不同维分数阶混沌预设时间有限时间投影同步

对于不同维分数阶混沌系统的投影同步问题,设计了一种自适应滑模控制器。这使得带有内部不确定量和外部扰动的驱动,响应系统能够在任意预设的时间完成同步,自适应律可以逼近未知量的上界。并针对自适应滑模控制器由于干扰产生抖振的问题,提出了两种解决方案。首先是设计二维滑模控制表,将模糊控制方法加入滑模控制器组成模糊自适应滑模控制器...     

基于非线性干扰观测器的高超声速飞行器滑模反演控制

针对高超声速飞行器非线性、强耦合和参数不确定弹性体模型,提出了一种基于非线性干扰观测器的滑模反演控制方法.将飞行器曲线拟合模型分解为速度子系统和高度相关子系统并表示为严格反馈形式,分别采用滑模和反演方法设计实际控制量与虚拟控制量.采用1阶低通滤波器获取虚拟控制量的导数,解决了传统反演控制方法"微分项膨胀"问题.基于改进滑模微分器设计了一种新型非线性干扰观测器,以此对模型不确定项进行估计和补偿.仿真结果表明,该控制器对模型不确定性和气动弹性影响具有鲁棒性,且实现了对速度和高度参考输入的稳定跟踪.     

基于自适应模糊滑模控制的分数阶混沌系统的投影同步

基于模糊控制理论和滑模控制理论以及自适应控制理论,研究了一类含有外部扰动的不确定分数阶混沌系统的混合投影同步问题.提出了一种自适应模糊滑模控制的分数阶混沌系统投影同步方法.模糊逻辑系统用来逼近未知的非线性函数和外部扰动,并且对逼近误差采用了自适应控制,同时构造了一种具有较强鲁棒性的分数阶积分滑模面.应用分数阶Barbalat引理设计了自适应模糊滑模控制器和参数自适应律.最后数值仿真结果验证了所提控制方法的有效性.     

具有非线性不确定参数的电液伺服系统自适应backstepping控制

针对电液伺服系统中存在非线性不确定参数的问题,提出了一种采用积分型Lyapunov函数的自适应backstepping控制方法.首先定义积分型Lyapunov函数,将电液伺服系统中的非线性不确定参数转化为线性表示;然后逐步递推设计backstepping控制器,同时在控制律中加入阻尼项,从而补偿外界干扰对控制性能的影响;基于Lyapunov稳定性方法,设计了参数自适应律,并且在自适应律中引入充分光滑投影算子,实现对电液伺服系统中不确定参数漂移的抑制作用.搭建了AMESim与MATLAB的联合仿真平台,对所设计的自适应backstepping控制器进行仿真,作为对比,设计了不带有非线性参数估计的自适应backstepping控制器和PID算法.仿真表明,本文所设计的控制器具有良好的跟踪性能和补偿非线性不确定参数变化的能力.     

基于模糊不确定观测器的四旋翼飞行器自适应动态面轨迹跟踪控制

针对具有未知外界扰动和系统不确定性的四旋翼飞行器,提出了一种基于模糊不确定观测器（Fuzzy uncertainty observer,FUO）的自适应动态面轨迹跟踪控制方法.通过将四旋翼飞行器系统分解为位置、姿态角和角速率三个动态子系统,使得各子系统虚拟控制器能够充分考虑欠驱动约束;采用一阶低通滤波器重构虚拟控制信号及其一阶导数,实现四旋翼跟踪控制设计的迭代解耦;设计了一种模糊不确定观测器,用以估计和补偿未知外界扰动与系统不确定性,从而确保闭环系统的稳定性和跟踪误差与其他系统信号的一致有界性.仿真研究验证了所提出的控制方法的有效性和优越性.     

不确定混沌系统用分数阶系统同步与参数辨识

针对不确定整数阶混沌系统的同步和参数辨识问题,提出一种新的策略即用分数阶混沌系统来同步整数阶混沌系统并实现不确定参数的辨识。首先引入预控制量并利用主动控制构造同步误差方程,然后用分数阶混沌系统稳定性理论和自适应控制理论,设计同步控制器及参数的自适应率,最终实现整数阶混沌系统用分数阶混沌系统同步和参数辨识。数值仿真实现参数不确定整数阶Lorenz系统用分数阶Lorenz系统进行同步和参数辨识仿真,结果表明提出方法的有效性。     

不同阶分数阶混沌系统的同步与参数辨识

针对不确定分数阶混沌系统的同步和参数辨识问题,提出一种新的方法,即用不同阶分数阶系统来同步和参数辨识.利用主动控制和预控制量方法,基于分数阶混沌系统稳定性理论和自适应控制理论,设计控制器,实现不同阶分数阶混沌系统之间的同步和参数辨识.理论和仿真结果实现了不同阶Chen 系统间的同步和辨识,表明了该方法的有效性.     

基于改进Oustaloup滤波器的分数阶PID控制器简化设计

针对分数阶微积分算子的直接和间接近似化方法所表现出来的形式复杂、运算量大的问题,对Oustaloup滤波器的结构进行改进,对常规分数阶PID控制器进行了简化设计,并采用自适应遗传算法对控制器的参数进行整定.选取两种代表性分数阶系统,在模型处于两种典型状态下,对简化型分数阶PID控制器、常规分数阶PID控制器和整数阶PID控制器的控制性能进行仿真实验对比.结果表明,在控制器性能基本相同的情况下,通过该方法设计的简化型分数阶PID控制器性具有结构简单,耗时量小的优点,提高了工程可实现性.     

考虑边端效应的直线感应电机投影自适应指令滤波反推控制

针对考虑边端效应的直线感应电机精确位置跟踪问题,设计一种基于间接矢量控制的投影自适应指令滤波反推控制器.首先,给出间接矢量控制下考虑边端效应的直线感应电机模型;其次,运用反推法设计控制器,同时采用限幅的指令滤波器处理反推法中计算膨胀和控制器饱和问题,并对指令滤波器产生的滤波误差设计补偿信号;然后,基于李雅普诺夫稳定性理论设计自适应律,估计直线感应电机控制系统中的不确定参数(移动物件的总质量、粘滞系数、外部的负载扰动),并引入投影算子保证估计值的有界性;最后,将所设计的控制器分别与传统PID控制器、指令滤波反推控制器对比.仿真结果表明,所设计的控制器具有更强的动态性能、抗干扰性及鲁棒性.     

自适应鲁棒控制器设计新方法在电液伺服系统中的应用

提出了一种自适应鲁棒控制器设计新方法, 并运用在阀控缸电液位置伺服系统中.首先, 将含有确定、不确定、已知、未知、线性和非线性项的电液伺服系统进行完整地数学建模, 以状态空间的形式表出.然后利用本文所提的新方法设计自适应鲁棒控制器和相应的自适应律来处理所建模型中的各项元素.该控制器通过设计一个带有虚拟控制量的控制状态空间表达式并结合状态观测器来获得.设计合适的虚拟控制量, 可在任意给定条件下, 使所有的系统状态都收敛到所设计的理想状态.接着设计李亚普诺夫函数来证明闭环系统的稳定性.最后建立硬件实验平台与经典自适应鲁棒控制方法进行对比实验验证此自适应鲁棒控制器设计新方法的有效性和优势.     

一类不确定运动系统的空间迭代学习控制

本文讨论了一类在有限空间区间内重复运行的不确定运动系统的跟踪控制问题.通过引入空间状态微分算子和空间复合能量函数,提出了一种空间周期的自适应迭代学习控制算法.首先利用空间状态微分算子,将系统从时间域转化到空间域形式.然后基于空间复合能量函数设计了控制器,利用含限幅作用的参数自适应律逼近系统中的不确定性,同时引入鲁棒项共同抑制非参数不确定性的影响.通过严格的数学分析,证明了在标准初始条件和随机有界初始误差两种情况下的跟踪误差收敛性.最后通过列车仿真进一步验证了该算法的有效性.     

A modified direct adaptive robust motion trajectory tracking controller of a pneumatic system

In this study, we developed and tested a high-precision motion trajectory tracking controller of a pneumatic cylinder driven by four costless on/off solenoid valves rather than by a proportional directional control valve. The relationship between the pulse width modulation （PWM） of a signal＇s duty cycle and control law was determined experimentally, and a mathematical model of the whole system established. Owing to unknown disturbances and unmodeled dynamics, there are considerable uncertain nonlinearities and parametric uncertainties in this pneumatic system. A modified direct adaptive robust controller （DARC） was constructed to cope with these issues. The controller employs a gradient type adaptation law based on discontinuous projection mapping to guarantee that estimated unknown model parameters stay within a known bounded region, and uses a deterministic robust control strategy to weaken the effects of unmodeled dynamics, disturbances, and parameter estimation errors. By using discontinuous projection mapping, the parameter adaptation law and the robust control law can be synthesized separately. A recursive backstepping technology is applied to account for unmatched model uncertainties. Kalman filters were designed sepa- rately to estimate the motion states and the derivative of the intermediate control law in synthesizing the deterministic robust control law. Experimental results illustrate the effectiveness of the proposed controller.     

Operator-based robust control design for a human arm-like manipulator with time-varying delay measurements

In this paper, an operator-based robust nonlinear control for a human multi-joint arm-like manipulator with time-varying delay measurements is proposed by using robust right coprime factorization approach, a delay compensation operator and a forward predictive operator. That is, first, considering the uncertainties of dynamic model consisting of measurement error and disturbances, an operator-based nonlinear feedback control scheme is designed to eliminate effect of uncertainties. Second, an operator controller based on real measured data from human multi-joint arm viscoelasticity is presented to obtain desired motion mechanism of human multi-joint arm viscoelastic properties, the unknown time-varying delay measurements are described by a delay operator, the delay compensation operator is designed to remove the effect of unknown time-varying delay measurements, and the forward predictive operator is designed to compensate the term related to effect of central nervous system (CNS) during human multi-joint arm movements. The BIBO stability can be guaranteed and the tracking performance can be realized by the designed operator controller, the delay compensation operator and the forward predictive operator. Finally, the effectiveness of the proposed design scheme is confirmed by the simulation results based on experimental data.     

Design of robust non-fragile H-infinity controller based on Delta operator theory

Considering that the controller parameters are of additive norm-bounded uncertainties when realized, a design method of robust non-fragile H-infinity controller for uncertain systems based on Delta operator theory is illustrated in this paper. A sufficient and necessary condition of the existence for the controller is given, which is presented in LMI forms. Finally, the designed method is used in the speed control system of a permanent magnet linear synchronous motor （PMLSM）. With the designed controller, the resulting speed closed-loop system is still stable and has the expected Hinfinity performance even if the sample period is reduced and the parameters of the controller and the controlled object are varied. The results show that the designed method is effective.     

Design of robust non-fragile H-infinity controller based on Delta operator theory

Considering that the controller parameters are of additive norm-bounded uncertainties when realized, a design method of robust non-fragile H-infinity controller for uncertain system based on Delta operator theory is illustrated in this paper. A sufficient and necessary condition of the existence for the controller is given, which is presented in LMI forms. Finally, the designed method is used in the speed control system of permanent magnet linear synchronous motor (PMLSM). With the designed controller, the resulted speed closed-loop system is still stable and has the expected Hinfinity performance even if the sample period is reduced and the parameters of the controller and the controlled object are of variations. The results show that the designed method is effective.     

Discrete-time robust backstepping adaptive control for nonlineartime-varying systems

This paper studies the problem of adaptive control for a class of nonlinear time-varying discrete-time systems with nonparametric uncertainties. The plant parameters considered here are not necessarily slowly time-varying in a uniform way. They are allowed to have a finite number of big jumps. By using the backstepping procedures with parameter projection update laws, a robust adaptive controller can be designed to achieve adaptive tracking of a reference signal for this class of systems. It is shown that the proposed controller can guarantee the global boundedness of the states of the whole adaptive system in the presence of parametric and nonparametric uncertainties. It can also ensure that the tracking error falls within a compact set whose size is proportional to the size of the uncertainties and disturbances. In the ideal case when there is no nonparametric uncertainties and time-varying parameters, perfect tracking can be achieved     

Adaptive control of a class of slowly time varying systems with modeling uncertainties

In a recent work, a new linear adaptive controller based on certainty-equivalence and backstepping design, which promises a level of transient and asymptotic performance comparable to that of the tuning functions adaptive backstepping controller without using high order nonlinearities, was proposed for linear time invariant systems. The proposal was supplemented with robustness and performance analysis in the presence of modeling uncertainties. In this note, the same idea is used to develop a new linear adaptive controller for slowly time varying systems with modeling uncertainties. The new adaptive control scheme guarantees robustness with respect to modeling errors via normalizing damping, parameter projection, and static normalization. Use of normalizing damping is essential in protecting the "linearity" of the system, which plays a key role in reaching the stability and robustness results.     

不确定Delta算子系统的鲁棒H∞重构控制

讨论一类含有参数不确定和执行器故障的Delta算子系统鲁棒H_∞ 重构控制设计问题. 通过利用故障检测与隔离(FDI)技术, 在考虑不可检测故障执行器输入为能量有界的干扰信号情形下, 基于H_∞ 干扰抑制的思想, 给出了系统可鲁棒H_∞ 镇定的充分条件. 所设计的控制器可使闭环系统鲁棒稳定, 而且对可允许的不确定性和执行器故障具有一定的H_∞ 性能. 数值例子说明了本文设计方法的有效性.     

存在匹配/非匹配不确定性的飞机舵面故障$L_1$容错控制

针对飞机舵面故障时产生的各种内部未建模动态、系统不确定参数、未知输入增益等问题,提出一种同时存在匹配/非匹配不确定性的多输入多输出飞机舵面故障$L_1$容错控制方法.首先,推导出等效线性参数时变模型;然后,基于投影算子提出$L_1$自适应容错控制方法,推导Lyapunov方程,并证明稳定性;最后,分析所提方法的瞬态和稳态性能.仿真结果验证了所提出方法良好的容错性、鲁棒性和稳定性,并保证了系统各参数的瞬态和稳态有界性.     

四旋翼无人机鲁棒自适应姿态控制

 四旋翼无人机的姿态控制是自主飞行控制的核心,针对四旋翼姿态易受外界环境干扰和内部参数摄动等不确定性影响的问题,设计了一种鲁棒自适应反步控制器,以提高四旋翼的鲁棒性。建立了四旋翼完整的姿态运动模型,并将其转化为含有广义不确定性的多输入多输出非线性系统。根据该系统满足严格反馈的结构特点,设计了反步控制器; 针对系统中存在的外部干扰和内部参数摄动等不确定性,引入了一类鲁棒自适应函数来抵消该不确定性对系统的影响; 采用非线性跟踪微分器估计虚拟控制量的微分信号,减小了反步控制器设计中普遍存在的“计算膨胀”问题; 通过构造Lyapunov 函数证明闭环系统是稳定且指数收敛的。仿真结果表明,所设计控制器具有良好的控制效果和鲁棒性。