Compensation for secondary uncertainty in electro-hydraulic servo system by gain adaptive sliding mode variable structure control

Based on consideration of the differential relations between the immeasurable variables and measurable variables in electro-hydraulic servo system,adaptive dynamic recurrent fuzzy neural networks(ADRFNNs) were employed to identify the primary uncertainty and the mathematic model of the system was turned into an equivalent linear model with terms of secondary uncertainty.At the same time,gain adaptive sliding mode variable structure control(GASMVSC) was employed to synthesize the control effort.The results show that the unrealization problem caused by some system's immeasurable state variables in traditional fuzzy neural networks(TFNN) taking all state variables as its inputs is overcome.On the other hand,the identification by the ADRFNNs online with high accuracy and the adaptive function of the correction term's gain in the GASMVSC make the system possess strong robustness and improved steady accuracy,and the chattering phenomenon of the control effort is also suppressed effectively.

Variable Structure Model Reference Adaptive Control with Unknown High Frequency Gain Sign

可变结构模型引用为有比一个和未知高频率获得符号大的相对的度的工厂的适应控制被建议。一个切换的计划基于为靠近的环系统的第一个辅助错误设计的监视功能被介绍。在至多切换和追踪的错误的一个有限数字收敛到能被适当地选择一些设计参数使任意地小的一个剩余集合以后，在监视函数的管理下面，切换停止，这被显示出在至多切换和追踪的错误的一个有限数字收敛到能被适当地选择一些设计参数使任意地小的一个剩余集合以后。

Adaptive Variable Structure Control of MIMO Nonlinear Systems with Time-varying Delays and Unknown Dead-zones

In this paper, adaptive variable structure neural control is presented for a class of uncertain multi-input multi-output （MIMO） nonlinear systems with state time-varying delays and unknown nonlinear dead-zones. The unknown time-varying delay uncer- tainties are compensated for using appropriate Lyapunov-Krasovskii functionals in the design. The approach removes the assumption of linear function outside the deadband without necessarily constructing a dead-zone inverse as an added contribution. By utilizing the integral-type Lyapunov function and introducing an adaptive compensation term for the upper bound of the residual and optimal approximation error as well as the dead-zone disturbance, the closed-loop control system is proved to be semi-globally uniformly ultimately bounded. In addition, a modified adaptive control algorithm is given in order to avoid the high-frequency chattering phenomenon. Simulation results demonstrate the effectiveness of the approach.

ADAPTIVE VARIABLE STRUCTURE CONTROLLERS AND APPLICATION TO ENGINE IDLE SPEED CONTROL SIMULATION

A neural-network-based adaptive variable structure control methodology isproposed for the tracking problem of nonlinear discrete-time input-output systems. The unknowndynamics of the system are approximated via radial basis function neural networks. The control lawis based on sliding modes and simple to implement. The discrete-time adaptive law for tuning theweight of neural networks is presented using the adaptive filtering algorithm with residueupper-bound compensation. The application of the proposed controller to engine idle speed controldesign is discussed. The results indicate the validation and effectiveness of this approach.

Adaptive variable structure control for large-scale time-delayed systems with unknown nonlinear dead-zone

The problem of adaptive fuzzy control for a class of large-scale, time-delayed systems with unknown nonlinear dead-zone is discussed here. Based on the principle of variable structure control, a design scheme of adaptive, decentralized, variable structure control is proposed. The approach removes the conditions that the dead-zone slopes and boundaries are equal and symmetric, respectively. In addition, it does not require that the assumptions that all parameters of the nonlinear dead-zone model and the lumped uncertainty are known constants. The adaptive compensation terms of the approximation errors axe adopted to minimize the influence of modeling errors and parameter estimation errors. By theoretical analysis, the closed-loop control system is proved to be semiglobally uniformly ultimately bounded, with tracking errors converging to zero. Simulation results demonstrate the effectiveness of the approach.

VARIABLE STRUCTURE MODEL－FOLLOWING ADAPTIVE CONTROL DESIGN FOR ROBOT MANIPULATORS

The increasing demand on robotic system performance leads to the use of advanced control strategies. A variable structure model-following adaptive control design is presented for the nonlinear robot manipulator systems, when subjected to fast and wide ranges of unknown-but-bounded parameter variations and disturbances. The design does not require any knowledge of a nonlinear robotic system. The system is robust and insensitive to the parameter variation, disturbances, as well as to the unmodeled dynamics. This insensitive property enables the elimination of interactions among the various joints of the robotic manipulator. In the closed loop, the robotic system asymptotically converges to the reference trajectory with a Prescribed transient resPOnse. The problem of chattering is discussed with the introduction of the special approaches: boundary layer, smoothing law, and nonlinear compensation.

Research on Variable Structure and Adaptive Control for Strap-on Rocket

Considering the increase of structural disturbance caused by large thrust misalignment and lack of synchronism after installation of the solid booster on the rock,as well as the increase of external disturbance resulting from the installation of the configuration and tail,while also considering the parameter uncertainties,parameter perturbations,unmodeled dynamics and coupling between channels during modeling,this paper proposes the design method for the adaptive control of sliding mode variable structure,based on the model reference. The paper firstly establishes the attitude dynamics model for the solid strap-on launch vehicle; then proposes the design method for the adaptive control of the sliding mode variable structure based on the model reference,implements the design of attitude control system for the three channels respectively,and uses the Lyapunov function to prove the global asymptotic stability; and finally verifies,through numerical simulation,that the control method proposed in this paper can guarantee the attitude stability of rockets in the primary flight phase.

A Variable Structure Model Reference Adaptive Control

A variable structure model reference adaptive control problem for the nonlinear system is studied in this paper. First, according to the relative degree concept of th nonlinear control system an error equation between the outputs of the reference model and the controlled plant is derived. Then, by using the variable structrue control method, an algorithm of variable structure model reference adaptive control is deduced on the basis of a new concept of reaching law. The definition of the SISO system is introduced into the MIMO nonlinear system. Finally, as an example, a pendulum nonlinear control system is simulated to demonstrated the effectiveness of the method. The results show that the method has some advantages: the design is simple, intuitive and easy to be realized in engineering. Besides, it is of practical significance for the synthesis of nonlinear control systems.

Adaptive Neural Control for a Class of Low-triangular-structured Nonlinear Systems with H-∞ Performance Analysis

In this paper, a neural-network-based variable structure control scheme is presented for a class of nonlinear systems with a general low triangular structure. The proposed variable structure controller is proved to be Cl, thus can be applied for backstepping design, which has extended the scope of previous nonlinear systems in the form of strict-feedback and pure-feedback. With the help of neural network approximator, H-∞ performance analysis of stability is given. The effectiveness of proposed control law is verified via simulation.

Adaptive Sliding Mode Control for MIMO Nonlinear Systems Based on Fuzzy Logic Scheme

In this study an indirect adaptive sliding mode control (SMC) based on a fuzzy logic scheme is proposed to strengthen the tracking control performance of a general class of multi-input multi-output (MIMO) nonlinear uncertain systems. Combining reaching law approach and fuzzy universal approximation theorem, the proposed design procedure combines the advantages of fuzzy logic control, adaptive control and sliding mode control. The stability of the control systems is proved in the sense of the Lyapunov second stability theorem. Two simulation studies are presented to demonstrate the effectiveness of our new hybrid control algorithm.

基于混沌控制的采摘机器人防碰撞系统设计

针对采摘机器人在作业过程中遇到障碍物导致路径规划出现混沌现象的问题,基于混沌控制对采摘机器人防碰撞系统进行设计,并采用模糊自适应控制算法和滑模变结构控制算法结构的方式对系统进行控制。为了验证防碰撞系统的有效性,对采摘机器人进行了防碰撞和采摘仿真试验,结果表明:采摘机器人在作业过程中可以避开障碍物,按照规划路线到达预设位置,完成果蔬的采摘。

融合反步法的无人驾驶汽车轨迹跟踪控制方法

为了解决无人驾驶汽车轨迹跟踪控制的准确性、稳定性和快速性问题,将反步法分别融合滑模变结构控制和模糊自适应控制.建立车辆三自由度运动学位姿误差微分方程,推导了基于反步法的车速和横摆角速度控制律,结合Lyapunov稳定性判据验证了系统稳定性.分别建立融合反步法的滑模变结构和模糊自适应轨迹跟踪控制方法,结合轨迹跟踪稳态误差、超调量和调整时间,验证、比较了控制方法准确性、稳定性和快速性3种性能的优劣.结果表明:融合反步法的滑模变结构轨迹跟踪控制的稳定性最好,轨迹跟踪超调量接近于0;融合反步法的模糊自适应轨迹跟踪控制快速性最好,轨迹跟踪调整时间相对于反步法缩短了18.2%.

Variable structure control for MRAC systems with perturbations in input and output channels

A design scheme of variable structure model reference control systems using only input and output measurements is presented for the systems with unmodeled dynamics and disturbances in input and output channels. The modeled part of the systems has relative degree greater than one and unknown upper bound of degree. By introducing some auxiliary signals and normalized signals with memory functions and appropriate choice of controller parameters, the developed variable structure controller guarantees the global stability of the closed-loop system and the arbitrarily small tracking error.

Adaptive estimation and nonlinear variable gain compensation of the contouring error for precise parametric curve following

Contour following is one of the most important issues faced by many computer-numerical-control(CNC) machine tools to achieve high machining precision. This paper presents a new real-time error compensation method aiming at reducing the contouring error caused by facts such as servo lag and dynamics mismatch in parametric curved contour-following tasks. Due to the lack of high-precision contouring-error estimation method for free-form parametric curved toolpath, the error can hardly be compensated effectively. Therefore, an adaptive accurate contouring-error estimation algorithm is proposed first, where a tangential-error backstepping method based on Taylor's expansion is developed to rapidly find the closest point on the parametric curve to the actual motion position. On this foundation, the contouring error is compensated using a proposed nonlinear variable-gain compensation method, where the compensation gain is obtained according to not only the contouring-error magnitude but also its direction variation. The stability of the system after compensation is analyzed afterwards according to the Jury stability criterion.By design of the compensator in accordance with the presented contouring-error compensation method as well as the stability analyzation result, the balance between the response speed and the contour control stability can be effectively made. Experimental tests demonstrate the feasibility of the presented methods in both contouring-error estimation and contour-accuracy improvement.Contributions of this research are significant for enhancing the contour-following performance of the CNC machine tools.

仿真转台控制系统变结构自适应控制技术研究

仿真转台是航空航天及工业领域重要的仿真设备。为了使仿真转台控制系统适应负载转动惯量变化,并增强其对控制系统数学模型参数摄动、外界干扰等的鲁棒性,现将自适应理论应用于仿真转台的伺服控制系统,并使用变结构滑模控制设计控制律,添加全程滑动模态因子,设计了一种基于现代控制的复合自适应控制器。使用Simulink和Matlab搭建仿真环境,在20 Hz的正弦信号下得到负载变化前后的仿真结果。PID控制系统和自适应控制系统的响应幅值误差分别增大了3.6%和1.3%,证明了自适应控制有效地降低了系统的误差。当输入阶跃信号时,自适应控制系统将稳态误差由3.2%减小到0.3%。最后在仿真转台上进行了实物实验。在幅值0.1°频率20 Hz的正弦信号下,添加负载及干扰后,PID控制系统的响应幅值误差增大了6.6%,而自适应控制系统的幅值误差仅增大2.4%,比PID控制系统误差变化小。实验结果表明,自适应控制器的控制效果优于PID控制器,所设计的自适应控制器提高了控制系统对负载变化和干扰的鲁棒性。

多虚拟同步机系统的自适应滑模变结构控制方法

虚拟同步机是一种可以改善分布式能源并网兼容性的技术手段。目前有关虚拟同步机滑模控制的研究大多数仅针对于单机系统。由于单机系统无需考虑多机系统中出现的虚拟惯量等参数之间的耦合影响,这导致现有的滑模变结构控制策略不适用于多虚拟同步机系统,当功率波动时系统频率有可能产生振荡。针对上述问题,提出了多虚拟同步机虚拟惯量的整定判据,并基于整定判据提出多虚拟同步机系统的自适应滑模变结构控制策略,可以使系统中各台机组在扰动状态下输出稳定频率。通过自适应滑模变结构控制策略使得多虚拟同步机组在功率波动时输出稳定的频率,从而避免系统频率失稳。最后,通过搭建PSCAD仿真模型验证了理论分析的正确性及有效性,所提控制方法可提高多虚拟同步机系统的稳定性与鲁棒性。

基于预瞄时间自适应的爆胎车辆横向控制

针对汽车在高速行驶过程中突然爆胎极易引发严重交通事故的问题,文章提出一种基于预瞄时间自适应的爆胎车辆横向控制方法。在单点预瞄驾驶员模型的基础上,提出一种预瞄时间自适应算法,通过预测未来一段时间内不同预瞄时间的车辆运行状况,将道路边界约束添加为约束条件设计优化函数,选取合适的预瞄时间,提高车辆的行驶稳定性;采用滑模控制理论设计主动转向控制器,根据爆胎前、后横摆角速度偏差对车辆前轮转角进行补偿,以解决爆胎导致的车辆横向偏航问题。在CarSim与Simulink联合仿真平台下进行的仿真验证结果表明,该文提出的控制方法可以使爆胎车辆基本保持在原路径上行驶,有效提高了车辆的稳定性和安全性。

基于参数摄动模型的航空发动机鲁棒弹性自适应控制

航空发动机特性随飞行条件和工作状态变化,在复杂工作环境中同时存在模型不确定性和控制器自身参数变化问题,很大程度上影响整个飞行包线的控制性能。为此,文章提出一种基于参数摄动模型的航空发动机鲁棒弹性自适应控制方法。其首先建立了航空发动机参数摄动结构化模型;然后针对被控对象模型的不确定性和控制器增益的摄动,利用李雅普诺夫稳定性(Lyapunov stability)理论和线性矩阵不等式约束,设计了增益摄动有界但上界未知时的鲁棒弹性自适应控制律,将控制器的设计问题转化为线性矩阵不等式的可行解问题,使控制器的设计仅依赖线性矩阵不等式解矩阵的存在性,并证明了算法的稳定性。在此基础上,文章对飞行包线内发动机不同工作状态进行控制仿真验证。结果显示,调节时间小于1.8 s,超调量小于5%,这表明所设计控制器具有良好的稳定性和控制性能。

基于ESO的磁悬浮直线同步电机变增益自适应迭代学习控制

对于可控励磁磁悬浮直线同步电机(CEMLLSM),常规迭代学习控制(ILC)精度低、抖振大,且抗外部扰动能力差。为提高跟踪精度,设计了一种基于扩张状态观测器(ESO)的变增益自适应ILC算法。首先,研究CEMLLSM的工作原理及数学模型。其次,设计基于ESO的变增益自适应迭代学习控制器,为控制器中固定增益部分引入指数可变增益,增加自适应迭代项对控制律中的未知参数进行迭代学习,从而减小系统抖振与误差并加快系统收敛速度。通过引入ESO观测系统的外部干扰,对控制量进行补偿,进而提高系统的抗扰动能力。最后,用MATLAB对控制系统进行仿真分析,仿真结果表明该算法能够有效减小跟踪误差,并对扰动有良好的抑制作用。

一种用于毫米波探测系统的变步长LMS-AGC方案

在毫米波探测系统中,自动增益控制(AGC)是信号处理系统的关键技术之一,其作用是应对大动态范围的中频信号接收。本文阐述了一种数字自动增益控制(DAGC)的实现方案,通过对中频信号的数字采样进行处理,采用基于平均功率参量的变步长LMS-AGC自适应算法,将自适应滤波器的变步长思想应用到AGC方案中,并对其步长算法进行优化。通过对比普通功率检测自动增益控制和固定步长LMS-AGC方案,本文提出的变步长LMS-AGC方案具有更快的收敛速度和更小的稳态误差。