光学头二维力矩器的三自由度动力学模型研究

力矩器多维运动间的串扰和耦合是影响其动态特性和光斑质量的关键因素。针对力矩器单自由度简谐振动模型的不足,利用拉格朗日第二类方程,建立了二维力矩器的三自由度动力学模型,描述了力矩器聚焦和循迹有效运动、聚焦和循迹运动间的耦合作用以及扭转串扰运动特性,反映了力矩器四个关键点的不一致对其动态特性的定量影响。模型与实验结果对比表明,各自由度误差均小于5%,模型具有实用性,对力矩器的设计开发和串扰抑制具有理论指导作用。     

多导体传输线串扰实验不确定度的预测

利用随机降阶模型（SROM）对影响线缆串扰的不确定变量进行了敏感性分析,在此基础上预测了在这些不确定性变量影响下的串扰不确定度。并搭建三导体传输线串扰实验系统,测量了近端串扰和远端串扰,根据标准GB/Z 6113.401—2018/CISPR/TR 16-4-1:2009,评估了串扰实验的测量不确定度。将基于SROM方法的串扰不确定度,与实际测量获得的不确定度进行对比。结果表明,二者随频率变化趋势一致,且实验测试不确定度在预测不确定度范围内。采用SROM方法选取样本计算的不确定度可用于预测串扰实际测量结果不确定度。     

悬线式力矩器磁路设计中的有限元分析应用

光学头力矩器的空间磁场分布直接决定了力矩器的动态性能,对磁场进行准确分析是力矩器设计的前提。分析了悬线式力矩器的空间磁场产生机理,并采用有限元分析法进行了理论推导。以一款动线圈式二维对称型只读悬线式力矩器为例,采用有限元仿真软件（ANSYS）分析并设计了其空间磁场分布,对影响力矩器空间磁场分布的相关因素进行了分析。将采用有限元法对悬线式力矩器空间磁场仿真计算得出的力矩器动态特性参数与实测力矩器动态特性参数相比,其结果均符合力矩器的设计要求,证明基于有限元分析法的悬线式力矩器空间磁场设计是可行的。     

基于自由曲面的裸眼3D显示柱透镜光栅设计

设计了一种用于裸眼3D显示屏的低串扰新型双面柱透镜光栅板,光栅板的入射面为等间距排列的与显示器子像素数量相同的凹形自由曲面光栅结构,出射面为斜置的凸形自由曲面光栅结构.根据裸眼3D显示原理和几何光学原理推导了双面光栅板的光栅单元自由曲面设计公式和光栅参数计算公式.通过MATLAB编程计算和SolidWorks软件建模得到光栅板模型.用TracePro软件对所设计的光栅板模型进行光线追迹仿真,结果表明:参数优化后的6视点斜置柱透镜双面光栅3D显示在最佳视角的图像串扰度为0.068%,与传统6视点斜置柱透镜光栅的最佳视角图像串扰度相比降低了2个数量级,并且在观看距离2 000mm~3 000mm范围内图像串扰度基本不变.     

大气湍流信道中聚焦涡旋光束轨道角动量串扰特性

携带轨道角动量的涡旋光束作为传输信息的载体能有效提高信息传输效率,然而在传输过程中受大气湍流影响轨道角动量会发生串扰.基于螺旋谱分析理论,推导得到了聚焦拉盖尔高斯光束在各向异性大气湍流中传输时的螺旋谱解析表达式,并对比分析不同湍流和光束参数对聚焦与非聚焦拉盖尔高斯光束接收功率的影响,最后利用多相位屏法进行模拟验证.结果表明:随着传输距离、湍流强度、拓扑荷数的增大以及湍流内尺度、光束波长的减小,接收功率减小,轨道角动量串扰增大;接收孔径到达一定值时对轨道角动量串扰的影响非常小;聚焦光束比非聚焦光束的轨道角动量串扰要小.这些结果将对提高自由空间光通信的质量有一定意义.     

不同材料CMOS阵列电串扰特性的分析及比较

从传感器的响应及电子扩散原理分析了影响CMOS阵列串扰特性的几个主要因素。选择了锗、硅、砷化镓这几种常见的光电材料,分析并比较了材料特性对CMOS阵列串扰特性的影响。具体分析了三种光电材料在各自光谱响应峰值波长下,不同入射条件和结构参数对应电串扰的输出情况。结果表明:在相同条件下,锗材料制作的CMOS阵列具有最大的电串扰输出,在结构条件一致的前提下,入射光的功率在200μW时,锗材料CMOS阵列的串扰比硅和砷化镓材料分别高了58.97 mV、115.81 mV。结构参数对不同材料CMOS阵列具有相同的影响规律,但是锗材料CMOS的串扰变化最为显著,在其他参数不变的情况下,耗尽层宽度为1μm时,锗材料CMOS的串扰输出比硅和砷化镓材料的分别高了56.67mV、121.84 mV。分析结果为CMOS阵列材料的选择及串扰抑制技术提供了参考数据。     

光分组交换节点中缓存器对串扰相干特性的影响

研究了光分组交换中光输出缓存器引起的排队延迟对节点串扰特性的影响，建立了节点串扰特性与缓存器长度之间关系的数学模型，结果表明，对光分组交换节点，由于缓存器的存在，串扰源数目随缓存器的长度增加而增加；串扰中，非相干串扰占多数，数目随机的相干串扰的影响较小，且当缓存器较长时，相干串扰的影响可以忽略，即可将所有串扰视为非相干。     

532nm激光器光存储聚焦技术研究

在光存储系统中，为了保证存取信息所用的激光束准确地聚焦在记录介质表面上，必须具有精密自动调焦系统，该系统包括激光光源，扩束准直和整形光学元件，光学物镜，光电探测器，以及能上下运动的双轴力矩器。其中执行机构是在磁场中的双轴力矩器，线圈中电流不同时双轴力矩器拖动聚焦物镜上下移动，达到聚焦的目的。此过程中，位置探测器探测到焦点离存储介质表面的距离参数，并转化成聚焦误差信号，由此聚焦误差信号对物镜相对于存储介质的距离进行修正，从而使得激光束能准确地聚焦在介质表面上。结合532nm绿光，采用CDRW可擦写光盘，得到了约500nm的光存储斑。     

光交换芯片的串扰分析与DQPSK信号传输实验

串扰和插入损耗是表征光交换芯片传输性能的重要参数。将串扰与插入损耗特性结合起来,提出一种分析光交换集成芯片串扰的理论模型,考虑了串扰对开关路由的依赖性。实验测量了基于马赫-曾德尔干涉仪(MZI)的4×4拜尼兹结构的光交换集成芯片的串扰和插入损耗系数,以及不同开关路由状态下40 Gb/s差分四相相移键控(DQPSK)信号的传输性能,实验结果与理论分析基本一致。根据测得的串扰和插入损耗系数,计算了16×16光交换芯片串扰范围。     

偏振眼镜立体显示的立体串扰度及其影响因素

偏振眼镜立体显示是使用偏振片来分离左右眼图像的,偏振片的参数决定了偏振眼镜立体显示的性能好坏。提出了偏振眼镜立体显示的立体串扰度概念,推导了立体串扰度与偏振片旋转角度和偏振片偏振度的关系式。结果表明,立体串扰度随偏振片旋转角的变大而增大,随偏振片偏振度的增大而减小。因此为偏振眼镜立体显示的性能改善提供了依据。     

多参量同时测量的干涉型光纤传感器

提出用椭圆纤芯高双折射光纤偏振干涉和双模干涉结合的四参量以及双模干涉的多参量同时测量的传感理论和实验原理，对交叉灵敏度作了分析，同时给出了误差分析，并结合理论模型对灵敏度矩阵的状态作了粗略估计。     

Der Regenbogeneffekt und Interferenzerscheinungen bei molekularen Stößen

Crossed beam measurements of differential elastic scattering cross sections for collisions of alkali atoms with mercury and xenon atoms as well as with different molecules are presented. Special attention is given to the rainbow effect including supernumary rainbows and to interference effects connected with rainbow scattering. The observation of well resolved primary and supernumary rainbows together with interference patterns make the determination of a three parameter potential model possible. Partial wave numerical calculations of differential cross sections are used to evaluate potential parameters and to discuss the limits of the semiclassical rainbow theory. Elastic scattering between reactive collision partners is investigated too and interpreted in terms of a simple optical model.     

Study of nuclear-coulomb interference effects in inelastic deuteron scattering on 238U

The angular distributions of elastically and inelastically scattered deuterons from ²³⁸U at E = 17 MeV are compared to coupled-channel calculations. The cross sections at small scattering angles are strongly influenced by nuclear-Coulomb interference effects and allow a simultaneous extraction of nuclear (optical potential) and charge quadrupole deformation parameters. Two different deformed Coulomb potentials and the parameters of the optical model are discussed.     

微机械薄膜变形镜自适应光学系统实验研究

为求出自适应光学系统的最优校正电压, 提出了一种基于改进奇异值分解的闭环迭代控制算法。该算法可通过调节控制参量g1,g2和w,优化模式的收敛速度, 使控制信号快速收敛到一个可靠的局部最优解。搭建基于微机械薄膜变形镜(MMDM)的自适应光学系统, 测量光学影响函数并验证单个电极电压和镜面变形之间的准平方线性关系, 以及各个驱动器电极响应之间的线性叠加性。分别采用模拟眼和人眼出射波前作为原始波前进行实验。实验结果表明, 改进算法能快速有效地对静态或动态畸变波前进行校正, 为基于MMDM的自适应光学系统提供了算法支持。     

An interference effect in the channel radiative neutron capture process

This study shows that the small thermal neutron radiative capture cross sections in ¹²C and neighbouring nuclides are the result of destructive interference between the potential scattering wave and the resonance scattering wave near the nuclear surface, resulting in a drastic cancellation in the radial integral. The behaviour of the scattering wave function is examined, and the general condition for the occurrence of such cancellation is discussed. The expression for the channel radiative capture cross section which has been derived has the same structure as the Lane-Lynn formula but is expressed in terms of different parameters. In addition, this investigation shows that if the optical model well depth is adjusted so that the binding energy of the $\text{p}{}_{\mathrm{<mtext>1</mtext><mtext>2</mtext>}}$ orbit in ¹²C is kept at the experimental value, then the calculated results for the potential and channel radiative neutron capture cross sections are insensitive to the value of the nuclear radius.     

中子与116,118,120,122,124Sn反应非弹性散射的理论计算和分析

应用现有的中子与原子核Sn及其同位素反应的总截面,去弹性散射截面,弹性散射截面和弹性散射角分布的实验数据,获得一组普适的中子与Sn及其同位素反应的光学模型势参数.利用这组光学模型势参数,扭曲波玻恩近似理论,核反应Hauser-Feshbach理论和预平衡反应的激子模型,计算和分析了中子与^{116,118,120,122,124}Sn反应分离能级的非弹性散射截面和角分布.理论计算与实验数据进行了分析比较.     

Tunable double-beam optical bistability in an asymmetric double quantum-well system

We have proposed a scheme for double-beam optical bistability in a tunnel-coupled asymmetric double quantum-well driven by two optical fields circulating inside two independently unidirectional ring cavities. In contrast to the single-cavity case where single-photon saturated absorption and self Kerr-nonlinearity are dominant, the two-photon absorption and cross phase modulation can be enhanced via tunneling induced interference and have an important influence to the formation of bistability. The bistable behavior can be controlled effectively via the system parameters such as the input and detuning of control field, the detuning of the probe field, Fano interference strength and cooperation parameter. Furthermore, the proposed scheme has the ability to manipulate the outputs of two optical cavities simultaneously. Due to the flexible design of semiconductor quantum well, our scheme is more practical than atomic system, therefore it can be utilized to achieve dual all-optical switching which has application in optical communication and computing.     

中子与52Cr反应截面的理论分析

根据中子与天然核Cr及其同位素反应的总截面,去弹性散射截面和弹性散射角分布的实验数据,获得了入射中子能量从1MeV—250MeV的一组普适中子与Cr及其同位素反应的光学模型势参数.应用光学模型,扭曲波玻恩近似理论,宽度涨落修正的Hauser-Feshbach理论,和预平衡反应的激子模型,计算和分析了中子与⁵²Cr反应的所有截面、角分布、能谱和双微分截面.理论计算与实验数据进行了分析比较.     

Unmanned air vehicle flow separation control using dielectric barrier discharge plasma at high wind speed

The present paper described an experimental investigation of separation control of an Unmanned Aerial Vehicle(UAV)at high wind speeds.The plasma actuator was based on Dielectric Barrier Discharge(DBD)and operated in a steady manner.The flow over a wing of UAV was performed with smoke flow visualization in theΦ0.75 m low speed wind tunnel to reveal the flow structure over the wing so that the locations of plasma actuators could be optimized.A full model of the UAV was experimentally investigated in theΦ3.2 m low speed wind tunnel using a six-component internal strain gauge balance.The effects of the key parameters,including the locations of the plasma actuators,the applied voltage amplitude and the operating frequency,were obtained.The whole test model was made of aluminium and acted as a cathode of the actuator.The results showed that the plasma acting on the surface of UAV could obviously suppress the boundary layer separation and reduce the model vibration at the high wind speeds.It was found that the maximum lift coefficient of the UAV was increased by 2.5%and the lift/drag ratio was increased by about 80%at the wind speed of 100 m/s.The control mechanism of the plasma actuator at the test configuration was also analyzed.