Observer‐based compensation control of servo systems with backlash

For compensating backlash phenomenon in servo systems, the authors propose an observer method in this paper to estimate both system states and vibration torque before controller design. First, a systematic scheme is given to obtain plant parameters, which is very important in observing system states. This is a parameter estimation principle that gives a crude estimation and computes the differences between the crude and true values. As a result, the precise value of the parameters is obtained by adding together the crude value and the difference. Then, based on the precise estimated parameters, an extended state observer (ESO) is designed to obtain feedback and feedforward signals. Consequently, robust compensation control is achieved by designing an output feedback controller, consisting of a feedback term and a feedforward term. Finally, in order to validate the proposed approach, extensive experiments are performed on a practical servo system with backlash nonlinearity.     

基于稳健设计的SGNS算法的超参数调优方法

通常给定超参数的若干取值选取性能最大的为最优组合(称为直接选优法),但是此方法的稳健性差。为此,提出了一种基于稳健设计的超参数调优方法(称为稳健调优法)。具体地,以SGNS算法中的超参数调优为例,在词语推断任务上实验并得出:经方差分析得到SGNS算法中的七个超参数中的五个对算法预测性能有显著影响,确定为主控因子,其余两个确定为噪声因子,且主控因子中有三个对性能估计的方差有显著影响,因此,调优中仅从期望最大来直接选优是不合理的;稳健调优法与直接选优法两者在预测性能上没有显著差异,但稳健调优法对噪声因子具有较好的稳健性。稳健调优法对一般的深度神经网络的调参有实际的借鉴意义。     

基于改进等效电流量测变换的状态估计算法

介绍了基于等效电流量测变换的状态估计算法,并在此基础上提出了一种改进算法.应用抗差估计的理论构造了一组权函数,在每次迭代的过程中对权重不断修改,从而达到提高估计精度的目的.Matlab仿真实验结果表明,估计精度得到了提高.     

Robust Near-Hovering Flight Controller for Model-Scale Helicopters Via Parametric Approach

This paper aims to provide a parametric design for robust flight controller of the model-scale helicopter. The main contributions lie in two aspects. Firstly, under near-hovering condition, a procedure is presented for simplification of the highly nonlinear and under-actuated model of the model-scale helicopter. This nonlinear system is linearized around the trim values of the chosen flight mode, followed by decomposing this high-order linear model into three lower-order subsystems according to the coupling properties among channels. After decomposition, the three subsystems are obtained which include the coupling subsystem between the roll (pitch) motion and the lateral (longitudinal) motion, the subsystem of the yaw motion and the subsystem of the vertical motion. Secondly, by using eigenstructure assignment, the problem of flight controller design can be converted into solving two optimization problems and the linear robust controllers of these subsystems are designed through solving these optimization problems. Besides, this paper contrasts and analyzed the performances of the LQR controller and the parametric controller. The results demonstrate the effectiveness and the robustness against the parametric perturbations of the parametric controller.     

改进的粒子群优化算法下的MIMO雷达稳健波束形成

在进行阵列自适应波束形成时,由于阵元导向矢量失配现象的存在,严重影响了常规最优波束形成的性能。考虑阵元的导向矢量误差,运用改进的粒子群优化算法对阵元的导向矢量进行纠正,使其误差达到最小,得到了一种适用于多输入多输出雷达的新的稳健波束形成方法。与现有的应用于MIMO雷达的稳健波束形成方法相比,在导向矢量误差较大或者误差随机变化的情况下新方法具有更高的输出信号干噪比,且其性能一直保持了较高的稳定性。数值仿真结果验证了新方法相比已有算法具有更好的鲁棒性和更高的输出性能。     

改进型特征权重自调节K-均值聚类算法

针对特征权重自调节K-均值聚类(FWSA-KM)算法对噪声敏感的问题,提出一种改进型特征权重自调节K-均值聚类(IFWSA-KM)算法。用一种非欧氏距离代替FWSA-KM算法中的欧氏距离,以增加聚类算法的抗噪声性能。通过用人工数据和真实数据的对比性实验,可验证IFWSA-KM算法的有效性。     

具有多重状态时滞与控制时滞的广义系统非脆弱保代价控制

针对一类不确定多时滞广义系统,该多时滞广义系统同时具有状态和控制时滞。假设不确定范数是有界的,且系统的状态是完全可测的,通过引进二次稳定性的概念,结合线性矩阵不等式的设计方法,给出了鲁棒非脆弱保代价控制的充分条件。通过对线性矩阵不等式的求解,可得非脆弱状态反馈鲁棒保代价控制器。该控制器对所有容许的不确定性,能保证闭环广义系统的稳定性,而且也能满足二次型代价函数的上界。最后,通过算例仿真表明所提出结论的可行性和有效性。     

基于代理模型的板料成形优化技术进展

综述了板料成形优化技术现状,针对优化中计算成本高的问题,提出了基于代理模型的优化技术,包括可立格模型、响应面模型、神经网络模型等。从实验设计、代理模型的建立,以及优化求解等方面进行了阐述。针对产品设计中因素的随机性和不确定性,为减小目标函数对设计变量的敏感性,将稳健设计理论应用于板料成形优化中,以提高产品的可靠性和稳健性。     

Global robust output tracking control for a class of cascade nonlinear systems with unknown control directions

We investigate the global robust tracking problem via output feedback for a class of cascade nonlinear systems with dynamic uncertainties and non-vanishing disturbances. It does not require a priori knowledge of the sign of the high-frequency gain. A recursive design scheme is presented using the ideas of pseudosign function, Nussbaum-type gain technique and the deadzone method. It is shown that under some conditions, the tracking error can be guaranteed asymptotic to the interval [?ε, ε]?? with arbitrary prescribed ε>0 after a finite time, while keeping all signals of the resulting closed-loop systems bounded. The simulation results demonstrate the effectiveness of the proposed algorithm.     

磁悬浮直线电动机H∞鲁棒控制器及其蚁群算法优化设计

磁悬浮永磁直线电动机在结构上取消了机械传动的中间环节,具有磁悬浮和直接驱动的特点.针对磁悬浮永磁直线电动机由于悬浮高度不同,在磁悬浮和直接驱动运行过程中存在自身参数摄动和外界干扰突出的问题,设计基于蚁群算法的H_∞鲁棒控制器,以保证系统对这些不确定性具有良好的鲁棒性.建立包含磁悬浮永磁直线电动机参数摄动和外界干扰的状态空间模型.推导出无须满足正则条件约束的Riccati不等式,给出H_∞鲁棒控制器的解析表达式.针对H_∞控制器中加权矩阵选择的困难,采用蚁群算法对加权矩阵进行寻优.最后在MATLAB环境下对控制系统进行仿真研究.仿真实验表明基于蚁群算法的磁悬浮永磁直线电动机控制系统的性能比优化前有较明显改善,说明该方法的可行性和有效性.