Electrically controllable spin filtering in zigzag phosphorene nanoribbon based normal–antiferromagnet–normal junctions

We investigated the electric controllable spin-filtering effect in a zigzag phosphorene nanoribbon(ZPNR) based normal–antiferromagnet–normal junction. Two ferromagnets are closely coupled to the edges of the nanoribbon and form the edge-to-edge antiferromagnetism. Under an in-plane electric field, the two degenerate edge bands of the edge-to-edge antiferromagnet split into four spin-polarized sub-bands and a 100% spin-polarized current can be easily induced with the maximal conductance 2e~2/h. The spin polarization changes with the strength of the electric field and the exchange field,and changes sign at opposite electric fields. The spin-polarized current switches from one edge to the other by reversing the direction of the electric field. The edge current can also be controlled spatially by changing the electric potential of the scattering region. The manipulation of edge current is useful in spin-transfer-torque magnetic random-access memory and provides a practical way to develop controllable spintronic devices.

Dynamics and de-spin control of massive target by single tethered space tug

This paper investigates the dynamics and de-spin control of a massive target by a single tethered space tug in the post-capture phase. The dynamic model of the tethered system is derived and simplified to a dimensionless form. Further, a decoupled PD controller is proposed, and the local stability of the controller is analyzed by linearization technique. Parametric studies of the dynamics and de-spin control of a massive target are conducted to characterize the dynamic process of de-spin with the proposed control law. It is shown that the massive target can be de-span by a single and small space tug with limited thrust within finite time. The thrust tangent with the tether de-spins the target while the thrust normal to the tether prevents the tether from winding up the target. The tether length has a positive contribution to the de-spin of a target. The longer tether leads to a faster de-spin process.

Influence of control strategy on stability of dual-spin projectiles with fixed canards

Existing literature has shown that the control force at the nose could cause dynamic instability for controlled projectiles. To lower the adverse impact on the dual-spin projectile with fixed canards under the premise of meeting guidance system requirements, the influence of control moment provided by a motor on the flight stability is analyzed in this paper. Firstly, the effect of the rolling movement on stability is analyzed based on the stability criterion derived using the Hurwitz stability theory. Secondly, the evaluation parameters combining the features of different control periods that could assess the variation of stability features after the motor torque are obtained. These effective formulas are used to indicate that, to reduce the flight instability risks, the stabilized rolling speed of roll speed keeping period should be as small as possible; the variation trend of motor torque during the rolling speed controlling period and the roll angle of the forward body during roll angle switching period are recommended corresponding to the projectile and trajectory characteristics. Moreover,detailed numerical simulations of 155 mm dual-spin projectile are satisfactory agreement with the theoretical results.

Quasi non-Markovian Approach to the Study of Decoherence of a Controlled-Not Quantum Gate in a Chain of Few Nuclear Spins Quantum Computer

We develop in the weak coupling approximation a quasi-non-Markovian master equation and study the phenomenon of decoherence during the operation of a controlled-not (CNOT) quantum gate in a quantum computer model formed by a linear chain of three nuclear spins system with second neighbor Ising interaction between them. We compare with the behavior of the Markovian counterpart for temperature different from zero (thermalization) and at zero temperature for low and high dissipation rates. At low dissipation there is a very small difference between Markovian and quasi no-Markovian at any temperature which is unlikely to be measured, and at high dissipation there is a difference which is likely to be measured at any temperature.

Rolling Control Characteristic Experimental Investigation of a Canard Missile with Free-Spinning Tail

To study the rolling control characteristics of a canard-controlled missile, a series of wind tunnel experiment is conducted. The experimental method, the structure features of wind tunnel model and the experimental results are introduced in this paper. The experimental data show that the canard is an inefficient rolling control device for canard-controlled missile with fixed tail fins; but for the free-spinning tail fin configuration, the canard can conduct rolling control of the missile, and even have higher controlling efficiency under larger canard deflection angle.

Controlling spins in silicon quantum dots

Spins in silicon(Si)quantum dots(QDs),as a new type of solid state qubits,is expected to be a competitive contender in the long run of scalable quantum computation[1].Quantum computation is believed to be the next-generation computing technology to solve the problems that no classical computer can feasibly tackle.In the last decade.

Spin-controlled directional launching of surface plasmons at the subwavelength scale

In this paper, we demonstrate a spin-controlled directional launching of surface plasmons at the subwavelength scale.Based on the principle of optical spin＇s effect for the geometric phase of light, the nanostructures were designed. The inclination of the structures decides the spin-related geometric phase and their relative positions decide the distance-related phase. Hence, the propagation direction of the generated surface plasmon polaritons（SPPs） can be controlled by the spin of photons. Numerical simulations by the finite difference time domain（FDTD） method have verified our theoretical prediction. Our structure is fabricated on the Au film by using a focused ion beam etching technique. The total size of the surface plasmon polariton（SPP） launcher is 320 nm by 180 nm. The observation of the SPP launching by using scanning near-field optical microscopy is in agreement with our theory and simulations. This result may provide a new way of spin-controlled directional launching of SPP.

STUDY ON THE RING SPINNING SYSTEM WITH A FIXED BELL SHAPED BALLOON CONTROLLER

On the basis of analyzing the typical kinds of balloon controllers used now, this article provides a new type one named Fixed Bell Shaped Balloon Controller. Experiments have been made to verify the function of it. Results indicated that the facility has quite good effect on the improvement of yarn quality and properties in addition to controlling yarn tension.

Investigation on the flow control of micro-vanes on a supersonic spinning projectile

Studies have shown that micro-wedge vortex generators(MVG)can effectively control the flow separation of supersonic boundary layer.In order to improve the flight stability of spinning projectile,the original standard 155 mm projectile was taken as an example,and the micro-vanes were mounted at the projectile shoulder to investigate the separation control on the aerodynamic characteristics of projectile.Numerical simulations were performed with the use of DES method for the flow fields of projectiles with and without micro-vanes,and the characteristics of the boundary layer structures and aerodynamic data were compared and discussed.Numerical results show that the micro-vanes can be used to inhibit separation of fluid on projectile surface,and improve the flight stability and firing dispersion of projectile.

Method of Time-Delay Calculating and Correcting to Control Spin-Stabilized Satellite Synchronously

The key to control Spin-Stabilized Satellites Synchronously is to determine the models for calculating and correcting of time-delay at the different situations. Based on the principle of Synchronous-Control mode, the methods of determining the models of calculating and correcting of time-delay are proposed. The methods have been proved to be effective in real satellite control engineering.

Second order sliding mode control with back stepping approach for moving mass spinning missiles

An attitude controller using the second order sliding mode control methodology with a backstepping approach（SOSMCB）is designed and implemented for a spinning missile with two internal moving mass blocks.The system consists of a rigid body and two radial internal moving mass blocks and its mathematical model is established based on Newtonian mechanics.The control scheme integrates a second order sliding mode control algorithm into the last step of the backstepping approach,and its stability is proved by means of a Lyapunov function.The performance of the controller is demonstrated by numerical simulations,the results show that the attitude controller is stable and effective.

Voltage control of ferromagnetic resonance and spin waves

The voltage control of magnetism has attracted intensive attention owing to the abundant physical phenomena associated with magnetoelectric coupling. More importantly, the techniques to electrically manipulate spin dynamics, such as magnetic anisotropy and ferromagnetic resonance, are of great significance because of their potential applications in high-density memory devices, microwave signal processors, and magnetic sensors. Recently, voltage control of spin waves has also been demonstrated in several multiferroic heterostructures. This development provides new platforms for energyefficient, tunable magnonic devices. In this review, we focus on the most recent advances in voltage control of ferromagnetic resonance and spin waves in magnetoelectric materials and discuss the physical mechanisms and prospects for practical device applications.

New-type of flying control for spinning TVC vehicle

A new kind of problem for TVC vehicle spinning in the boost stage had been researched. The study of non-linear flying dynamics modeling and dynamic properties of TVC vehicles reveal dominant coupled factors that affect the attitude stability and attitude precision of the pitch channel and yaw channel. The paper emphasizes the inertial delay coupled effects between vehicle＇s pitch servo system and yaw servo system, which have always been neglected. An uncoupled plan and control algorithm are put forward from the standpoint of engineering implementation to provide theoretical guidance and reference for further research on this complicated flying control.

Robust Graded Sliding Mode Tracking Control for Low Speed Spinning Ballistic Missiles

The nonlinear dynamic model of spinning ballistic missiles is established during the first boosting phase of the missile. Based on the conventional backstepping sliding mode control and the assumption of a two time-scale separation of missile dynamics, a graded sliding mode controller is designed with two sub-sliding surfaces which have invariability to external disturbances and parameter perturbations, and a matrix which comprises three first order low pass filters is introduced to prevent “explosion of terms”. Owing to the upper bounds of the uncertainties are difficult to obtain in advance, adaptive laws are introduced to estimate the values of the uncertainties in real-time. Eventually, the numerical simulation results given to show the proposed controller can ensure the steady flight of missiles.

Research on A Master - slave Multi - microcomputers Control System for Hollow Spindle Fancy Yarn Spinning Machine

In this paper, a successfully studied and developed master - slave muld - microcomputers control system based on PC - BUS for hollow spindle fancy yarn spinning machine, mainly Its overall scheme, software and hardware construction, is introduced. Spinning experiments show that the system achieves satisfactory result. This system can solve the diftkultles of mechatronical fusion between domestic hollow splndk fancy yarn spuming muchine and its microcomputer control technology.

基于小型化原子磁力计的零场NMR波谱仪搭建与测试

常规高场NMR波谱仪依托超导技术,其体积大、维护成本高,且存在样本磁化率不均匀导致的谱线展宽现象,零场或近零场NMR技术则可实现有效互补.本文自主搭建了一套基于小型原子磁力计的可移动零场NMR波谱仪,采用以多功能采集卡(National Instruments PCIe-6353)为核心的集成控制系统,仪器主磁场强度小于1nT,可实现高分辨率的J-耦合谱采集.为实现对自旋体系的有效操控,利用样品绝热初态的单脉冲激发实现对三轴脉冲线圈的精确标定.在此基础上,使用改进的组合脉冲序列实现了在^(13)C-^(1)H异核体系下的单自旋选择性操控,验证了零场NMR波谱仪的有效性.

基于CMOS有源超材料的生物分子的自旋太赫兹传感

基于互补金属氧化物半导体(CMOS)有源超材料,通过结合自旋太赫兹源,对生物分子的太赫兹频段指纹谱进行传感检测。对比基于自旋太赫兹源和基于光电导天线的太赫兹时域光谱系统测量的3种不同生物样品的指纹谱特征峰,验证了自旋太赫兹源测量生物样品的可行性。同时,提出一种基于CMOS有源超材料的生物分子太赫兹传感方案,仿真结果表明CMOS调控器件对生物样品的扫描测试表现为生物透射峰与器件谐振峰变化统一。当吸收峰位于器件的调控范围内时,随着加电压的增大,生物透射谱谐振频率减小,出现红移,最大红移量达到40 GHz。因为不同的生物样品有不同的吸收峰,根据不同的太赫兹指纹谱吸收峰的位置设计了5种对应中心频率的CMOS有源超材料,为实现生物分子太赫兹传感系统的小型化和集成化提供了理论及实验基础。

鸭舵式双旋弹舵翼非线性控制力建模与分析

鸭舵式双旋弹通过调节前体滚转角方位进行弹道修正,建立准确的舵翼控制力模型是深入研究其弹道特性和进行弹道设计的关键。综合考虑弹体和各片舵翼之间的干扰作用,在非滚转系中利用傅里叶级数对前体纵向对称面相对复攻角平面方位改变产生的周期性效应进行变换,建立适用于该类炮弹大攻角飞行的精确舵翼控制力工程计算模型,从原理上显示其与四片舵翼结构参数、复攻角幅值和相位以及前体滚转角方位间的关系。通过计算流体力学数值方法对不同前体滚转角和复攻角下的舵翼控制力进行仿真分析。研究结果表明:受一对减旋舵和操纵舵的法向力共同影响,舵翼控制力的大小和方向变化均呈现出强非线性特征,在大攻角条件下尤其突出;在任意复攻角和前体滚转角情况下,所建模型能够准确描述鸭舵式双旋弹的舵翼控制力及各因素对它的影响,为该类炮弹的前体结构设计、弹道特性分析和弹道设计等提供了理论依据与参考。

纺纱空调系统运行仿真及机器学习辅助调控

针对纺纱车间采用传统的PID控制车间温湿度不稳定问题,采用机器学习的BP神经网络对后台历史数据进行监督学习,并建立空调设备自控参数的专家库。当PID调控产生温湿度较大波动时采用信息库建立好的空调控制参数直接介入辅助控制。基于热量平衡、湿量平衡以及风量平衡开发了纺纱空调仿真系统,并分析了风机、水泵、二回风窗、新风窗对于车间温湿度控制的影响。为验证辅助调控的效果,将BP神经网络预测的空调控制参数介入车间温湿度控制,并与传统PID控制车间的温湿度进行了对比。结果表明:采用BP神经网络辅助调控空调系统的参数,车间温湿度稳定性优于传统PID控制。认为:机器学习辅助调控纺纱空调系统可达到稳定控制温湿度的目的。

基于模糊PID的旋压机进给系统动态仿真

为了改善铝杆旋压机进给系统的控制性能,在分析进给系统中两路伺服油缸在不同工况下的运动特点后,提出电液伺服系统位移协同控制策略。首先阐述了旋压机进给系统运动过程及技术指标,并对液压进给控制系统进行设计与研究;其次根据交叉耦合控制理论,建立了AMEsim和Simulink的联合仿真模型。最后,基于模糊PID设计了双缸闭环位置协同控制结构,完成了两路油缸的位置协同控制,保证了协同误差在精度范围内。联合仿真曲线对比结果表明,基于模糊PID的控制系统的协同精度远高于传统PID控制,有较好的控制性能。