分数阶终端滑模控制器在DTC系统中的应用

针对SVPWM调制的永磁同步电机直接转矩控制系统磁链和转矩波动较大的问题,结合非奇异终端滑模和分数阶微积分理论的特点,设计了一种分数阶非奇异终端滑模控制器。结合直接转矩原理和分数阶微积分理论,对误差进行分数阶微分后与误差之和作为滑模面;根据非奇异终端滑模控制原理,在所设计分数阶滑模面的基础上确定了相应的控制律;利用李亚普诺夫定理证明了滑模面的稳定性和可达性。仿真结果表明,该策略能提高系统的动静态性能,可以进一步抑制磁链和转矩波动。     

BTT导弹状态反馈H_∞控制自动驾驶仪设计

针对倾斜转弯(BTT)导弹自动驾驶仪的抗干扰性和鲁棒性问题,以考虑耦合的情况下建立的更接近于实际的导弹数学模型为基础,将通道间的耦合作为干扰,在弹道特征点上对导弹模型进行解耦和线性化,得到各个通道的数学模型;设计基于线性矩阵不等式(LMI)的状态反馈H_∞控制自动驾驶仪,搭建全耦合状态下的三通道仿真模型,并进行联合仿真研究。结果表明所设计的状态反馈H_∞控制自动驾驶仪能够实现对导弹制导指令的有效跟踪,满足BTT导弹控制的要求。     

基于FrFT的差分跳频通信LFM干扰抑制算法

针对差分跳频通信系统抗LFM干扰能力不足的问题,利用差分跳频信号和LFM干扰信号调频斜率参数的不同,通过估计采样信号中LFM干扰信号的调频斜率K和旋转阶次α参数,结合分段、参数估计和均值处理提高估计精度,进一步在采样信号的分数阶时频域二维参数平面(α,μ)中利用LFM干扰信号频带外的平面均值替代LFM信号成分,实现对差分跳频通信中LFM干扰信号的抑制。仿真结果表明,该算法可有效抑制差分跳频信号中LFM干扰信号,提高信噪比约11 d B。     

Interception probability simulation and analysis of salvo of two electromagnetic coil launched anti-torpedo torpedoes

Electromagnetic coil launch is an important branch of electromagnetic launch (EML) technology, which is suitable for launching anti-torpedo torpedo (ATT). This paper focuses on the EML parameters and the interception probability of the EML two ATTs salvo. Based on the launching model of a multi-stage coil launcher, the trajectory model of the ATT and the attacking torpedo, a calculation method for the EML two ATTs salvo parameters is proposed, with the conditions of capture and interception given reasonably. An adaptive particle swarm optimization (APSO) algorithm is proposed to calculate the optimal launching parameters, by designing the adaptive inertia weight and time-varying study factors. According to the analysis of the simulation with Monte Carlo method, EML will improve the interception probability effectively, and the interception probability is affected by the launching range. The results demonstrate good performance of the proposed APSO in calculating EML parameters for the two ATTs salvo in certain combat situation. Implications of these results are particular regarding the command and decision in the anti-torpedo combat.     

测试点的选取问题

在故障检测的过程中 ,每个测试点检测需要的时间可能不同。本文研究了如何选取一些测试点 ,使得这些测试点可以检测所有故障 ,而所需时间最少的问题。我们将其转化成整数规划问题 ,并给出一个求解算法 .最后给出一个实例对算法加以说明。     

高压强流脉冲变压器

在脉冲功率调制系统研究中 ,其核心技术之一是脉冲变压器的研制。本文描述了脉冲变压器的技术要求和结构参数设计 ,并给出了实验测试结果 :变压器的初级电感为 3 6μH ,耦合系数为 0 77。当初级输入电压为 60kV时 ,次级输出电压可达到 50 0kV。     

Applying Lanchester's linear law to model the Ardennes campaign

In modern warfare, many believe the decisive factor in winning a battle is seizing the right moment to shift from defense to attack, or vice versa. This paper attempts to bring that perspective to Lanchester's differential equations of warfare, and continues the application of Lanchester's linear law to the analysis of the World War II battle of Ardennes, as reported in earlier issues of Naval Research Logistics by Bracken and by Fricker. A new variable, shift time, accounting for the timing of the shift between defense and attack is explicitly included in our version of the model, and it helps obtain improved goodness of fit to historical data. © 2001 John Wiley & Sons, Inc. Naval Research Logistics 48:653–661, 2001     

Extending the MAD portfolio optimization model to incorporate downside risk aversion

A mathematical model of portfolio optimization is usually represented as a bicriteria optimization problem where a reasonable tradeoff between expected rate of return and risk is sought. In a classical Markowitz model, the risk is measured by a variance, thus resulting in a quadratic programming model. As an alternative, the MAD model was developed by Konno and Yamazaki, where risk is measured by (mean) absolute deviation instead of a variance. The MAD model is computationally attractive, since it is easily transformed into a linear programming problem. An extension to the MAD model proposed in this paper allows us to measure risk using downside deviations, with the ability to penalize larger downside deviations. Hence, it provides for better modeling of risk averse preferences. The resulting m‐MAD model generates efficient solutions with respect to second degree stochastic dominance, while at the same time preserving the simplicity and linearity of the original MAD model. © 2001 John Wiley & Sons, Inc. Naval Research Logistics 48: 185–200, 2001     

多次点火固体火箭发动机在面空导弹上的应用研究

论述了多次点火固体火箭发动机的多次点火的最佳控制,具体研究了两次点火固体火箭发动机的参数对飞行性能的影响,对两次点火固体火箭发动机结合弹道同时最佳化问题给出了仿真结果.     

多相永磁同步电动机的矢量控制及仿真

建立了多相永磁同步电动机定子静止坐标系以及d、q旋转坐标下的数学模型 ,对多相永磁同步电动机的矢量控制系统进行了一般性分析 .针对表面式永磁电动机提出了一种简单高效的转子磁场定向控制方法 .采用Simulink/PSB对系统进行了动态仿真研究