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1.
非奇异快速的终端滑模控制方法   总被引:10,自引:0,他引:10  
针对已有终端滑模控制的奇异和收敛缓慢问题,提出一种非奇异快速终端滑模函数,并利用李亚普诺夫方法证明其有限时间收敛特性.在此基础上,结合带负指数项的吸引子来设计控制律,使控制输入实现时间连续,并保证滑模面全局存在.理论分析表明,通过合理选择控制参数,可使系统避免“收敛停滞”,且对有界模型误差和外部干扰具有较好鲁棒性.  相似文献   

2.
王伟  师兴伟  林德福  毛宁 《控制与决策》2019,34(7):1553-1558
为了降低导弹飞行中不确定因素等对弹体滚转稳定的影响,设计两种新型基于二阶滑模控制理论的滚转稳定控制器,即基于二阶滑模控制理论的控制器与基于super-twisting算法的控制器.第一种控制器能够稳定地控制滚转角收敛至期望值,而第二种控制器不仅能够有效降低气动参数不确定性对弹体滚转控制造成的影响,而且能控制滚转角速度在有限时间内收敛至期望值,并有效抑制滑模算法固有的抖振现象.通过构造Lyapunov函数对所设计控制器的稳定性进行理论验证,将所设计的两种控制器与基于线性滑模控制理论的控制器和基于终端滑模控制理论的控制器进行仿真对比,并考虑不同攻角条件下气动参数的影响,以验证所设计的控制器的有效性、快速性和鲁棒性.  相似文献   

3.
磁悬浮是典型的非线性、不稳定系统.为了实现其控制,本文采用了一种结合二阶滑模和动态滑模两种设计思想的二阶动态滑模控制器的设计方法,首先推导了磁悬浮系统的线性化状态空间模型;然后针对被控对象设计了二阶动态滑模控制器;最后与普通滑模控制器进行对比仿真试验.仿真结果表明,所设计的二阶动态滑模控制器在使小球快速稳定到达平衡点的同时,大大削弱了普通滑模控制器中存在的严重抖振现象.  相似文献   

4.
利用Lyapunov稳定性理论研究了一类广义双线性系统的镇定问题.通过构造特殊的二阶终端滑模超曲面,设计相应的变结构控制器,使闭环系统在有限时间内实现滑动模运动,系统的状态在平衡点渐近稳定.该设计方法能有效削弱系统的高频抖振.仿真结果验证了设计方法的可行性.  相似文献   

5.
针对重装空投过程中,货物的持续移动及瞬间出舱影响空投任务完成性、威胁飞行安全等问题,提出了一种二阶终端滑模纵向飞行控制方法;该方法利用非线性多输入多输出反馈线性化完成系统解耦线性化,在此基础上采用二阶终端滑模变结构控制设计系统内环速度与俯仰姿态跟踪控制器,保证了系统鲁棒性,结合外环PID高度保持控制器完成了整个飞行控制系统的设计;数值仿真结果表明,该系统具有良好的响应特性,且对系统不确定性具有较强的鲁棒性。  相似文献   

6.
针对下肢外骨骼在轨迹跟踪时对内部参数扰动和外界干扰较为敏感的特性,设计一种基于非线性干扰观测器的下肢外骨骼机器人滑模控制策略。首先建立下肢外骨骼上楼梯的动力学模型,分析其动力学特性;其次设计非线性干扰观测器,对下肢系统的不确定性和外部干扰进行观测;在此基础上,为保证系统轨迹跟踪误差的收敛性和减弱抖振,设计了低通滤波的滑模控制器,根据李雅普诺夫稳定性理论证明了下肢系统的稳定性;最后通过仿真与实验验证,该控制策略能够有效克服多种因素引起的干扰,改善系统的控制性能,提高系统的稳定性。  相似文献   

7.
用于刚性机械手的无抖振快速终端滑模控制   总被引:6,自引:0,他引:6       下载免费PDF全文
冯勇  鲍晟  余星火 《控制与决策》2002,17(3):381-384
提出一种用于刚性机械手的无抖振动终端滑模鲁棒控制器。快速终端滑模综合了终端滑模和传统线性滑模的优,能在有限时间内到达平衡点,并降低系统稳态误差。采用优化方法推导出系统的跟踪精度和用于消除抖振的饱和函数和函数宽度之间的数学关系。利用系统的参数化模型,可将参数的不确定部分从回归矩阵中分离出来.根据每个参数不确定范围设计鲁棒控制器。仿真结果证明了该方法的有效性。  相似文献   

8.
针对下肢助力外骨骼膝关节位置伺服系统运动过程中伺服精度要求高、冲击力矩大、负载变化范围广等特点,提出了一种运用模糊规则调节的位置伺服系统滑模控制策略.该策略设计了一种新型带有积分项的滑模面模糊调节部分的结构为单输入双输出,选用模糊规则调节新型终端滑模型趋近率来抑制滑模抖振.仿真及实验表明,该控制策略稳定性和伺服跟踪性好,对负载干扰的鲁棒性强.  相似文献   

9.
为了提高永磁直线同步电机(PMLSM)的位置跟踪精度,本文提出了一种基于神经网络自适应观测器的反推终端滑模控制(TSMC)方法.首先,建立PMLSM的动力学模型.然后,利用RBF神经网络的万能逼近特性去逼近系统中不确定性,并将逼近后的输出信号输入给自适应观测器进行跟踪目标位置和速度的估计,补偿由不确定性所导致的跟踪误差,进而获得高精度的跟踪性能.同时反推TSMC方法能够保证系统状态在有限时间内收敛,有效改善了系统响应速度和鲁棒性能.此外,设计出一种新型饱和函数来改善系统抖振,并利用Lyapunov稳定性定理进行了闭环系统稳定性分析.最后,通过空载和负载实验证实了该控制方案的有效性.  相似文献   

10.
针对稳定平台伺服系统中干扰对跟踪精度的影响,提出一种高阶终端滑模控制算法.首先,提出一种基于super-twisting算法的高阶滑模干扰观测器的设计方法,实现对系统中干扰的快速估计与实时补偿.其次,提出一种基于Lyapunov函数的高阶终端滑模控制器,由到达条件推导而得,高阶终端滑模控制将不连续的切换项作用于变量的高...  相似文献   

11.
有限时间快速收敛滑模变结构控制   总被引:11,自引:1,他引:11       下载免费PDF全文
讨论了一类非线性系统的滑模变结构控制有限时间收敛问题.提出了一种新的收敛滑模超曲面及相应控制方案.研究结果表明,系统状态变量能以较快的收敛速度在有限时间内进入各级滑模超曲面最终到达平衡点,并具有良好的动态性能.最后仿真结果验证了该方案的有效性.  相似文献   

12.
In this paper, a generalized terminal sliding surface is proposed for second-order systems. It is shown that the proposed scheme guarantees that the system state gets to zero in a finite time, and the proposed generalized terminal sliding surface is a superset of the conventional terminal sliding surfaces. The experimental results are given to show the validity of the main result.  相似文献   

13.
基于自适应二阶终端滑模的飞行器再入姿态控制   总被引:2,自引:0,他引:2  
针对飞行器再入过程中存在着模型不确定性因素以及气动环境复杂等鲁棒控制问题,提出一种基于自适应二阶非奇异终端滑模的控制方案.设计的控制器保证姿态跟踪误差在有限的时间内收敛于零,不需要内外扰的先验知识,通过在线自适应辨识扰动上界以消除其影响.最后以气动参数摄动50%作为扰动条件进行了飞行器再入姿态控制仿真,结果表明了该方案的快速性和鲁棒性.  相似文献   

14.
A fast smooth second-order sliding mode control is presented for a class of stochastic systems driven by enumerable Ornstein–Uhlenbeck coloured noises with time-varying coefficients. Instead of treating the noise as bounded disturbance, the stochastic control techniques are incorporated into the design of the control. The finite-time mean-square practical stability and finite-time mean-square practical reachability are first introduced. Then the prescribed sliding variable dynamic is presented. The sufficient condition guaranteeing its finite-time convergence is given and proved using stochastic Lyapunov-like techniques. The proposed sliding mode controller is applied to a second-order nonlinear stochastic system. Simulation results are given comparing with smooth second-order sliding mode control to validate the analysis.  相似文献   

15.
Chattering avoidance by second-order sliding mode control   总被引:1,自引:0,他引:1  
Relying on the possibility of generating a second-order sliding motion by using, as control, the first derivative of the control signal instead of the actual control, a new solution to the problem of chattering elimination in variable structure control (VSC) is presented. Such a solution, inspired by the classical bang-bang optimal control strategy, is first depicted and expressed in terms of a control algorithm by introducing a suitable auxiliary problem involving a second-order uncertain system with unavailable velocity. Then, the applicability of the algorithm is extended, via suitable modifications, to the case of nonlinear systems with uncertainties of more general types. The proposed algorithm does not require the use of observers and differential inequalities and can be applied in practice by exploiting such commercial components as peak detectors or other approximated methods to evaluate the change of the sign of the derivative of the quantity accounting for the distance to the sliding manifold  相似文献   

16.
On multi-input chattering-free second-order sliding mode control   总被引:1,自引:0,他引:1  
A solution to the problem of eliminating the chattering effect, which is always associated with practical implementations of variable structure control, is presented with reference to a class of uncertain multi-input nonlinear systems. The solution procedure relies on the application of an original control approach capable of enforcing a second-order sliding mode (i.e., a sliding regime on a surface s[x(t)]=0 in the system state space, with s˙[x(t)] identically equal to zero, a regime enforced by a control signal depending on s[x(t)], but directly acting only on s¨[x(t)]). Such an approach, in its original formulation, only applies to single-input nonlinear systems with particular types of uncertainties. In the present paper, its validity is extended to multi-input nonlinear systems characterized by uncertainties of more general nature, covering a wide class of real processes  相似文献   

17.
自适应Terminal滑模控制及其在UASV再入中的应用   总被引:1,自引:0,他引:1  
黄国勇  姜长生  王玉惠 《控制与决策》2007,22(11):1297-1301
针对传统模糊干扰观测器在观测误差较小时学习速度缓慢的缺点,提出一种新型快速模糊干扰观测器;然后设计了基于快速模糊干扰观测器的自适应Terminal滑模控制方案,严格证明了跟踪误差和观测误差均在有限时间内收敛到非常小的区域;最后,仿真结果表明了所设计干扰观测器的优越性和闭环控制方案的有效性.  相似文献   

18.
ABSTRACT

This paper endows the second-order sliding mode control (2-SMC) approach with additional capabilities of learning and control adaptation. We present a 2-SMC scheme that estimates and compensates for the uncertainties affecting the system dynamics. It also adjusts the discontinuous control effort online, so that it can be reduced to arbitrarily small values. The proposed scheme is particularly useful when the available information regarding the uncertainties is conservative, and the classical `fixed-gain’ SMC would inevitably lead to largely oversized discontinuous control effort. Benefits from the viewpoint of chattering reduction are obtained, as confirmed by computer simulations.  相似文献   

19.
ABSTRACT

This paper deals with the design of adaptive suboptimal second-order sliding mode (ASSOSM) control laws for grid-connected microgrids. Due to the presence of the inverter, of unpredicted load changes, of switching among different renewable energy sources, and of electrical parameters variations, the microgrid model is usually affected by uncertain terms which are bounded, but with unknown upper bounds. To theoretically frame the control problem, the class of second-order systems in Brunovsky canonical form, characterised by the presence of matched uncertain terms with unknown bounds, is first considered. Four adaptive strategies are designed, analysed and compared to select the most effective ones to be applied to the microgrid case study. In the first two strategies, the control amplitude is continuously adjusted, so as to arrive at dominating the effect of the uncertainty on the controlled system. When a suitable control amplitude is attained, the origin of the state space of the auxiliary system becomes attractive. In the other two strategies, a suitable blend between two components, one mainly working during the reaching phase, the other being the predominant one in a vicinity of the sliding manifold, is generated, so as to reduce the control amplitude in steady state. The microgrid system in a grid-connected operation mode, controlled via the selected ASSOSM control strategies, exhibits appreciable stability properties, as proved theoretically and shown in simulation.  相似文献   

20.
The tracking control problem of hypersonic vehicles is studied and analyzed in this paper using terminal sliding mode control method (TSMC) and non-homogeneous disturbance observer(NHDO) considering parametric uncertainty and external disturbances. Non-singular terminal sliding mode controller is provided based on NHDO. The key idea is that the NHDO is adopted to estimate the aerodynamic uncertainties and external disturbances simultaneously, which can enhance the robustness of the system and lower the gain of the switch controller. Rigorous stability analysis for the closed-loop system is given via Lyapunov stability theory, which proves that the system states are always bounded even during the estimation process when the estimation error is not zero. The sliding manifold can be reached in finite time and the tracking errors can converge to zero asymptotically. Numerical simulations are conducted with the longitudinal nonlinear dynamic model of hypersonic vehicles to verify the effectiveness and robustness of the designed controller.  相似文献   

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