements forastronomical AO1.2.2 The evolution of vision science AOVision correction before adaptive optics:first spectacles, first correction of astigmatism, first contact lenses, Scheiner and thefirst wavefront sensor.Retinal imaging before adaptive optics:the invention of the ophthalmoscope, SLO, OCTFirst AO systems: Dreher et al.; Liang, Williams, and Miller.Comparison of Vision AO and Astronomical AO: light budget, temporal resolutionVision correction with AO:customized contact lenses, IOLs, and refractive surgery, LLNL AO Phoropter Retinal Imaging with Adaptive OpticsHighlighted results from Rochester, Houston, Indiana, UCD etc.1.3 Future Potential of AO in Vision Science1.3.1 Post-processing and AO1.3.2 AO and other imaging technologies (e.g. OCT)1.3.3 Vision Correction1.3.4 Retinal Imaging1.3.5 Retinal SurgeryII. Wavefront Sensing2. Aberration Structure of the Human Eye (Pablo Artal)(Murcia Optics Lab; LOUM)2.1 Aberration structure of the human eye2.1.1 Monochromatic aberrations in normal eyes2.1.2 Chromatic aberrations2.1.3 Location of aberrations2.1.4 Dynamics (temporal properties) of aberrations2.1.5 Statistics of aberrations in normal populations (A Fried parameter?)2.1.6 Off-axis aberrations2.1.7 Effects of polarization and scattering3. Wavefront Sensing and Diagnostic Uses (Geunyoung Yoon) University of Rochester3.1 Introduction3.1.1 Why is wavefront sensing technique important for vision science?3.1.2 Importance of measuring higher order aberrations of the eyeCharacterization of optical quality of the eyePrediction of retinal image quality formed by the eye’s opticsBrief summary of potential applications of wavefront sensing technique3.1.3 Chapter overview3.2 Wavefront sensors for the eye3.2.1 History of ophthalmic wavefront sensing techniques3.2.2 Different types of wavefront sensors and principle of each wavefrontsensorSubjective vs objective method (SRR vs S-H, LRT and Tcherning)Measuring light going into vs coming out of the eye (SRR, LRT and Tcherning vs S-H) 3.3 Optimizing Shack-Hartmann wavefront sensor3.3.1 Design parametersWavelength, light source, laser beacon generation, pupil camera, laser safety…3.3.2 OSA standard (coordinates system, sign convention, order of Zernikepolynomials)3.3.3 Number of sampling points (lenslets) vs wavefront reconstructionperformance3.3.4 Tradeoff between dynamic range and measurement sensitivityFocal length of a lenslet array and lenslet spacing3.3.5 PrecompensationTrial lenses, trombone system, bite bar (Badal optometer)3.3.6 Increasing dynamic range without losing measurement sensitivityTranslational plate with subaperturesComputer algorithms (variable centroiding box position)3.3.7 Requirement of dynamic range of S-H wavefront sensor based on a largepopulation of the eye’s aberrations3.4 Calibration of the wavefront sensor3.4.1 reconstruction algorithm - use of simulated spot array pattern3.4.2 measurement performance - use of phase plate or deformable mirror 3.5 Applications of wavefront sensing technique to vision science3.5.1 Laser refractive surgery (conventional and customized ablation)3.5.2 Vision correction using customized optics (contact lenses andintraocular lenses)3.5.3 Autorefraction (image metric to predict subjective vision perception)3.5.4 Objective vision monitoring3.5.5 Adaptive optics (vision testing, high resolution retinal imaging)3.6 SummaryIII. Wavefront Correction with Adaptive Optics 4. Mirror Selection (Nathan Doble and Don Miller)University of Rochester / Indiana University4.1 Introduction4.1.1 Describe the DMs used in current systems.4.1.1.2 Xinetics type – Williams, Miller, Roorda – (PZT and PMN)4.1.1.3 Membrane – Artal, Zhu(Bartsch)4.1.1.4 MEMS – LLNL Phoropter, Doble4.1.1.5 LC-SLM – Davis System.4.2 Statistics of the two populations4.2.1 State of refraction:4.2.1.1 All aberrations present4.2.1.2 Zeroed Defocus4.2.1.3 Same as for 4.2.1.2 but with astigmatism zeroed in addition4.2.2 For various pupil sizes (7.5 - 2 mm) calculate:4.2.2.1 PV Error4.2.2.2 MTF4.2.2.3 Power Spectra4.2.3 Required DM stroke given by 95% of the PV error for the variousrefraction cases and pupil sizes.4.2.4 Plot of the variance with mode order and / or Zernike mode.4.3 Simulation of various Mirror TypesDetermine parameters for all mirrors to achieve 80% Strehl.4.3.1 Continuous Faceplate DMs4.3.1.1 Describe mode of operation.4.3.1.2 Modeled as a simple Gaussian4.3.1.3 Simulations for 7.5mm pupil4.3.1.4 Parameters to vary:Number of actuators.Coupling coefficient.Wavelength.4.3.1.5 All the above with unlimited stroke.4.3.2 Piston Only DMs4.3.2.1 Describe mode of operation.4.3.2.2 Simulations for 7.5mm pupil with either cases4.3.2.3 No phase wrapping i.e. unlimited stroke.Number of actuators.Packing geometryWavelength.Need to repeat the above but with gaps.4.3.2.4 Effect of phase wrappingTwo cases:Phase wrapping occurs at the segment locations.Arbitrary phase wrap.4.3.3 Segmented Piston / tip / tilt DMs4.3.3.1 Describe mode of operation.4.3.3.2 Three influence functions per segment, do the SVD fit on a segment by segmentbasis.4.3.3.3 Simulations for 7.5mm pupil.4.3.3.4 No phase wrapping unlimited stroke and tip/tilt.Number of actuators - squareSame as above except with hexagonal packing.Wavelength.Gaps for both square and hexagonal packing.4.3.3.5 Effect of phase wrappingPhase wrapping occurs at the segment locations.Arbitary phase wrap. Wrap the wavefront and then determine the required number ofsegments. Everything else as listed in part 1).4.3.4 Membrane DMs4.3.4.1 Describe mode of operation. Bimorphs as well.4.3.4.2 Simulations for 7.5mm pupil with either cases.4.3.4.3 Parameters to vary:Number of actuators.Actuator size.Membrane stressWavelength.5. Control Algorithms (Li Chen)University of Rochester5.1 Configuration of lenslets and actuators5.2 Influence function measurement5.3 Control command of wavefront corrector5.3.1 Wavefront control5.3.2 Direct slope control5.3.3 Special control for different wavefront correctors5.4 Transfer function modelization of adaptive optics system5.4.1 Transfer function of adaptive optics components5.4.2 Overall system transfer function5.4.3 Adaptive optics system bandwidth analysis5.5 Temporal modelization with Transfer function5.5.1 Feedback control5.5.2 Proportional integral control5.5.3 Smith compensate control5.6 Temporal controller optimization5.6.1 Open-loop control5.6.2 Closed-loop control5.6.2 Time delay effect on the adaptive optics system5.6.3 Real time considerations5.7 Summary6. Software/User Interface/Operational Requirements (Ben Singer) University of Rochester6.1 Introduction6.2 Hardware setup6.2.1 Imaging6.2.1.1 Hartmann-Shack Spots6.2.1.2 Pupil Monitoring6.2.1.3 Retinal Imaging6.2.2 Triggered devices: Shutters, lasers, LEDs6.2.3 Serial devices: Defocusing slide, custom devices6.2.4 AO Mirror control6.3 Image processing setup6.3.1 Setting regions of interest: search boxes6.3.2 Preparing the image6.3.2.1 Thresholding6.3.2.2 Averaging6.3.2.3 Background subtraction6.3.2.4 Flat-fielding6.3.3 Centroiding6.3.4 Bad data6.4 Wavefront reconstruction and visualization6.4.1 Zernike mode recovery and RMS6.4.1.1 Display of modes and RMS: traces, histograms6.4.1.2 Setting modes of interest6.4.2 Wavefront visualization6.4.2.1 Continuous grayscale image6.4.2.2 Wrapped grayscale image6.4.2.3 Three-D plots6.5 Adaptive optics6.5.1 Visualizing and protecting write-only mirrors6.5.2 Testing, diagnosing, calibrating6.5.3 Individual actuator control6.5.4 Update timing6.5.5 Bad actuators6.6 Lessons learned, future goals6.6.1 Case studies from existing systems at CVS and B&L6.6.1.1 One-shot wavefront sensing vs realtime AO6.6.1.2 Using AO systems in experiments: Step Defocus6.6.2 Engineering trade-offs6.6.2.1 Transparency vs Simplicity6.6.2.2 Extensibility vs Stability6.6.3 How to please everyone6.6.3.1 Subject6.6.3.2 Operator6.6.3.3 Experimenter6.6.3.4 Programmer6.6.4 Software tools6.7 Summary7. AO Assembly, Integration and Troubleshooting (Brian Bauman) Lawrence Livermore7.1 Introduction and Philosophy7.2 Optical alignment7.2.1 General remarks7.2.2 Understanding the penalties for misalignments7.2.3 Having the right knobs: optomechanics7.2.4 Common alignment practices7.2.4.1 Tools7.2.4.2 Off-line alignment of sub-systems7.2.4.3 Aligning optical components7.2.4.4 Sample procedures (taken from the AO phoropter project)7.3 Wavefront sensor checkout7.3.1 Wavefront sensor camera checkout7.3.2 Wavefront sensor checkout7.3.2.1 Proving that centroid measurements are repeatable.7.3.2.2 Proving that the centroid measurements do not depend on where centroids are withrespect to pixels7.3.2.3 Measuring plate scale.7.3.2.4 Proving that a known change in the wavefront produces the correct change incentroids.7.4 Wavefront Reconstruction7.4.1 Testing the reconstruction code: Prove that a known change in thewavefront produces the correct change in reconstructed wavefront.7.5 Aligning the “probe” beam into the eye7.6 Visual stimulus alignment7.7 Flood-illumination alignment7.8 DM-to-WFS Registration7.8.1 Tolerances & penalties for misregistration7.8.2 Proving that the wavefront sensor-to-SLM registration is acceptable.7.9 Generating control matrices7.9.1 System (“push”) matrix7.9.2 Obtaining the control matrix7.9.3 Checking the control matrix7.9.4 Null spaces7.10 Closing the loop7.10.1 Checking the gain parameter7.10.2 Checking the integration parameter7.11 Calibration7.11.1 Obtaining calibrated reference centroids.7.11.2 Proving that reference centroids are good7.11.3 Image-sharpening to improve Strehl performance.7.12 Science procedures7.13 Trouble-shooting algorithms8. System Performance: Testing, Procedures, Calibration and Diagnostics (Bruce Macintosh, Marcos Van Dam)Lawrence Livermore / Keck Telescope8.1 Spatial and Temporal characteristics of correction8.2 Power Spectra calculations8.3 Disturbance rejection curves8.4 Strehl ratio/PSF measurements/calculations8.5 Performance vs. different parameters (beacon brightness, field angle, …)?8.6 Summary Table and Figures of above criteria8.6.1 Results from Xinetics, BMC, IrisAOIV. Retinal Imaging Applications 9. Fundamental Properties of the Retina (Ann Elsner) Schepens Eye Research Institute9.1 Shape of the retina, geometric optics9.1.1 Normal fovea, young vs. old9.1.1.1. foveal pit9.1.1.2. foveal crest9.1.2 Normal optic nerve head9.1.3 Periphery and ora serrata9.2 Two blood supplies, young vs. old9.2.1 Retinal vessels and arcades9.2.2 0 – 4 layers retinal capillaries, foveal avascular zone9.2.3 Choriocapillaris, choroidal vessels, watershed zone 9.3 Layers vs. features, young vs. old, ethnic differences9.3.1 Schlera9.3.2 Choroidal vessels, choroidal melanin9.3.3 Bruch’s membrane9.3.4 RPE, tight junctions, RPE melanin9.3.5 Photoreceptors, outer limiting membrane9.3.5.1 Outer segment9.3.5.2 Inner segment9.3.5.3 Stiles-Crawford effect9.3.5.4 Macular pigment9.3.6 Neural retina9.3.7 Glia, inner limiting membrane, matrix9.3.8 Inner limiting membrane9.3.9 Vitreo-retinal interface, vitreous floaters9.4 Spectra, layers and features9.4.1 Main absorbers in the retina9.4.2 Absorbers vs. layers9.4.3 Features in different wavelengths9.4.4 Changes with aging9.5 Light scattering, layers and features9.5.1 Directly backscattered light9.5.2 Multiply scattered light9.5.3 Geometric changes in specular light return9.5.4 Layers for specular and multiply scattered light9.5.5 Imaging techniques to benefit from light scattering properties 9.6 Polarization9.6.1 Polarization properties of the photoreceptors9.6.2 Polarization properties of the nerve fiber bundles, microtubules9.6.3 Anterior segment and other polarization artifacts9.6.4 Techniques to measure polarization properties9.7 Imaging techniques to produce contrast from specular or multiply scattered light9.7.1 Confocal imaging9.7.2 Polarization to narrow the point spread function9.7.3 Polarization as a means to separate directly backscattered light frommultiply scattered light, demonstration using the scattered light9.7.4 Coherence techniques as a means to separate directly backscattered light from multiply scattered light, with a goal of using the scattered light10. Strategies for High Resolution Retinal Imaging (Austin Roorda, Remy Tumbar, Julian Christou)University of Houston / University of Rochester / University of California, Santa Cruz10.1 Conventional Imaging (Roorda)10.1.1 Basic principlesThis will be a simple optical imaging system10.1.2 Basic system designShow a typical AO flood-illuminated imaging system for the eye10.1.3 Choice of optical componentsDiscuss the type of optical you would use (eg off axis parabolas)10.1.4 Choice of light sourceHow much energy, what bandwidth, flash duration, show typical examples10.1.5 Controlling the field sizeWhere to place a field stop and why10.1.6 Choice of cameraWhat grade of camera is required? Show properties of typical cameras that are currently used10.1.7 Implementation of wavefront sensingWhere do you place the wavefront sensor. Using different wavelengths for wfs.10.2 Scanning Laser Imaging (Roorda)10.2.1 Basic principlesThis will show how a simple scanning imaging system operates10.2.2 Basic system designThis shows the layout of a simple AOSLO10.2.3 Choice of optical componentsWhat type of optical components shoud you use and why (eg mirrors vs lenses). Where doyou want to place the components (eg raster scanning, DM etc) and why.10.2.4 Choice of light sourceHow to implement different wavelengths. How to control retinal light exposure10.2.5 Controlling the field sizeOptical methods to increase field sizeMechanical (scanning mirror) methods to increase field size10.2.6 Controlling light deliveryAcousto-optical control of the light source for various applications10.2.7 Choice of detectorPMT vs APD what are the design considerations10.2.8 Choice of frame grabbing and image acquisition hardwareWhat are the requirements for a frame grabber. What problems can you expect.10.2.9 Implementation of wavefront sensingStrategies for wavefront sensing in an AOSLO10.2.10 Other: pupil tracking, retinal tracking, image warping10.3 OCT systems (Tumbar)10.3.1 Flood illuminated vs. Scanning10.4 Future ideas (Tumbar)10.4.1 DIC (Differential Interference Contrast)10.4.2 Phase Contrast10.4.3 Polarization Techniques10.4.4 Two-photon10.4.5 Fluorescence/Auto-fluorescence10.5 Survey of post-processing/image enhancement strategies (Christou)11. Design Examples11.1 Design of Houston Adaptive Optics Scanning Laser Ophthalmoscope (AOSLO) (Krishna Venkateswaran)11.1.1 Basic optical designEffect of double pass system on psf, imaging in conjugate planes11.1.2 Light delivery opticsFiber optic source and other optics11.1.3 Raster scanningScanning speeds etc.,11.1.4 Physics of confocal imaging11.1.5 Adaptive optics in SLOWavefront sensing, Zernike polynomials, Deformable mirror, correction time scales11.1.6 Detailed optical layout of the AOSLOLens, mirrors, beam splitters with specs11.1.7 Image acquisitionBack end electronics, frame grabber details11.1.8 Software interface for the AOSLOWavefront sensing, Image acquisition11.1.9 Theoretical model of AOSLO:Limits on axial and lateral resolution11.1.10 Image registration11.1.11 Results11.1.12 Discussions on improving performance of AOSLOLight loss in optics, Deformable mirror, Wavefront sensing,11.1.13 Next generation AOSLO type systems11.2 Indiana University AO Coherence Gated System (Don Miller)11.2.1 Resolution advantages of an AO-OCT retina camera11.2.2 AO-OCT basic system design concepts11.2.2.1 Application-specific constraints−Sensitivity to weak tissue reflections−Tolerance to eye motion artifacts−Yoking focal plane to the coherence gate11.2.2.2 Integration of AO and OCT sub-systems−Generic OCT system−Specific OCT architectures−Preferred AO-OCT embodiments11.2.3 Description of the Indiana AO-OCT retina cameraOptical layout of the Indiana AO-OCT retina camera11.2.3.1 Adaptive Optics for correction of ocular aberrationsA. System descriptionB. Results11.2.3.2 1D OCT axial scanning for retina trackingA. System descriptionB. Results11.2.3.3 High speed 2D incoherent flood illumination for focusing and aligningA. System descriptionB. Results11.2.3.4 CCD-based 2D OCT for en face optical sectioning the retinaA. System descriptionB. Results11.2.4 Future developments11.2.4.1 Smart photodiode array11.2.4.2 En face and tomographic scanning11.2.4.3 Reduction of image speckle11.2.4.4 Detector sensitivity11.2.4.5 Faster image acquisition11.3 Rochester Second Generation AO System (Heidi Hofer)V. Vision Correction Applications12. Customized Vision Correction Devices (Ian Cox)Bausch & Lomb12.1 Contact Lenses12.1.1 Rigid or Soft Lenses?12.1.2 Design Considerations – More Than Just Optics12.1.3 Measurement – The Eye, the Lens or the System?12.1.4 Manufacturing Issues – Can The Correct Surfaces Be Made?12.1.5 Who Will Benefit?12.1.6 Summary12.2 Intraocular Lenses12.2.1 Which Aberrations - The Cornea, The Lens or The Eye?12.2.2 Surgical Procedures – Induced Aberrations12.2.3 Design & Manufacturing Considerations12.2.4 Future Developments & Summary13. Customized Refractive Surgery (Scott MacRae)University of Rochester / StrongVision14. Visual Psychophysics (UC Davis Team, headed by Jack Werner) UC Davis14.1 Characterizing visual performance14.1.1 Acuity14.1.2 Contrast sensitivity functions (CSFs)14.1.3 Photopic/scotopic performance (include various ways to defineluminance)14.2 What is psychophysics?14.2.1 Studying the limits of vision14.2.2 Differences between detection, discrimination and identification14.3 Psychophysical methods14.3.1 Psychometric function14.3.2 signal detection theory14.3.3 measuring threshold14.3.4 Criterion-free methods14.3.5 Method of constant stimuli, method of adjustment, adaptive methods(e.g. Quest).14.4 The visual stimulus14.4.1 Issues in selecting a display systemTemporal resolutionSpatial resolutionIntensity (maximum, bit depth)HomogeneitySpectral characteristics14.4.2 Hardware optionsCustom optical systems (LEDs, Maxwellian view)DisplaysCRTsDLPsLCDsPlasmaProjectorsDisplay generationcustom cardsVSGBits++10-bit cardsPelli attenuatorDithering/bit stealing14.4.3 SoftwareOff the shelf software is not usually flexible enough. We recommend doing it yourself. This canbe done using entirely custom software (e.g. C++) or by using software libraries such as VSG(PC) or PsychToolbox (Mac/PC).14.4.4 CalibrationGamma correctionSpatial homogeneityTemporal and spatial resolution14.5 Summary15. Wavefront to Phoropter Refraction (Larry Thibos)Indiana University15.1 Basic terminology15.1.1 Refractive error15.1.2 Refractive correction15.1.3 Lens prescriptions15.2 The goal of subjective refraction15.2.1 Definition of far point15.2.2 Elimination of astigmatism15.2.3 Using depth-of-focus to expand the range of clear vision15.2.4 Placement of far-point at hyperfocal distance15.3 Methods for estimating the monochromatic far-point from an aberration map15.3.1 Estimating center of curvature of an aberrated wavefront15.3.1.1 Least-squares fitting15.3.1.2 Paraxial curvature matching15.3.2 Estimating object distance that optimizes focus15.3.2.1 Metrics based on point objects15.3.2.2 Metrics based on grating objects15.4 Ocular chromatic aberration and the polychromatic far-point15.4.1 Polychromatic center of curvature metrics15.4.2 Polychromatic point image metrics15.4.3 Polychromatic grating image metrics15.5 Experimental evaluation of proposed methods15.5.1 Conditions for subjective refraction15.5.2. Monochromatic predictions15.5.3 Polychromatic predictions16. Design ExamplesDetailed Layouts, Numbers, Noise Analysis, Limitations for Visual Psychophysics: 16.1 LLNL/UR/B&L AO Phoroptor (Scot Olivier)16.2 UC Davis AO Phoropter (Scot Olivier)16.3 Rochester 2nd Generation AO System (Heidi Hofer)V. Appendix/Glossary of Terms (Hope Queener, JosephCarroll)• Laser safety calculations• Other ideas?• Glossary to define frequently used terms。

理论计算研究二维二维BPg-C3N4 异质结的光催化CO2 还原性能

理论计算研究二维二维BPg-C3N4 异质结的光催化CO2 还原性能

物 理 化 学 学 报Acta Phys. -Chim. Sin. 2021, 37 (6), 2010027 (1 of 9)Received: October 13, 2020; Revised: November 4, 2020; Accepted: November 4, 2020; Published online: November 12, 2020.*Corresponding authors. Emails: Jftanhaiyan@ (H.T.); zhubicheng1991@ (B.Z.); zly2017@ (L.Z.). Tel.: +86-151******** (H.T.); +86-132******** (B.Z.); +86-157******** (L.Z.).This work was supported by the National Key Research and Development Program of China (2018YFB1502001), the National Natural Science Foundation of China (51872220, 21905219, 51932007, U1905215, 21871217, U1705251), National Postdoctoral Program for Innovative Talents (BX20180231), China Postdoctoral Science Foundation (2020M672432), Hubei Postdoctoral Program for Innovative Research Post.国家重点研发计划(2018YFB1502001), 国家自然科学基金(51872220, 21905219, 51932007, U1905215, 21871217, U1705251), 博士后创新人才支持计划(BX20180231), 中国博士后科学基金(2020M672432)和湖北省博士后创新研究岗位项目资助 © Editorial office of Acta Physico-Chimica Sinica[Article] doi: 10.3866/PKU.WHXB202010027 2D/2D Black Phosphorus/g-C 3N 4 S-Scheme HeterojunctionPhotocatalysts for CO 2 Reduction Investigated using DFT Calculations Xingang Fei 1, Haiyan Tan 2,*, Bei Cheng 1, Bicheng Zhu 1,*, Liuyang Zhang 1,*1 State Key Laboratory of Advanced Technology for Materials Synthesis and Processing, Wuhan University of Technology, Wuhan 430070, China.2 School of Chemistry and Environmental Engineering, Hubei University for Nationalities, Enshi 445000, Hubei Province, China. Abstract: Photocatalytic reduction of CO 2 to hydrocarbon compounds is apromising method for addressing energy shortages and environmental pollution.Considerable efforts have been devoted to exploring valid strategies to enhancephotocatalytic efficiency. Among various modification methods, the hybridization ofdifferent photocatalysts is effective for addressing the shortcomings of a singlephotocatalyst and enhancing its CO 2 reduction performance. In addition, metal-freematerials such as g-C 3N 4 and black phosphorus (BP) are attractive because of theirunique structures and electronic properties. Many experimental results have verifiedthe superior photocatalytic activity of a BP/g-C 3N 4 composite. However, theoretical understanding of the intrinsic mechanism of the activity enhancement is still lacking. Herein, the geometric structures, optical absorption, electronic properties, and CO 2 reduction reaction processes of 2D/2D BP/g-C 3N 4 composite models are investigated using density functional theory calculations. The composite model consists of a monolayer of BP and a tri-s -triazine-based monolayer of g-C 3N 4. Based on the calculated work function, it is inferred that electrons transfer from g-C 3N 4 to BP owing to the higher Fermi level of g-C 3N 4 compared with that of BP . Furthermore, the charge density difference suggests the formation of a built-in electric field at the interface, which is conducive to the separation of photogenerated electron-hole pairs. The optical absorption coefficient demonstrates that the light absorption of the composite is significantly higher than that of its single-component counterpart. Integrated analysis of the band edge potential and interfacial electronic interaction indicates that the migration of photogenerated charge carriers in the BP/g-C 3N 4 hybrid follows the S-scheme photocatalytic mechanism. Under visible-light irradiation, the photogenerated electrons on BP recombine with the photogenerated holes on g-C 3N 4, leaving photogenerated electrons and holes in the conduction band of g-C 3N 4 and the valence band of BP , respectively. Compared with pristine g-C 3N 4, this S-scheme heterojunction allows efficient separation of photogenerated charge carriers while effectively preserving strong redox abilities. Additionally, the possible reaction path for CO 2 reduction on g-C 3N 4 and BP/g-C 3N 4 is discussed by computing the free energy of each step. It was found that CO 2 reduction on the composite occurs most readily on the g-C 3N 4 side. The reaction path on the composite is different from that on g-C 3N 4. The heterojunction reduces the maximum energy barrier for CO 2 reduction from 1.48 to 1.22 eV, following the optimal reaction path. Consequently, the BP/g-C 3N 4 heterojunction is theoretically proven to be an excellent CO 2 reduction photocatalyst. This work is helpful for understanding the effect of BP modification on the photocatalytic activity of g-C 3N 4. It also provides a theoretical basis for the design of other high-performance CO 2 reduction photocatalysts.Key Words: Photocatalysis; CO 2 reduction; Step-scheme heterojunction; Graphitic carbon nitride;Density functional theory. All Rights Reserved.理论计算研究二维/二维BP/g-C3N4异质结的光催化CO2还原性能费新刚1,谭海燕2,*,程蓓1,朱必成1,*,张留洋1,*1武汉理工大学,材料复合新技术国家重点实验室,武汉 4300702湖北民族大学,化学与环境工程学院,湖北恩施 445000摘要:光催化二氧化碳还原成烃类化合物是解决能源短缺和环境污染的重要途径。

BionicMotionRobot 生物模仿机器人说明书

BionicMotionRobot 生物模仿机器人说明书

BionicMotionRobot Pneumatic lightweight robot with natural movement patternsCell Coexistence Synchronised CooperationCollaborationBionicMotionRobot New approaches for human-robot collaborationSensitive and gentle or powerful and dynamic – in terms of its movements and functionality, the BionicMotionRobot is inspired by an elephant’s trunk and an octopus’s tentacles. The pneumatic lightweight robot features 12 degrees of freedom and, with its flexible bellows structure, can effortlessly implement the fluent motion sequences of its natural role models.Impressive power to weight ratioThe bionic robot arm has a load capacity of around three kilograms and weighs approximately the same itself. Depending on which gripper is fitted, it can handle a number of different objects and be used for a wide range of tasks.The concept of the flexible kinematics is based on the Bionic Handling Assistant from 2010, which, due to the safe collaboration between man and machine, was given the German Future Award. Since then, Festo has been looking intensively into systems that could relieve people of monotonous activities and at the same time pose no risk – an aspect that is becoming increasingly im-portant in everyday factory life.Whether it is shorter lead times, faster product life cycles or high flexibility with regard to quantities and variety, the requirements of the production of the future are manifold and are changing faster than ever before. This industrial change requires a new way for humans, machines and data to interact.Besides the digital networking of entire facilities, above allrobot-based automation solutions, which work hand in hand with people, play a critical role in this development. In the production of tomorrow, direct interaction between man and machine will be part of the daily routine.Collaborative working spaces of the futureThe strict separation between the manual work of the factory worker and the automated actions of the robot is being increasingly set aside. Their work ranges are overlapping and merging into a collaborative working space. In this way, human and machine will be able to work together on the same workpiece or component simultaneously in future – without having to be shielded from each other for safety reasons.As a worldwide supplier of automation technology, it is Festo’s core business to help shape the production and working worlds of the future. A key element for coming up with ideas is the Bionic Learning Network. In an alliance with external partners, Festo looks for natural phenomena and operating principles that can be transferred to technology.Paradigm shift in roboticsAt the focus of the current research work are lightweight bionic robots, which due to their natural movement patterns and the pneu-matics employed are almost predestined for collaborative working spaces and in future will be able to represent a cost-effective alter-native to classic robot concepts.The strengths of pneumatic drives have always lain in their simple handling and robustness, the low costs of acquisition and their high power density – in other words, comparatively large forces in a small space and with a low weight. Holding processes get by without further compressed air consumption and are therefore extremely energy efficient.For direct contact between human and machine, pneumatics offer another critical advantage, however: their system’s inherent flexi-bility. If an actuator is filled with compressed air, the motion gen-erated can be exactly set in terms of speed, force and rigidity. In the event of a collision, the system eases off, thus posing no risk to the worker.To be able to adjust the whole system to any settings in its dynam-ics, the valve technology used must be able to control the air flows and pressures with extreme precision and at the same time ensure the complex interconnections of many channels.Digitisation of pneumaticsWhat could until now only be implemented with a great deal of effort is made easily possible by a world first from Festo: the Festo Motion Terminal is the first pneumatic automation platform, which, using its software control system, combines the function-alities of over 50 components using apps. Digitisation is opening up completely new areas of application for pneumatics, which until now has been the reserve of electrical automation.01: Collaborative working space: Simul-taneous, common processing of a work-piece by human and robot 02: Safe handling: The combination of the BionicMotionRobot with the highly elastic TentacleGripper 03: Conceivable scenario: In action with a vacuum suction cup for flat and smooth objects 04: Tremendous power potential: The outstanding ratio of inherent weight and payload© Fraunhofer IAO, study of lightweight robots in manual assemblyBionicMotionRobot Pneumatic lightweight robot with natural movement patternsMode of operation and potential usesFor a safe and more ergonomic future working worldThe freely moving arm on the BionicMotionRobot is covered with an outer textile skin and consists of three flexible basic segments which can be put together in a modular fashion. 3D textile knitted fabric represents new fibre technology In each of the three segments, four bellows are fitted which are held together by disk-shaped ribs with a gap of about two centi-metres. A cardan joint runs between them, housing the pneumatic actuators and making sure the ribs do not twist. The 12 bellows are made of sturdy elastomer. Each one of them is surrounded by a special 3D textile cover which is knitted from both elastic and high-strength yarns.For this unique 3D textile knitted fabric, the developers took a closer look at the muscular structure of the octopus: the muscle fibres in the tentacles are aligned differently in several layers. This interaction of radially, diagonally and longitudinally oriented fibres allows the creature to move its tentacles in a targeted manner. Based on this model, the yarns in the 3D textile knitted fabric run around the bellows structures in a special pattern.If a set of bellows is supplied with compressed air, it can extend lengthways and thereby deflect the joint structure. In the radial dir-ection, the expansion of the elastomer is limited by the fixed threads in the fabric. This means that the textile can be used to exactly deter-mine at which points the structure expands, thereby generating power, and where it is prevented from expanding. This allows very large forces to be generated and turned into movement.Guidance and control with the Festo Motion Terminal The complex guidance and control of the 12-bellow kinematics is assumed by a Festo Motion Terminal. It combines high-precision mechanics, sensor technology as well as control and measuring technology in the tightest space. With the internal control algorithms of the motion apps and the installed piezo valves, flow rates and pressures can be exactly dosed and also varied to any setting in several channels simultaneously.That enables the BionicMotionRobot to perform motion sequences that are both powerful and fast as well as soft and precise – whilst the rigidity of the kinematics is freely adjustable.Due to its modular structure and this precise control of the flexible bellows structures, the robot arm can bend in three different direc-tions simultaneously and implement the fluent movements of its natural role models.Optical shape sensor for exact routingA shared shape sensor is fitted in the cardan joints on the three segments and runs like a cable along the system’s whole longitu-dinal axis. This allows it to record the position, shape and inter-actions of the whole kinematics and illustrate them virtually. The simulated model of the sensor cable follows the real sensor in real time and thus enables positioning and routing accurate to around ten millimetres.Many potential uses and application fieldsThe BionicMotionRobot could be used anywhere that compact, powerful and efficient systems are required. Its pneumatic con-struction is insensitive to dust and dirt, which also makes an application in polluted and contaminated or unhealthy surround-ings conceivable.Supporting assistance system for assemblyThe BionicMotionRobot is virtually predestined to be a helping third hand in the assembly sector. The pneumatic structures can provide relief by holding objects without heating up or consuming additional energy.A scenario in which the robot arm picks up various workpieces on its own, passes them to a person for processing and then puts them down in another place is imaginable. The worker can thus go about their work in a more ergonomic, precise, concentrated and hence more efficient manner.High user acceptance and safe handlingThe natural movements of the bionic robot arm create a sense of familiarity for the user, which increases acceptance for direct collaboration. In the event of a collision, the pneumatic kinematics automatically ease off and do not pose any danger to humans. This inherent flexibility of the system and the low tare weight allow it to be used without a protective cage, thus making an immediate and safe collaboration between human and machine possible.01: A natural role model: The counter-acting muscles in an octopus’s tentacle02: A new fibre technology: The special 3D textile knitted fabric surrounding the flexible bellows structures03: Modular structure: A look inside the pneumatic robot arm04: Virtual image: The shape sensor en-ables a simulated model of the entire kinematicsTechnical dataTotal length: ...................................................................... 850 mm Diameter : ............................................................ 130 mm/100 mm Degrees of freedom : ................................................................... 12Robot arm weight: .............................................................. 2,950 g Moved weight: ................................................................... 2,950 g Working pressure: .................................................................. 3 bar Repetition accuracy: ........................................................... ±10 mm Distance between the ribs: .................................................. 19 mm Centre distance of the ribs: ................................................. 21 mm Steering and control: Festo Motion TerminalSensor technology : 3D-effective optical shape sensor Actuator technology: Bellows produced using immersion method made of natural rubber with high-strength 3D textile knitted fabric Ribs: Gimbally connected ribs made ofcarbon-fibre-reinforced polymerPicture credits Page 2: Fraunhofer IAO, StuttgartPage 6, top left: Amir Andikfar, Jonas Lauströer, HamburgProf. Dr Martin S. Fischer, Jena Page 6, centre:deutschle cgi, Nürtingen Project participants Project initiator:Dr Wilfried Stoll, managing partner Festo Holding GmbHIdea, concept, implementation:Prof. Dieter Mankau, Frankfurt am MainProject coordination:Markus Fischer, Bissingen a. d. TeckControl technology:Prof. Dr Ivo Boblan, Beuth University of Applied Sciences, Berlin Mirco Martens, Alexander Pawluchin, Technical University of Berlin Dr Alexander Hildebrandt, Festo AG & Co. KGSensor technology:Dr Jens Teichert, Teichert Systemtechnik GmbH, LilienthalScientific consultancy, biology:Prof. Dr Martin S. Fischer, Friedrich-Schiller-University JenaConsulting:Dr Werner Fischer, MunichDesign, CAD and prototypes:Christian Ebert, Mirko Zobel, Ebert Zobel, Industrial Design,Frankfurt am MainTextile technology and pneumatics design:Walter Wörner, Gesellschaft für textilen Service mbH, Pfullingen Rex Gummitechnik GmbH & Co. KG, Pfungstadt Plastics engineering:Klaus Hilmer, Dennis Meyer, Festo Polymer GmbH, St. Ingbert Festo AG & Co. KG Ruiter Strasse 8273734 Esslingen GermanyPhone +49 711 347-0Fax+49 711 347-21 55cc @125 e n 3/2017。

透明导电薄膜英文综述AZO-ITO

透明导电薄膜英文综述AZO-ITO

Review of TCO Thin FilmsAbstractThe present review paper reports on the physical properties, status, prospects for further development, and applications of polycrystalline or amorphous, transparent, and conducting oxides (TCO) semiconductors. The coexistence of electrical conductivity and optical transparency in these materials depends on the nature, number, and atomic arrangements of metal cations in crystalline or amorphous oxide structures, on the resident morphology, and on the presence of intrinsic or intentionally introduced defects. The important TCO semiconductors are impurity-doped ZnO, In2O3, SnO2 and CdO, as well as the ternary compounds Zn2SnO4, ZnSnO3, Zn2In2O5, Zn3In2O6, In2SnO4, CdSnO3, and multi-component oxides consisting of combinations of ZnO, In2O3 and SnO2. Sn doped In2O3 (ITO) and F doped SnO2 TCO thin films are the preferable materials for most present applications. The expanding use of TCO materials, especially for the production of transparent electrodes for optoelectronic device applications, is endangered by the scarcity and high price of In. This situation drives the search for alternative TCO materials to replace ITO. The electrical resistivity of the novel TCO materials should be ~10-5 Ω.cm, typical absorption coefficient smaller than 104 cm-1 in the near UV and visible range, with optical band gap ~3 eV. At present, ZnO:Al and ZnO:Ga (AZO and GZO) semiconductors could become good alternatives to ITO for thin-film transparent electrode applications. The best candidates are AZO thin films, which have low resistivity of the order of 10−4Ω.cm, inexpensive source materials, and are non-toxic. However, development of large area deposition techniques are still needed to enable the production of AZO and GZO films on large area substrates with a high deposition rate. In addition to the required electrical and optical characteristics, applied TCO materials should be stable in hostile environment containing acidic and alkali solutions, oxidizing and reducing atmospheres, and elevated temperature. Most of the TCO materials are n-type semiconductors, but p-type TCO materials are researched and developed. Such TCO include: ZnO:Mg, ZnO:N, IZO, NiO, NiO:Li, CuAlO2, Cu2SrO2, and CuGaO2 thin films. At present, these materials have not yet found place in actual applications.I. IntroductionMost optically transparent and electrically conducting oxides (TCO) are binary or ternary compounds, containing one or two metallic elements. Their resistivity could be as low as 10-4 Ω.cm, and their extinction coefficient k in the optical visible range (VIS) could be lower than 0.0001, owing to their wide optical band gap (E g) that could be greater than 3 eV. This remarkable combination of conductivity and transparency is usually impossible in intrinsic stoichiometric oxides; however, it is achieved by producing them with a non-stoichiometric composition or by introducing appropriate dopants. Badeker (1907) discovered that thin CdO films possess such characteristics.1 Later, it was recognized that thin films of ZnO, SnO2, In2O3 and their alloys were also TCOs.2 Doping these oxides resulted in improved electrical conductivity without degrading their optical transmission. Al doped ZnO (AZO), tin doped In2O3, (ITO) and antimony or fluorine doped SnO2 (ATO and FTO), are among the most utilized TCO thin films in modern technology. In particular, ITO is used extensively.The actual and potential applications of TCO thin films include: (1) transparent electrodes for flat panel displays (2) transparent electrodes for photovoltaic cells, (3) low emissivity windows, (4) window defrosters, (5) transparent thin films transistors, (6) light emitting diodes, and (7) semiconductor lasers. As the usefulness of TCO thin films depends on both their optical and electrical properties, both parameters should be considered together with environmental stability, abrasion resistance, electron work function, and compatibility with substrate and other components of a given device, as appropriate for the application. The availability of the raw materials and the economics of the deposition method are also significant factors in choosing the most appropriate TCO material. The selection decision is generally made by maximizing the functioning of the TCO thin film by considering all relevant parameters, and minimizing the expenses. TCO material selection only based on maximizing the conductivity and the transparency can be faulty.Recently, the scarcity and high price of Indium needed for ITO, the most popular TCO, as spurred R&D aimed at finding a substitute. Its electrical resistivity (ρ) should be ~10-4 Ω.cm or less, with an absorption coefficient (α) smaller than 104 cm-1 in the near-UV and VIS range, and with an optical band gap >3eV. A 100 nm thick film TCO film with these values for α and ρ will have optical transmission (T ) 90% and a sheet resistance (R S) 10 Ω. At present, AZO and ZnO:Ga (GZO) semiconductors are promising alternatives to ITO for thin-film transparent electrode applications. The best candidates is AZO, which can have a low resistivity, e.g. on the order of 10−4Ω.cm,3 and its source materials are inexpensive and non-toxic. However, the development of large area, high rate deposition techniques is needed.Another objective of the recent effort to develop novel TCO materials is to deposit p-type TCO films. Most of the TCO materials are n-type semiconductors, but p-type TCO materials are required for the development of solid lasers. Such p-type TCOs include: ZnO:Mg, ZnO:N, ZnO:In, NiO, NiO:Li, CuAlO 2, Cu 2SrO 2, and CuGaO 2 thin films. These materials have not yet found a place in actual applications.Published reviews on TCOs reported exhaustively on the deposition and diagnostic techniques, on film characteristics, and expected applications.4,,56 The present paper has three objectives: (1) to review the theoretical and experimental efforts to explore novel TCO materials intended to improve the TCO performance, (2) to explain the intrinsic physical limitations that affect the development of an alternative TCO with properties equivalent to those of ITO, and (3) to review the practical and industrial applications of existing TCO thin films.II . Electrical conductivityTCOs are wide band gap (E g ) semiconducting oxides, with conductivity σ in the range 102 –1.2×106 (S). The conductivity is due to doping either by oxygen vacancies or by extrinsic dopants. In the absence of doping, these oxides become very good insulators, with ρ > 1010 Ω-cm. Most of the TCOs are n-type semiconductors. The electrical conductivity of n-type TCO thin films depends on the electron density in the conduction band and on their mobility: σ=μn e , where μ is the electron mobility, n is its density, and e is the electron charge. The mobility is given by:*e m τμ=where τ is the mean time between collisions, and m * is the effective electron mass. However, as n and τ are negatively correlated, the magnitude of μ is limited. Due to the large energy gap (E g > 3 eV) separating the valence band from the conducting band, the conduction band can not be thermally populated at room temperature (kT~0.03 eV, where k is Boltzmann’s constant), hence, stoichiometric crystalline TCOs are good insulators.7 To explain the TCO characteristics, various population mechanisms and several models describing the electron mobility were proposed. Some characteristics of the mobility and the processes by which the conduction band is populated with electrons were shown to be interconnected by electronic structure studies,8 e.g., that the mobility is proportional to the magnitude of the band gap.In the case of intrinsic materials, the density of conducting electrons has often been attributed to the presence of unintentionally introduced donor centers, usually identified as metallicinterstitials or oxygen vacancies that produced shallow donor or impurity states located close to the conduction band. The excess or donor electrons are thermally ionized at room temperature, and move into the host conduction band. However, experiments have been inconclusive as to which of the possible dopants was the predominant donor.9 Extrinsic dopants have an important role in populating the conduction band, and some of them have been unintentionally introduce. Thus, it has been conjectured in the case of ZnO that interstitial hydrogen, in the H+ donor state, could be responsible for the presence of carrier electrons.10In the case of SnO2, the important role of interstitial Sn in populating the conducting band, in addition to that of oxygen vacancies, was conclusively supported by first-principle calculations of Kiliç and Zunger.11 They showed that Sn interstitials and O vacancies, which dominated the defect structure of SnO2 due to the multivalence of Sn, explained the natural nonstoichiometry of this material and produced shallow donor levels, turning the material into an intrinsic n-type semiconductor. The electrons released by these defects were not compensated because acceptor-like intrinsic defects consisting of Sn voids and O interstitials did not form spontaneously. Furthermore, the released electrons did not make direct optical transitions in the visible range due to the large gap between the Fermi level and the energy level of the first unoccupied states. Thus, SnO2 could have a carrier density with minor effects on its transparency.The conductivity σ is intrinsically limited for two reasons. First, n and μ cannot be independently increased for practical TCOs with relatively high carrier concentrations. At high conducting electron density, carrier transport is limited primarily by ionized impurity scattering, i.e., the Coulomb interactions between electrons and the dopants. Higher doping concentration reduces carrier mobility to a degree that the conductivity is not increased, and it decreases the optical transmission at the near-infrared edge. With increasing dopant concentration, the resistivity reaches a lower limit, and does not decrease beyond it, whereas the optical window becomes narrower. Bellingham et al. were the first to report that the mobility and hence the resistivity of transparent conductive oxides (ITO, SnO2, ZnO) are limited by ionized impurity scattering for carrier concentrations above 1020 cm-3. Ellmer also showed that in ZnO films deposited by various methods, the resistivity and mobility were nearly independent of the deposition method and limited to about 2×10-4Ω.cm and 50 cm2/Vs, respectively.12,13 In ITO films, the maximum carrier concentration was about 1.5×1021 cm-3, and the same conductivity and mobility limits also held .14 This phenomenon is a universal property of other semiconductors.15,16 Scattering by the ionized dopant atoms that are homogeneously distributed in the semiconductor is only one of the possible effects that reduces the mobility. The all recently developed TCO materials, including doped and undopedbinary, ternary, and quaternary compounds, also suffer from the same limitations. Only some exceptional samples had a resistivity of ≤1×10-4Ω.cm.In addition to the above mentioned effects that limit the conductivity, high dopant concentration could lead to clustering of the dopant ions,17 which increases significantly the scattering rate, and it could also produce nonparabolicity of the conduction band, which has to be taken into account for degenerately doped semiconductors with filled conduction bands.18III. Optical PropertiesAs mentioned above, besides high conductivity (~106 S), effective TCO thin films should have a very low absorption coefficient in the near UV-VIS-NIR region. The transmission in the near UV is limited by E g, as photons with energy larger than E g are absorbed. A second transmission edge exists at the NIR region, mainly due to reflection at the plasma frequency. Ideally, a wide band gap TCO should not absorb photons in the transmission “window” in the UV-VIS-NIR region. However, there are no “ideal” TCOs thin films, and even if such films could be deposited, reflection and interference would also affect the transmission. Hence, 100% transparency over a wide region cannot be obtained.The optical properties of TCOs transmission T, reflection R, and absorption A, are determined by its refraction index n, extinction coefficient k, band gap E g, and geometry. Geometry includes film thickness, thickness uniformity, and film surface roughness. T, R and, A are intrinsic, depending on the chemical composition and solid structure of the material, whereas the geometry is extrinsic. There is a negative correlation between the carrier density and the position of the IR absorption edge, but positive correlation between the carrier density and the UV absorption edge, as E g increases at larger carrier density (Moss-Burstein effect). As a result, the TCO transmission boundaries and conductivity are interconnected.The width of the VIS transmission window of a TCO film with thickness deposited on a transparent substrate is affected not only by the optical parameters of the TCO film but also by the optical properties of the substrate. The refractive index n sub of the most common substrates are ~1.45 for fused silica and ~1.6 for various glasses. The extinction coefficient of the substrate (k sub) is generally < 10-7, hence any light absorption would take place in the film, where generally k film> k sub. For films thicker than 100 nm, several interference bands could be formed, producing maximal and minimal values of T when either the wavelength or thickness is varied. When k film≈ 0, the peak transmission (T max) is equal to the transmission of the substrate.19 Hence, assuming that the sample is in air, T max = 90% and 93% for films deposited on glass and fused silica, respectively. The minimum sample transmission (T min) in air is expressed by:2min 2224(1)()sub sub n n T n n n =++As most TCO films have values of n in the VIS in the range 1.8 – 2.8, T min will be in the range 0.8 – 0.52. T min is closely approximated by the relation: T min = 0.051n 2-0.545n +1.654. As n in the VIS decreases with wavelength, T min increases with wavelength, but will not exceed ~0.8. When the film extinction coefficient is not negligible and affects the transmission, T max < T sub , and T min also decreases. By decreasing the TCO film thickness, T is increased but the sheet resistance decreases. Combining together the optical and electrical properties of the film, the fraction of the flux absorbed in a film (A ) is given by the expression:1exp RA α −σ≅− Fig. 1 presents plots of the fraction of the absorbed power at wavelength of 400 nm and k ~0.02 as a function of the conductivity for three representative values of R S . For a given σ, low values of R S necessitate using thick films, and lower conductivity requires the use of even thicker films, resulting in an increase in the loss of radiative power. The dependence of film thickness on the conductivity for three values of R s is presented in Fig. 2.Fig. 1Fig.1. Fraction of absorbed power as function of TCO conductivity.Using the same film conductivity, applications requiring the lowest R S will be thicker and, and the absorbed fraction will be higher. At present, only high quality ITO is compatible at present with the condition that the absorbed power fraction be lower than 10% and R S = 10 Ω. At lower extinction coefficient (k) films with lower conductivities can be used, e.g., when k = 0.002 instead of 0.02, the absorbed power A is lower by a factor of ~8, and allows the use of thicker films. The combination of film thickness, conductivity, and extinction coefficient determine the absorption of the radiation flux. However, when the total transmission T is considered, reflection and interference must be considered, which depend on the refractive indices of the substrate and the film, and the film thickness. A general formula for T and R was given by Cisneros.20Fig. 2. TCO film thickness as function of film conductivityIV. Trends in the development of TCO materialsWhile the development of new TCO materials is mostly dictated by the requirements of specific applications, low resistivity and low optical absorption are always significant pre-requisites. There are basically two strategies in managing the task of developing advanced TCOs that could satisfy the requirements. The main strategy dopes known binary TCOs with other elements, which can increase the density of conducting electrons. As shown in Table 1, more than 20 different doped binary TCOs were produced and characterized,21 of which ITO was preferred, while AZO and GZO come close to it in their electrical and optical performance. Doping with low metallic ion concentration generates shallow donor levels, forming a carrier population at room temperature. Doping In2O3 with Sn to form ITO substantially increased conductivity. It is believedthat substituting Sn4+ for In3+ provides carrier electrons, as Sn4+ is supposed to act as a one-electron donor.22 Similarly, aluminum is often used for intentional n-type doping of ZnO, but other group III impurities, such as Ga and In, and group IV, such as Sn and Ge, also work. Doping by Al produced the relatively high conductivity AZO. Doping with non-metallic elements is also common, e.g., ZnO:Ge (GZO), SnO2:F (FTO) and SnO2:Sb (ATO).23,24 Recently, AZO films with resistivityρ ~8.5.10-5 Ω.cm was reported by Agura et al.25 An even lower resistivity was reported for GZO, ~8.1. 10-5Ω.cm.26 This ρ is very close to the lowest resistivity of ITO27 of 7.7·10-5Ω.cm, with a free carrier density of 2.5.1021 cm-3.Table 1. TCO Compounds and DopantsTCO DopantSnO2Sb, F, As, Nb, TaZnO Al, Ga, B, In, Y, Sc, F, V, Si, Ge,Ti, Zr, Hf, Mg, As, HIn2O3Sn, Mo,Ta, W, Zr, F, Ge, Nb, Hf, MgCdO In,SnTa2OGaInO3Sn, GeCdSb2O3YThe above described metallic dopant ions should have appropriate valency to be an effective donor when replacing the native metallic ion. However, when an O2- ion is replaced with a F- ion, a donor level is again produced. Thus, doping SnO2 by F increased the carrier electron mobility by a factor of ~2 and their concentration also by a factor of 2, reducing the resistivity by a factor of 4.28 The concentration of F- dopant ions should not exceed an upper limit, as an increase in carrier scattering by F ions led to a decrease in the conductivity.29 Doping SnO2 with Sb initially introduces Sb5+ ions that act as donors. When the doping concentration was increased beyond a certain level, however, Sb3+ ions began to replace the Sn4+ ions. The introduction of Sb3+ ions generates an acceptor level that compensates the donors and increases the resistivity.This effort to increase the conductivity without degrading the transparency was paralleled by a more elaborate strategy in which phase-segregated two-binary and ternary TCOs were synthesized and characterized. The phase-segregated two-binary systems include ZnO-SnO2, CdO-SnO2, andZnO-In2O3. In spite of the expectations, the electrical and optical properties of the two-binary TCOswere much inferior to those of ITO. The phase diagram of the ternary TCOs could be schematicallypresented by a three-dimensional or four-dimensional phase combination of the most commonternary TCO materials.21,30 based on known binary TCO compounds. Accordingly, the ternary TCOcompounds could be formed by combining ZnO, CdO, SnO2, InO1.5 and GaO1.5 to obtain Zn2SnO4,ZnSnO3, CdSnO4, ZnGa2O4, GaInO3, Zn2In2O5, Zn3In2O6, and Zn4In2O7. However, as Cd and itscompounds are highly toxic, the utilization of these TCOs is limited, though they have adequateelectrical and optical properties. Other binary TCOs were synthesized from known binary TCOsand also from non-TCO compounds, such as In6WO12 and the p-type CuAlO2.The first-principle model of Kiliç and Zunger, showed the importance of the composition inturning an insulating oxide into a TCO. However, structural considerations should also be included.Hosono et al.31 investigated the conditions for depositing wide-gap amorphous oxides with highelectron mobility. They indicated that since the mobility is proportional to the width of theconduction bands, a large overlap between relevant orbitals is required. In addition, the magnitudeof the overlap needs to be insensitive to the structural randomness that is intrinsic to the amorphousstate. They assumed that since the spatial spreading of the ns orbital is large and the overlapbetween these ns orbitals with spherical symmetry is large and insensitive to any angular variationsin the M-O-M bonds (where M is a metal cation) compared with p-p or d-p orbitals having highanisotropy in geometry. Oxides composed of metal cations with an electronic configuration (n-l)d10ns0 would satisfy these requirements, as the lowest part of the conduction band in these oxidesis primarily composed of ns orbitals.32 Hosono et al. also conjectured that because of this, ternaryoxides are preferred to binary oxides for the formation of amorphous TCO thin films. Scanning theperiodic table, they identified 105 combinations of elements as promising ternary oxide candidates.As indicated by Mizoguchi and Woodward, not only do binary n-type TCO materialscontain a metal with (n -1)d10ns0 electronic configuration, but also the ternary and quaternarycomplex TCOs. In a study of CdSnO3, Cd2SnO4, and CdIn2O4, Shannon et al. conjectured that theformation of a transparent conductor could result from edge sharing of Cd2+, In3+, and Sn4+octahedra.33 Nearly all of the complex TCOs found to date possess cations in octahedral coordination, as do most binary TCOs, with the exception of ZnO (wurtzite structure) and β-Ga2O3.These and other studies show that similar complex oxides may be a rich source of new TCO 353637 Mizoguchi and Woodward concluded, however, that based on their research the materials.34,,,only necessary condition for an oxide, binary or complex, to be a transparent conductor was to havea structure causing the lowest energy band to be dispersed and split off from the rest of theconduction band, whereas continuous edge sharing of the structural octahedra is only accidental.The lowest energy band in the conduction band of an effective transparent conductor should be wide so that carriers introduced upon doping will be highly mobile. This condition is met when the anion coordination environment is fairly symmetric, as is the case in binary TCOs. This is a necessary but not sufficient condition for transparent conductivity. The second condition for a good TCO material is that it must be possible to effectively populate the conduction (or valence) band by doping, and that the doping should not seriously degrade the carrier mobility or the optical transmission.8,31.Considering the ternary TCO compound (A x M y O z), where A is a lower valency cation and M is a main group ion with higher valency, if the valance of the A-O and M-O interactions were not too different, as they would be when the A-cation has an (n - 1)d10ns0 electron configuration, the oxygen bonding was likely to remain reasonably symmetric and a disperse conduction band would result, in agreement with the necessary condition specified above. The dispersion of the conduction band energy in such compounds may not be as large as in a binary oxide, yet, there could be extra freedom to manipulate the composition and structure of such oxides, facilitating the adaptation of the electronic energy levels for applications with specific needs.All of the TCOs discussed above are n-type semiconductors. In addition, p-type doped TCOs were also developed and could find interesting future applications, in particular in the new optoelectronic field of “transparent electronics”.38 Fabricating undoped or doped p-type TCOs was found to be more difficult than the n-type. The first p-type TCO was made from CuAlO2 by Kawazoe in 1997.39 Prior to this, however, in 1993 Sato et al. reported on a semi-transparent p-type TCO with ~40% visible transmission.40 It has been reported that is possible to form acceptor levels in ZnO, doping with N, P and As. The difficulty in producing p-type oxide was hypothesized to result from the strong localization of holes at oxygen 2p levels or due to the ionicity of the metallic atoms. O 2p levels are far lower lying than the valence orbit of metallic atoms, leading to the formation of a deep acceptor level with the holes. Hence, these holes are localized and require sufficiently high energy to overcome a large barrier height in order to migrate within the crystal lattice, resulting in poor hole-mobility and conductivity.41,42 Following this hypothesis, an effort was made to grow p-type TCO based on “Chemical Modulation of the Valence Band (CMVB)”, where the oxide composition and structure were expected to delocalize the holes in the valence band. The recent detailed report of Benerjee and Chattopadhyay lists several groups of such synthesized p-type TCOs, e.g., CuM iii O2, AgM iii O2 where M iii is a trivalent ion. Compared with the n-type TCOs, these TCO have relatively lower conductivities, of the order of 1 S/cm, and lower transmission, < 80%.Growing p-ZnO was an important milestone in ‘‘Transparent Electronics’’, allowing fabrication of wide band gap p-n homo-junctions, which is a key structure in this field. It was anticipated that higher conductivity and optical transmission could be obtained by doping ZnO with N, F, P, Sb, and As, however, it was also shown that such doping had some serious limitations.43,44 Based on first principle calculations, Yamamoto and Yoshida45 proposed that co-doping of donor-acceptor dopants (e.g. Ga and N, respectively) in ZnO might lead to p-type ZnO. Joseph et al. applied this principle to simultaneously dope ZnO with an acceptor (N) and a donor (Ga), where the acceptor concentration was twice that of the donor. The optical transmission was greater than 85%, but the conductivity was low, ~1 S/cm.46 p-type ZnO:Sb was deposited with a filtered vacuum arc equipped with a Zn cathode doped by Sb.47 The conductivity was ~0.5 S/cm, the mobility 9-20 cm2/Vs and the hole density ~4·1016 cm-3, with transmission of ~85%. It is evident that the challenge to grow p-type TCO with ρ ~ 10-3 Ω.cm, or better, still exists.The need to produce n-type TCOs with higher conductivity and better transmission, without relying on In, inspired research and development effort to discover and study some unconventional TCOs . Novel transparent conductors were proposed using oxides with s2 electron configurations. Oxides of Mg, Ca, Sc and Al also exhibited the desired optical and electronic features; however, they have not been considered as candidates for achieving good electrical conductivity because of the challenge of efficiently generating carriers in these wide band gap materials. The approach suggested was to increase the mobility rather than the carrier density. If this goal could be achieved, the optical properties would not deteriorate at lower resistivity. Recently, mobility with more than twice that of commercial ITO was observed in Mo-doped In2O3 (IMO), and it was shown that the conductivity can be significantly increased with no changes in the spectral transmittance upon doping with Mo.48,49 Electronic band structure investigations of IMO by Medvedeva revealed that the magnetic interactions which had never been considered to play a role in combining optical transparency with electrical conductivity ensure both high carrier mobility and low optical absorption in the visible range.50Recently, new thin film geometries were also explored in search of TCO films with higher conductivity. Dingle et al.51 showed that higher conductivity could be obtained by doping modulation, which spatially separates the conduction electrons and their parent impurity atoms (ions) and thereby reduced the effect of ionized and impurity scattering on the electron motion. Rauf52 used a zone confining process to deposit ITO with ρ = 4.4·10-5 Ω.cm and μ = 103 cm2/Vs. The highly and lowly doped regions were laterally arranged in the films, rather than vertically as in superlattice structures. A theoretical outline of a method to engineer high mobility TCOs was presented by Robbins and Wolden,53 based on the high mobility transistor structure discovered。

光纤延时线-手动微调款 (ODL-100)说明书

光纤延时线-手动微调款 (ODL-100)说明书

OPTICAL DELAY LINESFeatures•Low insertion lossDelay Line with Manual Lead Screw (ODL-100)Reflector Style Delay Line with Manual Lead Screw (ODL-600)Delay Line with Micrometer (ODL-200)Delay Line with Servo Motor (ODL-300)Miniature Delay Line (ODL-700)Reflector Style Delay Line with Servo Motor (ODL-650)Extended (330 ps or 600 ps) Manual ReflectorStyle Delay Line (ODL-600)NEWExtended (330 ps or 600 ps) Reflector Style Delay Line with Servo Motor (ODL-650)NEWFigure 1. Dimensions of ODL-100 Model Figure 2. Dimensions of ODL-200 Model Delay lines are offered using singlemode, multimode or Polarization Maintaining (PM) fibers. In general, OZ Optics uses polarization maintaining fibers based on the PANDA fiber structure when building polarization maintaining components and patchcords. However OZ Optics can construct devices using other PM fiber structures. We do carry some alternative fiber types in stock, so please contact our sales department for availability.If necessary, we are willing to use customer supplied fibers to build devices.Delay lines are offered in both manual or electrically controlled versions. Manual delay lines utilize either a lead screw or a micrometer to adjust the spacing. Electrically controlled versions utilize a servo motor with encoders to monitor the motion. With this device submicron resolution (<0.003ps) is achieved. The delay line is easily controlled by a computer via an RS-232 interface or manually using some simple TTL input signals. These devices are calibrated to provide the delay in picoseconds. Home and end position sensors prevent accidental damage to the device.A miniature style delay line provides up to 13 picoseconds delay in a miniature package. The unit takes up little more space than an ordinary patch-cord connection, and is easily adjustable and lockable.Units are in inches.Units are in inches.2-56 UNC TAPPED3.42” [87mm] (REF)0.40” [10.2mm]Delay Adjustment KnobDelay Lock NutFigure 5. Dimensions of ODL-700 Model Figure 3. Dimensions of ODL-300 ModelFigure 4. Dimensions of ODL-600 Model Units are in inches.Units are in inches.Units are in inches.2-56 UNC TAPPED4.124.00Figure 6. Dimensions of ODL-650 Model 2.00B0.5310.69 0.3751.190.430.66 1.370.191A1.190.6442-56UNC-2B4PLCS.0 0.06C A0 0.0601.942.00Figure 7. Dimensions of ODL-650 Model: Extended range 330 ps and 600 ps Units are in inches.Units are in inches.Dim.330 ps 600 psA 4.12 6.12B 5.227.22C4.066.06Bar Code Part NumberDescription13757ODL-650-11-1550-8/125-P-60-3A3A-1-1-MC/RS232Electrically Controlled Reflector Style Variable Fiber Optic Delay Line for 1550 nm, with 60 dB return loss. Pigtails are 1 meter long, 8/125 PM fibers, protected with 0.9 mm OD hytrel tubing, and with FC/APC connectors, RS232 Interface.Ordering Examples For Standard PartsA customer is building a polarization mode dispersion compensator using a polarization maintaining electrically controlled delay line and com-puter interface. The delays in their system are 50 picoseconds or less. His system is sensitive to both insertion losses and return losses, so a low return loss device is needed.Bar Code Part NumberDescription9432 ODL-100-11-1550-9/125-S-60-3A3A-3-1 Variable Fiber Optic Delay Line for 1550 nm, with manual lead screw and 60 dB return loss. Pigtails are 1 meter long, 3 mm OD PVC cabled 9/125 SM fibers, FC/APC connectors.13421 ODL-100-11-1550-8/125-P-60-3A3A-3-1 Variable Fiber Optic Delay Line for 1550 nm, with manual lead screw and 60 dB return loss. Pigtails are 1 meter long, 3 mm OD PVC cabled 8/125 PM fibers, FC/APC connectors.10468 ODL-200-11-1550-8/125-P-60-3A3A-1-1 Variable Fiber Optic Delay Line for 1550 nm, with manual micrometer and 60 dB return loss. Pigtails are 1 meter long, 8/125 PM fibers, protected with 0.9 mm OD hytrel tubing, and with FC/APC connectors.14645 ODL-600-11-1550-9/125-S-60-3A3A-1-1 Reflector Style Variable Fiber Optic Delay Line for 1550 nm, with manual lead screw and 60 dB return loss. Pigtails are 1 meter long, 0.9 mm OD tight buffered 9/125 SM fibers, FC/APC connectors.13755 ODL-600-11-1550-8/125-P-60-3A3A-1-1Reflector Style Variable Fiber Optic Delay Line for 1550 nm, with manual lead screw and 60 dB return loss. Pigtails are 1 meter long, 8/125 PM fibers, protected with 0.9 mm OD hytrel tubing, and with FC/APC connectors.13756 ODL-650-11-1550-9/125-S-60-3A3A-1-1-MC/RS232 Electrically Controlled Reflector Style Variable Fiber Optic Delay Line for 1550 nm, with 60 dB return loss. Pigtails are 1 meter long, 0.9 mm OD tight buffered 9/125 SM fibers, FC/APC connectors, RS232 Interface.13757ODL-650-11-1550-8/125-P-60-3A3A-1-1- MC/RS232Electrically Controlled Reflector Style Variable Fiber Optic Delay Line for 1550 nm, with 60 dB return loss. Pigtails are 1 meter long, 8/125 PM fibers, protected with 0.9 mm OD hytrel tubing, and with FC/APC connectors, RS232 Interface.Ordering Information For Standard Parts For more Standard Parts, please see our Online Catalog Figure 8. Dimensions of ODL-600 Model: Extended range 330ps and 600ps Units are in inches.2.00B0.69 0.3750.4971.190.43A1.190.6442-56UNC-2B 4PLCS.0 0.06C A0 0.061.942.00 Dim.330 ps 600 ps A 4.12 6.12B 4.80 6.80C4.066.06Environmental Specification For Singlemode Or PM ODL-650 Systems At 1550 nmOperating Temperature (°C)-10°C to +60°CTemperature Dependent Loss (Measured over the Entire Scanning Range)<1 dB from +10°C to +40°C <2 dB from -10°C to +60°COperating LifetimeOver 5000 hours, continuous operationStandard Product SpecificationsTable 1. Manual delay lineTable 2. Motorized delay line1Theoretical, based on thread pitch and motor/encoder resolution. The MC/RS232 versions of the ODL-300 and ODL-650 can generate two counts per encoder pulse, effectively doubling the resolution.2Includes variation of insertion loss over the entire travel range.3For 1550nm wavelengths singlemode or PM fibers, at room temperature.4ODL-600 and ODL-650 delay lines are offered with 167psec delay range as standard, or 330psec, or 600psec as an option.5An 8mm/sec version is offered.6This is the maximum speed. The speed may be programmed to a lower value by the user.Application NotesExample Application:Polarization mode dispersion (PMD) is an important issue in the quest to build high speed (10GBs, 40GBs, and high-er) communication networks. An input signal travelling along a single mode fiber normally has some distortion, due to polarization mode dis-persion. The signal effectively has been split into two arbitrary, yet orthogonal polarizations, and one polarization is leading the other. A delay line is a crucial element in building compensators for PMD.The figure below shows how to use a delay line to compensate for polarization modes dispersion. The light from the singlemode input is split into two using a polarizing beam splitter. A polarization controller installed just before the splitter is used to convert the arbitrary polarizations that the signal has been split into S and P polarization. The faster S polarization is routed through the delay line while the slower P polariza-tion is sent straight into the combiner. The combined signals then reach the receiver. A control system monitors the quality of the signal at the receiver, and dynamically adjusts the polarization and the delay to get the two signals to match up again. Thus the PMD is in the system Part NumberDescriptionODL-650-11-1300-9/125-S-60-XX-1-1,10 -MC/RS232-330Electrically controlled reflector style variable fiber optic delay line for 1300 nm with 60 dB return loss. Pigtails are 1 meter long on the input, 10 meters long on the output 0.9 mm OD hytrel jacketed 9/125 singlemode fibers, no connectors. Unit comes with a RS232 interface, 330 psec delay range.Ordering Examples For Custom PartsA customer building an interferometer needs a motorized reflector style delay line for 1300nm, using singlemode fiber. He needs pigtails 1meter long on one side, and 10meters long on the other side, and does not need connectors. Because he is fusion splicing, he prefers uncabled fiber. He needs as long a travel range as possible at least 250psecond. Return losses do need to be as low as possible, to prevent additional interference effects. He will control with RS232 commands.ODL-A -11-W -a/b -F -LB -XY -JD -L (-I )A = Version:100 = Standard Style, with lead screw 200 = Standard Style, with micrometer300 = Standard Style, with DC servo motor 600 = Reflector Style, with lead screw*650 = Reflector Style, with Servo motor*700 = Miniature Style* at the end of the part number add- 330 for 330 ps option - 600 for 600 ps option(available for 1550 nm, 1310 nm, and 1064nm)L = Fiber length, in meters, on each side of the device.Example: To order 1 meter of fiber at the input and 7 meters at the output, replace the L with 1,7W = Wavelength: Specify in nanometers(Example: 1550 for 1550 nm)a/b = Fiber core/cladding sizes, in microns,9/125 for 1300/1550 nm SM fiber sizes 8/125 for 1550 nm PM fiber sizesSee Tables 1 to 5 of the Standard Tables https:///ALLNEW_PDF/DTS0079.pdf data sheet for other fiber sizesF = Fiber type: M=MultimodeS=SinglemodeP=Polarization maintaining LB = Backreflection level: 40 dB forwavelength outside 1300–1550 nm. 60dB for 1300 and 1550 nm only. Multimode devices are only available with 35 dB.JD = Fiber Jacket type:1 = 900 micron OD hytrel jacket3 = 3 mm OD kevlar reinforced PVC cable See Table 7 of the Standard Tableshttps:///ALLNEW_PDF/DTS0079.pdf for other jacket sizes.X ,Y = Input & Output Connector Codes:X = No connector3S = Super NTT-FC/PC 3U = Ultra NTT-FC/PC 3A = Angled NTT-FC/PC 8 = AT&T-ST SC = SCSCA = Angled SC LC = LCLCA = Angled LC MU = MUI = Interface (ODL-300 & 650 models only)MC/RS232 for Intelligent RS232 Interface with built-in manual TTL control lines PC for direct connections to the motor, encoder and limit switches (no driver).Ordering Information For Custom PartsOZ Optics welcomes the opportunity to provide custom designed products to meet your application needs. As with most manufacturers, cus-tomized products do take additional effort so please expect some differences in the pricing compared to our standard parts list. In particular, we will need additional time to prepare a comprehensive quotation, and lead times will be longer than normal. In most cases non-recurring engi-neering (NRE) charges, lot charges, and a 1 piece minimum order will be necessary. These points will be carefully explained in your quotation,so your decision will be as well informed as possible. We strongly recommend buying our standard products.Questionnaire For Custom Parts1.What Delay Range (in psec or mm) do you need?2.What Resolution (in psec or mm) do you need?3.Do you need a readout of the position?4.Do you need electrical control?5.Do you need computer control? What Interface will you use?6.Do you intend to make your own drive circuit?7.What wavelength will you be using?8.What fiber type are you using? Singlemode, Multimode or Polarization Maintaining?9.What is the worst acceptable return loss?10.What kind of fiber connectors are you using?Figure 9. PMD Compensation System Using a Variable Delay LineMounting:The base of the delay lines have mounting holes for attachment to a rack or printed circuit board. For best results, the mounting surface should be rigid and free of vibration. Do not over-tighten the mounting screws and use screws that thread in no more than。

选区激光熔化AlSi10Mg合金镜的表面性能

选区激光熔化AlSi10Mg合金镜的表面性能

第51卷第11期2020年11月中南大学学报(自然科学版)Journal of Central South University(Science and Technology)V ol.51No.11Nov.2020选区激光熔化AlSi10Mg合金镜的表面性能韩潇1,2,康楠3,焦建超1,2,王超1,2(1.北京空间机电研究所,北京,100094;2.先进光学遥感技术北京市重点实验室,北京,100094;3.西北工业大学凝固技术国家重点实验室,陕西西安,710072)摘要:基于激光增材制造技术适用于复杂轻量化结构光学元件的快速成形,且采用同种材料一体化光机结构能够降低空间光学成像系统的温度敏感性,提高稳定性,利用选区激光熔化(SLM)技术制备全铝空间光学相机用AlSi10Mg铝合金反射镜。

研究结果表明:采用SLM制备的AlSi10Mg铝合金组织致密(相对密度大于99.5%),且退火后力学性能优异;通过单点金刚石车削(SPDT)获得光学级表面,表面粗糙度达8~ 13nm,面形精度达到0.28λ(λ为波长,λ=632nm)。

该研究结果可以应用于空间光学反射镜的设计与制造。

关键词:增材制造;选区激光熔化;铝镜;空间光学;表面性能;金刚石车削中图分类号:TB34;TG113文献标志码:A开放科学(资源服务)标识码(OSID)文章编号:1672-7207(2020)11-3088-05Surface characteristics of selective laser melted AlSi10Mg mirrorsHAN Xiao1,2,KANG Nan3,JIAO Jianchao1,2,WANG Chao1,2(1.Beijing Institute of Space Mechanics and Electricity,Beijing100094,China;2.Beijing Key Laboratory of Advanced Optical Remote Sensing Technology,Beijing100094,China;3.State Key Laboratory of Solidification Processing,Northwestern Polytechnical University,Xi'an710072,China)Abstract:Considering that additive manufacturing(AM)technologies is adapted for the optical components with complex lightweight structure,using the opto-mechanical structure with the same material can reduce temperature sensitivity,selective laser melting(SLM)technology was utilized to fabricate the AlSi10Mg mirror for aluminum alloy space optical sensor.The results show that the relative density of as-fabricated AlSi10Mg sample is above99.5%,and the tensile strength and the ductility are excellent.The single point diamond turning(SPDT)is appliedto deliver the optical surface with thoughness of8−13nm and accuracy of0.28λ(λ=632nm).The results can be used to manufacture the lightweight space optical mirrors.Key words:additive manufacturing;selective laser melting;aluminum mirror;space optical;surface characteristics;diamond turningDOI:10.11817/j.issn.1672-7207.2020.11.010收稿日期:2020−08−26;修回日期:2020−09−22基金项目(Foundation item):国家自然科学基金资助项目(U1537105)(Project(U1537105)supported by the Natural National Science Foundation of China)通信作者:韩潇,博士,高级工程师,从事空间光学遥感器先进制造及其材料性能评价技术研究;E-mail:hanxiao1998@126.com第11期韩潇,等:选区激光熔化AlSi10Mg合金镜的表面性能随着空间光学遥感技术的迅速发展,高分辨率轻质空间光学相机已成为各国研究热点。

翻译稿稀疏孔径成像系统的设计与实现

翻译稿稀疏孔径成像系统的设计与实现

稀疏孔径成像系统的设计与实现Soon-Jo Chung*, David W. Miller**, Olivier L. de Weck***空间系统实验室,麻省理工学院,马萨诸塞州,02139,美国摘要为了更好地了解在设计和建设稀疏孔径阵列中遇到的技术困难,进行了建设白光Golay-3望远镜的挑战项目。

麻省理工学院自适应侦察Golay-3光学卫星(Adaptive Reconnaissance Golay-3 OpticalSatellite ,ARGOS)项目利用广角斐索干涉仪技术重点是将光学和航天器子系统模块化。

开发出了独特的设计程序包括相干波前传感的性质,控制和结合其它各种系统工程的多个方面,以实现成本效益。

为了演示一个完整的航天器在1-g的环境中的运行情况,ARGOS 系统被安装在一个无摩擦的气浮轴承上,并具有能够跟踪像国际空间站或行星这类快速轨道卫星的能力。

利用波前传感技术减少初始偏差,并反馈实时畸变到光控制环路。

本文介绍了ARGOS系统在构想、设计和实施阶段的得出的不用结果和经验。

初步评估报告表明光束组合是稀疏光学阵列中最具挑战性的问题。

由于公差紧束的原因,进行光学控制是最重要的。

波前传感/控制要求似乎是一种主要的技术和成本动因。

关键词:稀疏孔径;多孔径光学系统;斐索干涉仪;相控阵望远镜1简介在天文学中要求更大的细角分辨率就必须要增大望远镜的口径。

但是,空间望远镜的主镜口径受到体积、运载火箭的最大承受重量以及制造成本的限制[1]。

因为单个镜片的制造成本随着面积的增大而飞速上升,比如像哈勃空间望远镜就已经处于经济上可行的极限,我们正采用像分段镜望远镜和干涉稀疏孔径光学系统这些突破性的技术来努力打破这一趋势。

而长基线恒星迈克尔逊干涉仪从一个独立的收集器中提供光源进行光束合成,在一段时间后获得干涉条纹,斐索干涉仪能产生具有完全即时U-V覆盖的直接图像。

因此,斐索干涉仪是适合于扩展对象的光学成像和快速变化的目标。

光学模型介绍英文作文

光学模型介绍英文作文

光学模型介绍英文作文英文:Optical models are mathematical representations of how light interacts with different materials and surfaces. They are used in a variety of fields, including computer graphics, physics, and engineering.In computer graphics, optical models are used to simulate how light behaves in a virtual environment. For example, a ray tracing algorithm can use an optical model to calculate how light will reflect off of different surfaces in a 3D scene. This can create realistic lighting effects, such as reflections and shadows.In physics, optical models are used to study the properties of light and how it interacts with matter. For example, an optical model can be used to calculate the refractive index of a material, which determines how much light is bent when it passes through the material. This isimportant in fields such as optics and photonics.In engineering, optical models are used to design and optimize optical systems, such as lenses and mirrors. An optical model can be used to calculate the focal length of a lens, for example, which determines how much the lens will magnify an image.Overall, optical models are an important tool for understanding and manipulating light. They allow us to create realistic visual effects, study the properties of light, and design optical systems that meet specific requirements.中文:光学模型是一种数学表达方式,用于描述光在不同材料和表面上的相互作用。

FCC规定设备说明书

FCC规定设备说明书

used in accordance with the instructions manual, may cause interference to radio communications. It has been tested an found to comply with limits for a Class A digital device pursuant to subpart J of Part 15 of FCC Rules, which are designed to provide reasonable protection against interference when operated in a commercial environment. Operation of this equipment in a residential area is likely to cause interference in which case the user at his own expense will be required to take whatever measures to correctany person other than the authorized technicians opens the machine. The user should consult his/her dealer for the problem happened. Warranty voids if the user does not follow the instructions in application of this merchandise. The manufacturer is by no means responsible for any damage or Posiflex has made every effort for the accuracy of the content in this manual. However,technical inaccuracies or editorial or other errors or omissions contained herein, nor for direct, indirect, incidental, consequential or otherwise damages, including without limitation loss of data or profits, resulting from the furnishing, performance, or use of this material.“as is” and Posiflex Technologies, Inc. expressly disclaims any warranties, expressed, implied or statutory, including without limitation implied warranties of merchantability or fitness for particular purpose, good title and The information in this manual contains only essential hardware concerns for general user and is subject to change without notice. Posiflex reserves the right to alter productBRIEF INTRODUCTIONTHE PRODUCTThe PD-309/ PD-2605 is a pole mount customer display option designed for Posiflex mini slim base of KS-2010 or DT-20X POS terminals. It is delivered in separate carton for the host system and shall be installed per instructions in this manual.FEATURES• LCD (Liquid crystal display) with dark blue character and yellowgreen back-light for PD-309• Bright VFD (vacuum fluorescent display) with green filter for PD-2605• Two-line display with 20 characters per line• Easy viewing characters (6.0 mm by 9.66 mm for PD-309 / 9.03mm by 5.25 mm for PD-2605)• Long life and trouble free operation• 15¢X, 30¢X and 45¢X adjustable viewing angles• Display frame can rotate horizontally 270° freely• Selectable command emulation modes including PST and EPSONcommand emulation modes for PD-309• Various command emulation modes selectable by DIP switch forPD-2605• Support 13 Code Pages of 128 characters each for PD-2605• Support 12 international character sets of 12 characters each forPD-2605• Simple installation• Selectable between Serial (RS232) interface model and USBinterface model• Supports UPOS 1.8 and is WEPOS ready for PD-2605metal base plate of the PD to bottom of mini slim base or DT-20X at the circled positions. For mini slim base Connect the interface cable to go into the base through at right to the main unit. For DT-20X arrange the interface cable to go through underbottom to connector area arrowed in Pix. 1 at above right.COMMAND EMULATION MODE SETUP (FOR PD-2605)Now please check the back of PD-2605 display head as in the above left picture in Pix. 3. There is a small piece of plastic cover for the “DIP switch window”. Slide the cover downward but don’t pull it off otherwise you may have to practice for inserting it back. You can find 6 positions ofDIP switch windowPix. 3Pix. 2Pix. 1SPECIFICATIONOPTICALNumber of digits 20 digits/row, 2 rowsDot matrix 5 X 7 dotsDigit height 9.66 mm (PD-309) / 9.03 mm (PD-2605) Digit width 6.0 mm (PD-309) / 5.25 mm (PD-2605) Display color Dark blue (PD-309) / Green (PD-2605)MECHANICALTotal Height 283 mmDisplay Head Height 57.5 mmDisplay Head Width 196.6 mmDisplay Head Depth 39.5 mmCase color BlackELECTRICAL。

用于光束整形与超分辨成像的衍射光学元件的设计和实验的开题报告

用于光束整形与超分辨成像的衍射光学元件的设计和实验的开题报告

用于光束整形与超分辨成像的衍射光学元件的设计和实验的开题报告摘要:本文介绍了一种基于衍射光学元件的光束整形和超分辨成像的方法,包括设计、制备和实验。

首先,我们使用Zemax软件来设计一种衍射光学元件,将光束结构进行整形。

我们采用库仑算法进行优化设计,以在指定波长下得到最佳成像质量。

然后,我们使用电子束光刻技术在光学玻璃基片上制备了该元件,并进行了表征。

最后,我们使用超分辨成像技术对该元件进行了测试。

实验结果表明,该衍射光学元件能够有效地整形光束,并实现超分辨成像。

本文的研究对于光束整形和超分辨成像的应用具有一定的理论和实验参考价值。

关键词:衍射光学元件;光束整形;超分辨成像;光学玻璃基片;库仑算法;电子束光刻技术Abstract:This paper presents a method of beam shaping and super-resolution imaging based on diffractive optical elements, including design, fabrication, and experiments.Firstly, we use Zemax software to design a diffractive optical element that shapes the beam structure. We use the Coulomb algorithm for optimized design to obtain the best imaging quality at a specified wavelength. Then, we use electron beam lithography technology to fabricate the element on an optical glass substrate and characterize it. Finally, we test the element using super-resolution imaging technology. The experimental results show that the diffractive optical element can effectively shape the beam and achieve super-resolution imaging.The research in this paper has certain theoretical and experimental reference value for the application of beam shaping and super-resolution imaging.Keywords: diffractive optical element; beam shaping; super-resolution imaging; optical glass substrate; Coulomb algorithm; electron beam lithography technology1.研究背景和意义光束整形和超分辨成像作为现代光学技术的前沿领域,在科学和工程应用中发挥着越来越重要的作用。

  1. 1、下载文档前请自行甄别文档内容的完整性,平台不提供额外的编辑、内容补充、找答案等附加服务。
  2. 2、"仅部分预览"的文档,不可在线预览部分如存在完整性等问题,可反馈申请退款(可完整预览的文档不适用该条件!)。
  3. 3、如文档侵犯您的权益,请联系客服反馈,我们会尽快为您处理(人工客服工作时间:9:00-18:30)。

2. Absorption only
The simplest participating medium has cold perfectly black particles which absorb all the light that they intercept, and do not scatter or emit any. For simplicity, assume that the particles are identical spheres, of radius r and projected area A =πr2, and let ρ be the number of particles per unit volume. Consider a small cylindrical slab with a base B of area E, and thickness ∆s, as shown in figure 1, with the light flowing along the direction ∆s, perpendicular to the base. The slab has volume E∆s, and thus contains N = ρE∆s particles. If ∆s is small enough so that the particle projections on the base B have low probability of overlap, the total area that they occlude on B is approximated by NA = ρAE∆s. Thus the fraction of the light flowing through B that is occluded is ρAE∆s/E = ρA∆s. In the limit as ∆s approaches zero, and the probability of overlap approaches zero also, this gives the differential equation dI ---- = – ρ ( s ) AI ( s ) = – τ ( s ) I ( s ) (1) ds
Interpolating f first permits the optical properties to change rapidly within a single volume element, to emphasize a small range of scalar values. It is possible to compute the optical properties only at the grid vertices, and then interpolate them instead, but this may eliminate fine detail. The situation is analogous to the superiority of Phong shading (interpolating the normal) over Gouraud shading (interpolating the shaded color) for representing fine highlight detail. To compute an image, the effects of the optical properties must be integrated continuously along each viewing ray. This does not mean that only ray tracing can be used. Mathematically equivalent integration can be performed with polyhedron compositing (Shirley and Tuchman [2], Max et al. [3], Wilhelms and van Gelder [4], Williams and Max [5]). If the integral is approximated by a Riemann sum, as discussed below, then the plane-by-plane compositing methods of Dreben et al. [6] and Westover [7] can also produce equivalent approximations. In this paper, I will not be concerned with the distinctions between these methods. Instead, I will deal with the mathematical forms that the continuous integral takes, depending on the optical model. Siegel and Howell [8] is a good general reference for the physics behind these models. The optical properties which affect the light passing through a “participating medium” are due to the absorption, scattering, or emission of light from small particles like water droplets, soot or other suspended solids, or individual molecules in the medium. For the models below, I will describe the geometric optics effects of the individual particles, and then derive a differential equation for the light flow in the medium. The differential equations are for a continuous medium, in the limit where the particles are infinitesimally small, so that the absorption, emission, and scattering take place at every infinitesimal segment of the ray. I will write the equations taking the intensity and optical properties to be scalars, for black-and-white images. For multiple wavelenin a color image, the equations are repeated for each wavelength, so these quantities become vectors.
1. Introduction
A scalar function on a 3D volume can be visualized in a number of ways, for example by color contours on a 2D slice, or by a polygonal approximation to a contour surface. Direct volume rendering refers to techniques which produce a projected image directly from the volume data, without intermediate constructs such as contour surface polygons. These techniques require some model of how the data volume generates, reflects, scatters, or occludes light. This paper presents a sequence of such optical models with increasing degrees of physical realism, which can bring out different features of the data. In many applications the data is sampled on a rectilinear grid, for example, the computational grid from a finite difference simulation, or the grid at which data are reconstructed from X-ray tomography or X-ray crystallography. In other applications, the samples may be irregular, as in finite element or free lagrangian simulations, or with unevenly sampled geological or meteorological quantities. In all cases, the data must be interpolated between the samples in order to use the continuous optical models described here. For example, linear interpolation can be used on tetrahedra, and trilinear or tricubic interpolation can be used on cubes. A number of other interpolation methods are given in Nielson and Tvedt [1]. Here I will just assume the interpolation is done somehow to give a scalar function f(X) defined for all points X in the volume. Optical properties like color and opacity can then be assigned as functions of the interpolated value f(X). (The physical meaning of these optical properties will be discussed in detail below.)
相关文档
最新文档