基于PVDF和PTFE摩擦电机制的自供电温度传感

针对温度监测外部电源限制寻找一种柔性自供电、响应时间快、具有长期循环稳定性的温度传感器件具有重要的实际应用价值.介绍了一种基于摩擦机制的接触分离式自供电温度传感器制备方法.利用聚偏氟乙烯(PVDF)的热释电性增强摩擦层接触表面的电荷密度, PVDF表面Ag电极被用作底部电极层和摩擦层.聚四氟乙烯(PTFE)作为顶部摩擦层其与顶部电极导电铜箔相连接.将中空结构的间隔层(Kapton)置于PTFE膜和Ag电极之间形成空腔结构;研究结果表明,在295～335 K温度范围内,传感器输出电压随温度增加呈线性增加,并且其温度响应时间大约为0.1 s,灵敏度为0.25 V/K, 5 500次周期性接触分离循环仍具有优异的稳定性.该摩擦发电机在安全监测,自供电温度传感方面具有潜在应用价值.     

热浸镀铝工艺及镀层分析

在实验室条件下通过多次实验研究了采用熔剂法进行纯铁表面热浸镀铝的工艺及低真空处理方法，摸索出较为合理的工艺流程及筛选出合适的助镀剂和镀铝液表面熔剂，并简要分析了原因．对影响镀层的几个工艺参数，如浸镀时间、温度等进行分析讨论，利用扫描电镜对其镀层进行成分和结构分析．同时，对经过低真空处理的试样和没有处理的试样做了成分对比分析．     

MgO（111）弛豫表面氢的吸附问题研究

针对氢在MgO(111)表面的吸附问题,结合基于密度泛函理论的第一性原理方法,对氢在MgO(111)表面的势能面和4种可能吸附位置及2种不同吸附方式的能量进行了计算,并对吸附H原子过程中的电荷转移情况进行了研究.研究表明,H2分子在MgO(111)表面垂直吸附时均为物理吸附,最优吸附位置为fcc,而平行吸附时均为化学吸附;H原子在Mgo(111)表面的hcp和on-top吸附位置处的吸附能相差不超过0.1 eV;电荷密度计算观察到吸附H原子后,与H原子最近邻的Mg原子表面发生了电荷转移.     

循环赛图Kv(I)与完备匹配Mi的算法

给出了边矩阵和循环赛图的定义.为K2n 1的2n 1个对集的划分,提出了完全图K2n 1或边矩阵K′2n 1的△(G) 1-边着色法和平行线法.为K2n的2n个完备匹配的划分,提出了顶点序号的排序法.介绍了循环赛图的构造过程.讨论了循环赛图及完备匹配的计数问题.     

宽波束双基地高频雷达海杂波谱特性研究

双基地角在杂波单元内的连续变化导致宽波束双基地高频雷达的海杂波谱不同于窄波束.为了揭示这种差异,在G ill和W alsh窄波束双基地海面雷达散射截面积(RCS)基础上,提出了宽波束双基地海面RCS模型;结合高频地波雷达方程,得到宽波束双基地海杂波功率谱密度模型,通过仿真计算得到海杂波谱的具体形态.理论分析和仿真结果表明,在发射机附近以及基线附近的雷达探测区域,宽波束海杂波谱具有明显的展宽效应.     

换相期间无刷直流电机转矩脉动的抑制策略

无刷直流电机的转矩脉动是影响其性能的重要因素.针对换相期间的转矩脉动进行了分析,重点研究了非理想反电势、关断相和开通相相电流变化速率不等这两个因素引起的转矩脉动,为了抑制这两个因素引起的转矩脉动,提出了分段控制的策略.该策略集成了转矩直接控制和重叠换相法的优点,可以有效抑制由非理想反电势、关断相和开通相相电流变化速率不等引起的转矩脉动.通过仿真分析验证了该方法和其中两种方法单独应用时的差异,证明了分段控制策略在换相期间抑制转矩脉动的有效性.     

非换相期间无刷直流电机转矩脉动分析与抑制

无刷直流电机的转矩脉动是影响其性能的重要因素。该文针对非换相期间的转矩脉动进行了分析,重点研究了PWM_ON调制方式时的转矩脉动。PWM信号为"OFF"时续流引起的转矩脉动占主要部分,非导通相续流在一定程度上可以补偿PWM关断时造成的转矩脉动。同时,提出使用滞环电流控制方法,采用该方法可以抑制非换相期间转矩脉动。通过仿真分析和实验验证了该方法和传统方法的差异,证明了该方法在非换相期间抑制转矩脉动的有效性。     

Control and state observation of periodic linear multimodal systems

This paper investigates the control and state observation problem for periodic linear controllable and observable multimodal systems. For a controllable periodic linear multimodal system, this paper proposes an alternative minimum-norm dynamic state feedback control scheme for state transition matrix assignment. Also presented is a new design of state observers for an observable periodic linear multimodal system. Finally, an analysis of closed-loop behaviour of controlled periodic linear multimodal systems using a state-estimate is given     

Aiming point guidance law for air-to-air missiles

A new aiming point guidance (APG) law is presented which generates a missile turn rate command proportional to the heading error, that is defined as the angle between the current missile heading and predicted aiming point. The target under consideration is assumed to be manoeuvring with constant longitudinal and/or lateral accelerations, and the missile dynamics are modelled as an acceleration-limited first-order lag point mass. The aiming point is calculated based on current intercept geometry and target velocity and position. Time-to-go, a key factor for successful interception, is estimated by a time-to-go predictor. With the heading error defined as stated above, the guidance law can guide the missile into the collision course in the early stage of the engagement. As a consequence, the later part of the missile trajectory tends to be a straight line, provided that the target maintains its current status. The performance of the proposed APG is evaluated by simulation and is compared with the proportional navigation guidance (PNG) and Kim's prediction guidance (PRG) law (Kim 1985). Numerical simulations show that APG is superior to PNG and PRG in both intercept time and miss distance     

Minimum energy control of time delay systems via piecewise linear polynomial functions

The piecewise linear polynomial function approach to the minimum energy control of linear systems with time delay, is presented in this paper. The concepts of a delay shift matrix and an operational matrix for integration are employed in solving the related state and costate equations containing terms with advanced and delayed arguments. An attractive feature of the present method is its ultimate simplicity and convenience. The differential equations with delay and advance terms are converted into a set of linear algebraic equations using a recurrence algorithm. An example demonstrates the accuracy of the method.