基于滑模观测器的非线性系统迭代学习控制

针对相当广泛的一类非线性系统有限时间轨迹跟踪问题,提出了一种基于滑模观测器的迭代学习控制算法。根据系统的非线性特性,利用一种滑模观测器对系统的状态进行估计,根据估计信号设计了一种类D型开环迭代学习控制律。这种控制方法不需要对系统的跟踪误差信号进行微分,从而对系统的量测噪声不敏感。给出了控制算法的收敛性证明,通过仿真实验证明了这种算法的有效性。     

基于非线性干扰观测器的高超声速飞行器反演滑模控制

针对高超声速飞行器非线性动力学系统中存在的高度非线性、多变量耦合及参数不确定等特点,利用非线性干扰观测器对各种干扰的逼近特性,结合反演滑模控制,设计了一种飞行器反演滑模控制器。该方法首先利用干扰观测器观测出系统的干扰,未观测出的部分干扰使用反演滑模控制进行补偿,避免了累积误差,实现对制导指令的鲁棒输出跟踪,并证明了系统稳定性。仿真结果验证了该方法能较理想地观测干扰,保证系统良好的鲁棒性。     

基于二阶滑模的BTT导弹反演滑模控制

针对具有非匹配不确定性的倾斜转弯(bank-to-turn, BTT)导弹非线性动力学模型,基于反演思想和二阶终端滑模控制方法,设计了一种新的BTT导弹反演滑模控制器。反演设计的每一步均采用滑模控制对不确定性进行补偿,并在最后一步设计中采用非奇异二阶终端滑模控制,既能防止抖振对舵机造成损坏,又减小了累积误差。采用精确微分器解决“计算膨胀”问题,并证明了跟踪误差最终有界。仿真结果表明,通过适当选取设计参数,跟踪误差将收敛到原点附近任意小的邻域内。     

一类不确定离散网络系统的全局滑模控制

针对动态传输控制协议(transmission control protocol, TCP)网络的拥塞问题,基于离散全局滑模控制理论设计了一种主动队列管理(active queue management, AQM)算法,该算法消除了滑模控制的到达阶段,保证网络系统在整个控制过程中的鲁棒性。为了减弱离散指数趋近律的抖振现象,给出了一种改进的滑模趋近律,使得复杂的网络系统具有良好的性能。仿真结果验证了所设计的控制器对活动的TCP连接数、链路带宽及往返时延的不确定性具有很强的稳定性和鲁棒性。     

基于观测器的不确定非线性系统L1自适应控制

针对一类严格块反馈型不确定非线性系统,采用反步设计方法提出了一种新的基于滑模状态观测器的L1自适应控制方案。由于系统状态不完全可测,首先设计滑模观测器对系统状态进行估计,并分析观测器的收敛性,在此基础上,通过反步法得到系统的理想控制律。为了消除反步控制中的“项数膨胀”,引入非线性跟踪微分器来提取理想控制律的微分信号。为提高系统响应的瞬态性能,消除控制输入的高频振荡,引入L1自适应控制对控制律进行改进,通过理论推导证明了闭环系统的稳定性。最后通过数值仿真算例验证了所设计控制方案具有快速的收敛性、良好的跟踪性等期望性能。     

Neural network based adaptive sliding mode control of uncertain nonlinear systems

The purpose of this paper is the design of neural network-based adaptive sliding mode controller for uncertain unknown nonlinear systems. A special architecture adaptive neural network, with hyperbolic tangent activation functions, is used to emulate the equivalent and switching control terms of the classic sliding mode control (SMC). Lyapunov stability theory is used to guarantee a uniform ultimate boundedness property for the tracking error, as well as of all other signals in the closed loop. In addition to keeping the stability and robustness properties of the SMC, the neural network-based adaptive sliding mode controller exhibits perfect rejection of faults arising during the system operating. Simulation studies are used to illustrate and clarify the theoretical results.     

不确定奇异系统的Terminal滑模控制

针对一类不确定奇异系统,研究其Terminal滑模控制问题。通过非奇异线性变换把不确定奇异系统变换成受限等价形式,利用Lyapunov函数方法,首次提出了一种新的Terminal滑模控制策略,给出了特殊的Terminal滑模超曲面,设计了相应的滑模控制器,实现了滑模运动,保证了系统状态变量在有限时间内收敛到平衡点。给出数值算例,说明了方法的有效性。     

Discrete sliding mode prediction control of uncertain switched systems

The robust stabilization problem for a class of uncertain discrete-time switched systems is presented. A predictive sliding mode control strategy is proposed, and a discrete-time reaching law is improved. By applying a predictive sliding surface and a reference trajectory, combining with the state feedback correction and rolling optimization method in the predictive control strategy, a predictive sliding mode controller is synthesized, which guarantees the asymptotic stability for the closed-loop systems. The designed control strategy has stronger robustness and chattering reduction property to conquer with the system uncertainties. In addition, a unique nonswitched sliding surface is designed. The reason is to avoid the repetitive jump of the trajectories of the state components of the closed-loop system between sliding surfaces because it might cause the possible instability. Finally, a numerical example is given to illustrate the effectiveness of the proposed theory.     

飞行器自适应反推Terminal滑模轨迹跟踪控制

飞行器非线性动力学模型通常包含由未知外界干扰和未建模动态构成的非匹配不确定性。针对建立的飞行器纵向运动仿射非线性模型,提出了一种基于非线性干扰观测器(nonlinear disturbance observer, NDO)的自适应反推非奇异终端滑模(adaptive backstepping nonsingular terminal sliding mode,AB-NTSM)轨迹跟踪控制方法。设计非线性干扰观测器对未知干扰进行观测补偿,无需干扰上界先验知识。设计未建模动态自适应律,提高控制器对系统不确定性的鲁棒性。对3种不同情况的仿真表明,干扰观测器能够实现对不同干扰精确观测,仅在干扰突变时有较大观测误差。在不确定性影响下,采用提出的控制方法,系统能够实现对指定轨迹的稳定跟踪,并有效消除控制信号的抖振。     

基于RBF神经网络的鲁棒滑模观测器设计

针对非线性不确定性系统,提出一种鲁棒滑模观测器。所提出的鲁棒滑模观测器通过滑模与相应的控制策略来实现。设计参数的选取不需要求解大量方程,同时能保证对系统的非线性不确定性具有鲁棒性,系统中不确定性的上界值采用RBF神经网络进行自适应学习。通过设计滑模,可以调整观测器跟踪系统状态的收敛速度,使状态估计达到预期的指标。仿真结果验证了提出方法的有效性。     

Robust control of uncertain time delay system:a novel sliding mode control design via LMI

1 .INTRODUCTIONTi me-delay commonly occurs in various industrialsystems ,such as turbojet engines , electrical net-works ,automotive systems ,and chemical process ,etc .Its existenceis usually a source of poor systemperformance ,or instability . Hence ,the control ofti me delay systems has received considerable atten-tion over the past two decades , and different de-sign approaches have been proposed[1]. We wouldlike to point out SMC is a reasonable method tostabilize the uncertain ti me…     

基于NDO的飞行模拟转台伺服系统跟踪控制

针对飞行模拟转台伺服系统跟踪控制问题,提出了一种基于非线性干扰观测器(nonlinear disturbance observer, NDO)的反推全局滑模控制方案。该方案利用NDO观测系统的参数不确定性及非线性摩擦干扰,通过选择适当的设计参数使观测误差指数收敛,进而对引入NDO的系统采用反推全局滑模设计控制器,控制律的设计保证了闭环系统的稳定性。仿真结果表明,所提控制方案能够有效克服参数不确定性及非线性摩擦干扰的影响,实现了转角位置的精确跟踪,并且有效去除了控制抖振。     

Global robust optimal sliding mode control for uncertain affine nonlinear systems

The problem of robustifying linear quadratic regulators (LQRs) for a class of uncertain affine nonlinear systems is considered. First, the exact linearization technique is used to transform an uncertain nonlinear system into a linear one and an optimal LQR is designed for the corresponding nominal system. Then, based on the integral sliding mode, a design approach to robustifying the optimal regulator is studied. As a result, the system exhibits global robustness to uncertainties and the ideal sliding mode dynamics is the same as that of the optimal LQR for the nominal system. A global robust optimal sliding mode control (GROSMC) is realized. Finally, a numerical simulation is demonstrated to show the effectiveness and superiority of the proposed algorithm compared with the conventional optimal LQR.     

基于有限时间收敛干扰观测器的探导控一体化设计

针对滚仰式半捷联寻的制导导弹,提出一种基于有限时间干扰观测器(finite time disturbance ob-server,FTDO)的探导控一体化滑模控制器设计方法.首先基于滚仰式半捷联导引头动力学模型和导弹制导控制模型,建立了全状态耦合探测、制导、控制一体化控制模型.在模型中将不确定项和误差视为干扰,通过有限...     

固定时间收敛扰动观测终端滑模制导律设计

针对机动目标拦截问题,设计了基于固定时间收敛扰动观测器(fixed time disturbance observer, FxTDO)的终端角度约束非奇异快速终端滑模制导律(nonsingular fast terminal sliding mode guidance law, NFTSMGL)。通过具有固体时间收敛特性的扰动观测器对导弹拦截过程的外部扰动进行快速、精确估计。同时为了抑制抖振影响以及保证制导信号在有限的时间范围内收敛,设计了NFTSMGL,并进行了稳定性分析。仿真结果表明，FxTDO-NFTSMGL可以使制导信号在有限的时间范围内收敛至期望状态,并满足对机动目标拦截的要求,相较于无观测器的NFTSMGL收敛速度更快,且避免了抖振现象。     

Sliding mode H∞ control for a class of uncertain nonlinear state-delayed systems

A new proportional-integral (PI) sliding surface is designed for a class of uncertain nonlinear state-delayed systems. Based on this, an adaptive sliding mode controller (ASMC) is synthesized, which guarantees the occurrence of sliding mode even when the system is undergoing parameter uncertainties and external disturbance. The resulting sliding mode has the same order as the original system, so that it becomes easy to solve the H∞ control problem by designing a memoryless H∞ state feedback controller. A delay-dependent sufficient condition is proposed in terms of linear matrix inequalities (LMIs), which guarantees the sliding mode robust asymptotically stable and has a noise attenuation level γ in an H∞ sense. The admissible state feedback controller can be found by solving a sequential minimization problem subject to LMI constraints by applying the cone complementary linearization method. This design scheme combines the strong robustness of the sliding mode control with the H∞ norm performance. A numerical example is given to illustrate the effectiveness of the proposed scheme.     

Decentralized model reference adaptive sliding mode control based on fuzzy model

1.INTRODUCTIONIn recent years,decentralized control of interconnect-ed systems has become an i mportant and challengingtopic[1~3].However,it is usually difficult to modelthe systemexactly due to the complex real environ-ment.In the past several years,active research hasbeen carried out in controller design based on univer-sal approxi mators,such as fuzzy control and neuralnetwork control[4~6].For a class of SISO nonlinearsystems,adaptive fuzzy control approaches were pro-posed based on …     

Robust bounded control for uncertain flight dynamics using disturbance observer

The robust bounded flight control scheme is developed for the uncertain longitudinal flight dynamics of the fighter with control input saturation invoking the backstepping technique. To enhance the disturbance rejection ability of the robust flight control for fighters, the sliding mode disturbance observer is designed to estimate the compounded disturbance including the unknown external disturbance and the effect of the control input saturation. Based on the backstepping technique and the compounded disturbance estimated output, the robust bounded flight control scheme is proposed for the fighter with the unknown external disturbance and the control input saturation. The closed-loop system stability under the developed robust bounded flight control scheme is rigorously proved using the Lyapunov method and the uniformly asymptotical convergences of all closed-loop signals are guaranteed. Finally, simulation results are presented to show the effectiveness of the proposed robust bounded flight control scheme for the uncertain longitudinal flight dynamics of the fighter.     

不确定时滞反应扩散系统的滑动模控制

借助不等式分析方法研究一类不确定时滞反应扩散系统的滑动模控制问题,设计了滑模控制器。分析了在滑动模切换面上滑动模控制系统关于不确定量的不变性特征,为研究在系统工作环境的变化、降阶近似、线性化近似、测量误差等因素干扰下所建立的实际控制系统的数学模型———不确定时滞分布参数控制系统的鲁棒性问题奠定了理论基础。     

不确定多变量线性系统的快速收敛滑模控制

讨论了一类不确定多变量线性系统滑模变结构控制的快速收敛问题,提出一种指数型快速终端滑模变结构控制方案。通过非奇异线性变换将不确定系统化为简约标准型,而后设计了非线性指数型快速终端滑模超曲面,给出了滑模面参数矩阵的选择方法。在此基础上设计了变结构控制律,使系统状态在有限时间内到达滑模面上,随后保持在滑模面上并按指数型终端滑模的规律运动,在有限时间内收敛到平衡点。与普通的快速终端滑模相比,系统状态能以更短的时间到达平衡点。该方法具有全局稳定性和鲁棒性,仿真结果证明其有效性。