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1.
A sliding mode control algorithm using output information only is developed in this paper for a linear system with mismatched disturbance. The nominal system is allowed to be nonminimum phase. A scheme designed to combine the output‐dependent integral sliding surface with a reduced‐order observer is proposed. Utilizing an H control analytical technique, once the system is in the sliding mode, the proposed algorithm can guarantee robust stabilization and sustain the nature of performing disturbance attenuation when the solution to one algebraic Riccati inequality can be found. A controller is designed to satisfy the reaching and sliding condition in line with the reduced‐order observer. Finally, a numerical example is explained to show the applicability of the proposed scheme. Copyright © 2011 John Wiley and Sons Asia Pte Ltd and Chinese Automatic Control Society  相似文献   

2.
This paper is concerned with the problem of observer‐based control for a class of uncertain neutral‐type systems subjected to external disturbance by utilizing sliding mode technique. A novel sliding mode control (SMC) strategy is proposed based on the state estimate and the output. A new sufficient condition of robust asymptotic stability with disturbance attenuation level for the overall systems composed of the original system and error system in the sliding mode is derived in terms of a linear matrix inequality (LMI). Then, a new adaptive controller is designed to guarantee the reachability of the predefined sliding surface in finite‐time. Finally, numerical examples are provided to verify the effectiveness of the proposed method.  相似文献   

3.
针对欠驱动TORA系统,提出一种基于自调节滑模干扰补偿器的解耦滑模控制方法。所提出的控制方法无需系统不确定性上界的先验信息,对于系统不确定性具有良好的适应性。该控制方法包括设计一种自调节滑模干扰补偿器和一种新型的双幂次趋近律,所设计的自调节滑模干扰补偿器能够利用切换增益自适应算法准确逼近上界未知的系统不确定性,所提出的新型双幂次趋近律能够保证系统状态的快速趋近并抑制控制器的高频抖动。采用Lyapunov稳定性理论证明闭环控制系统的稳定性,并通过数值仿真实验验证所提出的控制方法的有效性。  相似文献   

4.
In this paper, a robust adaptive sliding mode control strategy of micro electro-mechanical system (MEMS) triaxial gyroscope using radial basis function (RBF) neural network is presented for the system identification of MEMS gyroscope. A key property of this scheme is that the prior knowledge of the upper bound of the system uncertainties is not required. An adaptive RBF neural network controller is used to learn the unknown upper bound of model uncertainties and external disturbances. The adaptive RBF neural network is incorporated into the adaptive sliding mode control in the Lyapunov sense, and the stability of the proposed adaptive neural sliding mode control can be established. The dynamics and angular velocities of gyroscope can be identified in real time. Numerical simulations are investigated to verify the effectiveness of the proposed adaptive neural sliding mode control scheme, showing that the designed control system has better robust performance in its insensitivity to system nonlinearities; moreover, system parameters including angular velocity can be consistently estimated and tracking errors converge to zero asymptotically.  相似文献   

5.
This paper presents a fixed-time cooperative guidance law for leader-following missiles, comprising one leader missile with the target seeker and several seeker-less follower missiles. The aim is to achieve a simultaneous attack on a maneuvering target at desired impact angles. First, a guidance law with impact angle control for the leader missile against a maneuvering target is proposed based on nonsingular fast terminal sliding mode (NFTSM) control algorithm. Then, the design of cooperative guidance law for the follower missiles is composed of two parts: along the follower-to-leader line of sight (LOS) direction, the guidance command derived from bi-homogeneous property is designed to ensure that the follower-leader ranges keep proportional consensus with the range-to-go of the leader missile, thus avoiding the estimation of time-to-go ( ); in the normal follower-to-leader LOS direction, considering the relative impact angle constraints which is determined by the leader LOS angle, the guidance command is proposed based on predefined-time sliding mode control method. What's more, a distributed fixed-time observer is designed for the follower missiles to compensate for unobtainable leader missile information. The fixed-time stability of the proposed methods is demonstrated using the Lyapunov theory and bi-homogeneous property. Finally, simulation results confirm the effectiveness and superiority of the proposed fixed-time cooperative guidance law with leader-following strategy.  相似文献   

6.
本文针对Boost变换器的负载电阻扰动和输入电压变化等系统不确定因素对输出电压的影响,提出了一种基于扩张状态观测器的改进滑模控制算法.首先,设计扩张状态观测器对系统状态、负载电阻和输入电压值进行估计,然后基于得到的估计值采用改进滑模控制算法设计系统控制器.通过理论分析,证明了Boost变换器闭环控制系统的稳定性.仿真和实验结果表明,与传统的滑模控制算法相比,本文所提出的控制算法更好地改善了系统的跟踪性能,提升了系统的鲁棒性.  相似文献   

7.
本文主要解决具有约束的二阶系统的固定时间跟踪控制问题,分别讨论了具有输出约束与具有全状态约束的控制算法设计.首先,为解决输出约束下的固定时间控制问题,本文构建了具有输出约束的新型终端滑模变量,并设计了具有扰动抑制能力的固定时间滑模控制律,保证系统输出始终满足约束条件,同时跟踪误差在固定时间内收敛到原点的充分小的邻域内.进一步,为了处理具有全状态约束的控制问题,本文构建了具有全状态约束的终端滑模变量并设计了相应的固定时间滑模控制律.鉴于系统控制律的不连续性,文章采用非光滑分析及Lyapunov稳定性理论证明了闭环控制系统的稳定性.最后,在数值仿真中,将本文提出的方法与传统固定时间滑模方法进行对比,验证了所建立算法的有效性.  相似文献   

8.
This brief proposes a robust control algorithm for stabilization of a three-axis stabilized flexible spacecraft in the presence of parametric uncertainty, external disturbances and control input nonlinearity/dead-zone. The designed controller based on adaptive variable structure output feedback control satisfies the global reaching condition of sliding mode and ensures that the system state globally converges to the sliding mode. A modified version of the proposed control law is also designed for adapting the unknown upper bounds of the lumped uncertainties and perturbations. The stability of the system under the modified control law is established. Numerical simulations show that the precise attitude pointing and vibration suppression can be accomplished using the derived robust or adaptive controller.  相似文献   

9.
崔凯凯  韩维  张勇  张凯伦  刘洁 《控制与决策》2022,37(9):2255-2264
针对舰载机的抗侧风着舰控制问题,设计一种低通非奇异终端滑模引导算法(LNTSMC)用于提高舰载机的抗侧风引导能力. 首先, 基于 H混合灵敏度控制设计内环姿态鲁棒控制系统, 并推导舰载机着舰飞行时的侧向引导方程;然后,基于齐次性理论设计一种积分非奇异终端滑模面,使其在满足低通滑模控制器设计要求的同时避免控制奇异现象;进一步,设计一种带边界层的幂指数趋近律来抑制滑模控制中的抖振情况,并引入非齐次干扰观测器来改善边界层内部的鲁棒稳定性; 最后, 通过 Lyapunov 定理证明所设计算法的有限时间稳定性, 并给出仿真结果. 仿真结果表明,所设计的引导算法具有良好的抗侧风性能,通过与已有算法进行对比,验证了所提出算法的优越性.  相似文献   

10.
将预测控制和滑模控制结合起来,提出一种非线性性模型预测控制方法。给出一种可行的双模控制方案,系统状态位于终端区外时采用提出的预测控制,在终端区内部采用高线设计的滑模控制。对系统终端滑模附加不等式约束,使得系统状态在预测时域的末端位于高线设计的滑动模态区内,从而使预测时域减小。仿真结果表明了算法的有效性。  相似文献   

11.
针对被控对象的参数时变和外部扰动问题,本文融合神经网络的万能逼近能力和自适应控制技术,并结合分数阶微积分理论,提出了基于神经网络和自适应控制算法的分数阶滑模控制策略.本文采用等效控制的方法设计滑模控制律,并利用神经网络的万能逼近能力估测控制律的变化,结合自适应控制算法和分数阶微积分理论抑制传统滑模控制系统的抖震,同时根据Lyapunov稳定性理论分析了系统的稳定性,最后给出了实验结果.实验结果表明,本文提出的基于神经网络和自适应控制算法的分数阶滑模控制系统,能保持滑模控制器对系统外部扰动和参数变化鲁棒性的同时,也能有效地抑制抖震,使得系统获得较高的控制性能.  相似文献   

12.
为稳定放卷张力,提出了自适应滑模摩擦补偿控制算法,对放卷机构中的负载惯量与摩擦进行在线辨识。以放卷电机的转速和角位移误差为变量设计了线性滑模面;以惯量及摩擦估计误差变量及滑模面的偏移变量为基础设计了Lyapunov函数;以该函数的梯度下降为原则设计了在线辨识的自适应律。当系统在自适应滑模控制器的作用下稳定在滑模面上时,负载惯量及摩擦便趋近于其实际值。通过该摩擦补偿方法实现了张力控制目标。对所提方法进行单轴仿真及试验验证,表明该算法能有效提高张力的控制精度。  相似文献   

13.
刘希  孙秀霞  徐嵩  蔡鸣 《控制理论与应用》2014,31(11):1441-1447
针对一类不确定系统,提出了一种具有次优保性能滑模面的静态输出反馈滑模控制方法.首先将滑模面的设计问题等价为一个对称矩阵的求解问题,基于等效控制法,推导了保性能滑模面存在的充分条件.然后基于迭代线性矩阵不等式(iterative linear matrix inequality,ILMI)方法,给出了次优保性能线性滑模面的求解算法,最后基于线性矩阵不等式(linearmatrix inequality,LMI)方法,设计了输出反馈滑模控制器,使得闭环系统渐近稳定且切换函数能在有限时间内到达零.该方法首次实现了输出反馈滑模面的优化,且具有保守性小、无需对被控系统模型进行坐标变换的优点.仿真结果验证了本文方法的优越性.  相似文献   

14.
为了提高传统二阶终端滑模控制的全局收敛性,提出一种快速二阶终端滑模控制算法.设计一种二阶趋近律,将绝对值函数隐藏在积分项里,并增加线性项以提高全局收敛性.当系统状态未到达滑模面时,采用二阶趋近律,并通过调整参数避免奇异问题;当系统状态到达滑模面时,采用不含不连续符号项的指数趋近律,以保证控制误差有限时间收敛.采用Lyapunov直接法证明快速二阶终端滑模控制算法的稳定性,及其比super twisting算法具有更优良的收敛特性.以下肢外骨骼为研究对象,建立动力学模型.在考虑建模误差和外部干扰的情况下,将该算法应用于下肢外骨骼的姿态控制.仿真结果表明,所提出的控制算法能够有效抑制抖振,并且比super twisting算法具有更良好的跟踪性能,验证了该算法的有效性.  相似文献   

15.
滑模预测离散变结构控制   总被引:8,自引:1,他引:7  
研究了不确定离散时间系统的变结构控制设计问题,提出了基于滑模预测思想的离散变结构控制系统设计新思路.该方法综合考虑抖振、鲁棒性以及控制量约束等指标要求,利用当前及过去时刻的滑模信息预测未来时刻的滑模动态,实现了滚动优化求解.仿真结果表明,该方法可有效消除抖振现象,并能够保证闭环系统的鲁棒稳定性.  相似文献   

16.
李义强  周惠兴  CHEN Yaobin 《控制工程》2011,18(5):771-774,814
为提高永磁同步直线电机伺服系统的控制精度和鲁棒性,满足高速度高精度运动控制系统的要求,提出了一种快速终端滑模控制方法并建立了电机系统数学模型.分析和证明该控制算法的稳定性和鲁棒性.与传统的滑模控制方法相比,该算法确保了系统状态在平衡点邻域内具有更快的收敛速度,并最终收敛至平衡点.通过选择控制算法中合适的参数值,系统可达...  相似文献   

17.
A robust tracking control is proposed for the fractional‐order systems (FOSs) to achieve a tracking response with no overshoot, even in the presence of a class of disturbances. The control proposed makes use of a newly designed integral sliding mode technique for FOSs, which is capable of rejecting the bounded disturbances acting through the input channel. The proposed integral sliding mode control design has two components: a nominal control component and a discontinuous control component. The overshoot in the system response is avoided by the nominal control designed with the use of Moore's eigenstructure assignment algorithm. The sliding mode technique is used for the design of discontinuous part of the control that imparts the desired robustness properties.  相似文献   

18.
In general, a Variable Structure (VS) system is designed with a sliding mode. Recently a sliding sector, designed by an algebraic Riccati equation, has been proposed to replace the sliding mode for chattering‐free VS controllers. In this paper we extend the design algorithm for the sliding sector to a time‐varying sliding sector. The time‐varying sliding sector is defined by functions dependent on both state and time, hence time‐varying uncertainty can be considered. The VS controller is designed to stabilize an uncertain system, quadratically. The design procedure for real systems is introduced via an implementation to the control of “Furuta pendulum”. To enhance the stability it is necessary to compensate the time‐varying nonlinear static friction of the actuator adequately, hence this problem is a good example to demonstrate the performance of the proposed VS control method. In the experiment, it will be shown that the VS control with the time‐varying sliding sector is superior to an orthodox chattering‐free VS control.  相似文献   

19.
For uncertain time‐delay systems with mismatch disturbances, this paper presented an integral sliding mode control algorithm using output information only. An integral sliding surface is comprised of output signals and an auxiliary full‐order compensator. The designed output feedback sliding mode controller can locally satisfy the reaching and sliding condition and maintain the system on the sliding surface from the initial moment. Since the system is in the sliding mode and two specific algebraic Riccati inequalities are established, the proposed algorithm can guarantee the stability of the closed‐loop system and satisfy the property of disturbance attenuation. Moreover, the design parameters of the controller and compensator can be simultaneously determined by solutions to two algebraic Riccati inequalities. Finally, a numerical example illustrates the applicability of the proposed scheme. Copyright © 2011 John Wiley and Sons Asia Pte Ltd and Chinese Automatic Control Society  相似文献   

20.
利用一种非线性干扰观测器观测减摇鳍系统的不确定性和随机海浪干扰,通过选择设计参数使观测误差指数收敛.针对引入非线性干扰观测器后的系统采用滑模反演法设计控制器,控制律的设计保证了闭环系统的稳定性.仿真结果表明,在不同浪向角和航速的各种海况下采用该控制策略,系统均能取得较好的减摇效果,同时能很好地克服对象的不确定性和随机海浪干扰,鲁棒性较强.  相似文献   

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