一种新的滑动模态到达条件

给出了确定滑动模态吸引区的新方法，用此方法讨论了控制受限情况下变结构控制系统的稳定性，研究了利用非线性切换函数设计的变结构控制系统。     

A Sub-Optimal Second Order Sliding Mode Controller for Systems With Saturating Actuators

In this technical note, the problem of the possible saturation of the continuous control variable in the sub-optimal second order sliding mode controller, applied to systems with saturating actuators, is addressed. It is proved that during the sliding phase, if basic assumptions are made, the continuous control variable never saturates. On the contrary, during the reaching phase, the presence of saturating actuators can make the steering of the sliding variable to zero in a finite time not always guaranteed. In the present technical note, the original algorithm is modified in order to solve this problem: a new strategy is proposed, which proves to be able to steer the sliding variable to zero in a finite time in spite of the presence of saturating actuators.      

用于离散滑模重复控制的新型趋近律

针对不确定离散时间系统, 提出一种新型的离散趋近律, 构造理想切换动态, 并基于理想切换动态设计离散滑模重复控制器. 在消除系统颤振的同时, 完全抑制周期扰动带来的影响, 改善控制品质. 分别推导了切换函数的绝对收敛层、单调收敛层和拟滑模带的边界, 用于刻画在不同控制器参数下闭环系统的趋近过程和拟滑模运动. 数值仿真和在伺服装置上的实验结果证实了所提出控制方法的有效性.     

战车稳定器最优滑动模态变结构控制仿真研究

该文为战车稳定器提供一种有实用价值的现代设计方法 ,文中的滑动模态变结构控制在趋近段也具有鲁棒性。在变结构控制中采用观测器可有效地消除系统未建模动态在输出中引起的振荡或抖振 ,是一种可供广泛应用的设计方法     

Backstepping - Sliding Mode Controllers Applied to a Fixed-Wing UAV

This paper deals with the design of five controllers, based on Backstepping and Sliding Modes, which are applied to a fixed-wing unmanned aerial vehicle (UAV). We are interested to realize a comparative analysis of such methodologies in order to know what controller has a better performance when they are used to the autonomous flight (altitude, yaw and roll) of a fixed-wing UAV. The designed controllers are: Backstepping, Sliding Mode control (SMC), Backstepping with Sliding Mode control, Backstepping with two Sliding Mode control, and Backstepping with high order Sliding Mode (HOSM) control. Simulation results are obtained in order to analyze the controllers performance. We finally present an experimental result, in open-loop, with the purpose of validate the magnitude of the control signals obtained in the simulations.     

分散自适应模糊滑模控制器的设计与分析

研究了一类具有函数控制增益的耦合大系统的分散自适应模糊控制问题 ,提出了能够利用专家的语言信息和数字信息的分散自适应模糊滑模控制器的设计方案 .通过理论分析 ,证明了分散自适应模糊控制系统是全局稳定的 ,跟踪误差可收敛到零的一个邻域内     

Sliding Mode and PI Controllers for Uncertain Flexible Joint Manipulator

This paper is dealing with the problem of tracking control for uncertain flexible joint manipulator robots driven by brushless direct current motor(BDCM). Flexibility of joint in the manipulator constitutes one of the most important sources of uncertainties. In order to achieve high performance, all parts of the manipulator including actuator have been modeled. To cancel the tracking error, a hysteresis current controller and speed controllers have been developed. To evaluate the effectiveness of speed controllers, a comparative study between proportional integral(PI) and sliding mode controllers has been performed. Finally, simulation results carried out in the Matlab simulink environment demonstrate the high precision of sliding mode controller compared with PI controller in the presence of uncertainties of joint flexibility.     

引入趋近律的功率因数校正滑模控制仿真研究

提出一种引入趋近律的滑模变结构控制(SMVSC)方法来实现有源功率因数校正(APFC),减少电流的谐波成分.SMVSC是一种解决非线性时变系统(如APFC系统)问题的良好办法,但是实际应用中SMVSC的"抖振"现象问题必须要解决好.引入趋近律来削弱APFC系统在滑模控制中的"抖振"现象,并且依此推导出了控制APFC系统中的功率开关的PWM占空比.采用Matlab平台进行仿真验证控制策略控制APFC电路几乎得到单位功率因数,同时超调减小、响应时间缩短.     

基于变指数趋近律的起重机自适应滑模控制

以起重机升降系统位置控制为目标,针对传统滑模控制中要求系统不确定因素的界为已知的缺点,将自适应控制引入传统滑模变结构控制中,通过设计自适应律对起重机升降系统参数的变化及外部扰动进行辨识,同时采用变指数趋近律进一步克服传统滑模方法中存在的抖振问题。仿真结果表明,该控制算法不仅保持了传统滑模方法良好的鲁棒性,而且提高了系统的控制精度,减小了系统的抖振。     

Sliding Mode Control with Adaptive Fuzzy Immune Feedback Reaching Law

In this paper, a novel adaptive fuzzy immune feedback reaching law (AFIFRL) based sliding mode control (SMC) strategy is proposed for uncertain nonlinear systems with time-varying disturbances. First, a nonlinear immune feedback reaching law (IFRL) inspired by biological immune feedback regulation mechanism is designed to alleviate chattering effect without losing the robustness against disturbances. Second, an improved IFRL is developed in a thin boundary layer to enhance tracking performance. Then, the applied fuzzy controller adjusts the boundary layer online to further improve control performance despite large system uncertainties and disturbances. Furthermore, an adaptive law is employed to estimate the unknown bound of uncertainties, which can effectively attenuate chattering and minimize control effort. The stability analysis is derived by Lyapunov stability theorem. Finally, numerical simulations are conducted to evidence the effectiveness and superiority of the proposed AFIFRL based SMC scheme.     

一类非线性不确定系统的高阶积分自适应滑模控制

为有效改善传统积分滑模在一类非线性不确定系统的应用中存在的抖振问题,结合有限时间收敛理论、高阶积分滑模理论和自适应控制理论,提出了一种高阶积分自适应滑模控制方法;该方法通过选取有限时间收敛反馈量和设计高阶积分滑模面,不仅确保了系统状态误差在有限时间内的收敛性,而且还保证了系统具备对不确定性干扰的抑制能力;同时,当系统的不确定项的边界范围无法预先确定时,采用自适应方法对滑模控制的趋近速率进行估计;仿真结果表明所提方法能够有效抑制非线性不确定系统的抖动,并具有较高的控制精度.     

永磁同步电机自适应高阶滑模Type-2模糊控制

针对t永磁同步电机数学模型不确定问题,提出一种自适应高阶滑模Type-2模糊控制方法.采用积分滑模面二阶滑模控制律,保持传统滑模控制的鲁棒性并实现不含不确定高阶输入输出有限时间稳定;不需要预先确定干扰与不确定上边界,利用yapunov理论获得自适应调节Type-2模糊规则生成Super--Twisting信号削弱抖振.仿真结果表明永磁同步电机具有良好的跟踪性能,同时验证了该方法的可行和有效性.     

基于改进型PI趋近律的无刷直流电机滑模控制

针对无刷直流电机模型参数时变的特性,为解决传统PID控制易受模型参数变化影响的弊端与传统滑模控制(SMC)的抖振问题,将分数阶PI与变速趋近律结合,提出了一种改进型PI趋近律的无刷直流电机滑模控制算法。该算法通过对趋近律的改进,既避免了模型参数变化的影响,又减小了系统输出的抖振。仿真与实验结果表明,与传统滑模控制、传统PI控制相比,具有响应快、鲁棒性强、超调小、抖振小等优点,是一种更优的控制方法。     

Fractional Order Exponential Type Discrete-time Sliding Mode Control

International Journal of Control, Automation and Systems - In this paper, a new fractional order exponential type reaching law (FOE-RL) is presented for the uncertain discrete-time system. The...     

基于积分滑动流形的高阶滑模控制器设计

滑模变结构控制方法因其易实现,鲁棒性强等优点广泛应用于实际控制系统中,讨论了具有积分滑动流形的高阶滑模控制器的设计方法.通过设计含积分滑动流形的高阶滑模面,使系统状态在一阶乃至高阶滑模面上均能达到滑动模态.同时利用高阶滑模面为状态变量设计新的状态空间系统,将原先促使系统状态接近并停留在滑模面上的控制目标,拓展为使高阶滑模状态变量趋近于零的控制目标,并结合最优控制方法来设计等效控制量,利用积分流形设计切换控制的切换面,通过严格证明来证实控制器设计的稳定性.在仿真验证部分采用了一阶倒立摆模型,通过比较常规趋近律滑模控制方法和本文方法的仿真结果,可以得出本文方法在减小系统控制量抖振方面的重要作用和优异效果.     

一种多幂次滑模趋近律设计与分析

针对传统滑模趋近律使系统存在抖振现象、收敛速度较慢及动态响应不平滑等问题, 提出一种多幂次滑模趋近律.该趋近律通过三个幂次项系数在系统趋近过程不同阶段进行针对性地调节, 使系统动态响应过程的收敛速度大幅度提高, 且无抖振现象.理论验证了其存在性、可达性及稳定性, 并详细推导了趋近速率及干扰稳定界.以航天器姿态机动控制系统为例, 对比仿真结果表明该趋近律下, 系统的动态过程有较大改善并消除了抖振, 且在存在模型不确定性及外加干扰作用下, 系统仍可较快地收敛到平衡点附近的邻域内.     

不确定离散系统自适应趋近律滑模控制技术研究

针对受噪声干扰的含有未知参数的离散系统控制问题,首先利用强跟踪滤波器对未知参数进行估计,接着提出了一种自适应离散趋近律滑模控制方法．深入研究分析了该离散趋近律方法的抖振问题,设计了基于该新型趋近律的滑模控制器．仿真结果表明所设计的控制器能有效降低抖振,改善控制性能．     

基于高层滑模具有最少规则的模糊滑模控制

通过引进高层滑模,进一步简化了模糊滑模控制的结构。有效地避免了则的组合爆炸,仿真结果表明了该方法的有效性和简单性。