一类高阶非线性系统的级联自抗扰控制

针对类似板球系统的一类高阶、强耦合、不确定非线性系统,利用backstepping算法的思想,提出以多个低阶自抗扰控制器级联实现控制的方法.通过各低阶自抗扰控制器的扩张状态观测器观测出各级对象的内外扰动,然后进行补偿,较好地解决了高阶非线性系统的不确定性、耦合性及干扰抑制问题.以板球系统的轨迹跟踪控制为例进行研究,所得结果表明,该方案适用于复杂高阶非线性级联系统的控制,具有良好的动态特性及鲁棒性.     

基于自抗扰技术的光伏发电并网控制系统

单相可再生能源并网发电系统是一非线性系统,受电网和环境的影响,系统存在较强的外部干扰和非线性不确定因素.针对系统的工作特点,采用自抗扰控制技术来实现对系统的有效控制.系统利用自抗扰控制器(ADRC)的扩张状态观测器,来对系统模型中的不确定因素和外扰进行动态观测,使系统对扰动具有很好的适应能力.并在系统的扩张状态观测器和非线性状态误差控制器中引入非线性幂指数函数,使系统运算变得更加简单.仿真结果表明所设计的控制器具有良好的动态性能和较强的鲁棒性,即本文所设计的系统是可行的.     

惯性串联系统的自抗扰控制

针对非线性不确定惯性串联系统的控制问题,提出了惯性串联型扩张状态观测器（Extended state observer,ESO）,使其可直接对惯性串联系统的扩张状态进行估计,同时把被控对象的极点配置到期望位置,在此基础上提出了适合惯性串联系统的自抗扰控制（Active disturbance rejection control,ADRC）方法,该惯性串联型ADRC方法可以充分利用被控对象的已有知识.论文还给出了惯性串联型ADRC和基于扰动观测器（Disturbance observer,DOB）的控制方法之间的联系,指出它们具有相同的三自由度（three-degree of freedom control,3-DOF）控制系统结构和模块功能,都能实现对系统期望模型以外的总扰动进行估计和补偿.仿真结果表明,所提出的方法是有效的,惯性串联型ESO能实现系统总扰动的估计,惯性串联型ADRC能使系统输出能很好地跟踪系统参考输入.     

An integrated approach to hypersonic entry attitude control

This paper presents an integrated approach based on dynamic inversion(DI)and active disturbance rejection control(ADRC)to the entry attitude control of a generic hypersonic vehicle(GHV).DI is frstly used to cancel the nonlinearities of the GHV entry model to construct a basic attitude controller.To enhance the control performance and system robustness to inevitable disturbances,ADRC techniques,including the arranged transient process(ATP),nonlinear feedback(NF),and most importantly the extended state observer(ESO),are integrated with the basic DI controller.As one primary task,the stability and estimation error of the second-order nonlinear ESO are analyzed from a brand new perspective:the nonlinear ESO is treated as a specifc form of forced Li′enard system.Abundant qualitative properties of the Li′enard system are utilized to yield comprehensive theorems on nonlinear ESO solution behaviors,such as the boundedness,convergence,and existence of periodic solutions.Phase portraits of ESO estimation error dynamics are given to validate our analysis.At last,three groups of simulations,including comparative simulations with modeling errors,Monte Carlo runs with parametric uncertainties,and a six degrees-of-freedom reference entry trajectory tracking are executed,which demonstrate the superiority of the proposed integrated controller over the basic DI controller.     

Active disturbance rejection control for power plant with a single loop

The cascade proportional‐integral‐derivative (PID) control method is widely used in power plant control field. In this paper, an active disturbance rejection control (ADRC) for a power plant with a single loop is introduced for eliminating the shortcomings of the cascade PID control method. The proposed controller based on the ADRC method consists of a tracking differentiator (TD), an extended state observer (ESO) and a nonlinear combination of errors. In this approach, the processes with higher orders, uncertainties and unmodeled dynamics are viewed as lower‐ordered systems with general disturbances, and the general disturbances are estimated by ESO, and then actively compensated. Besides, only one measured output is needed in the proposed method instead of two or three in the cascade PID control method. Some simulation studies compared with the regular cascade PID control method show the proposed method has better performance beyond the regular cascade PID control method. Copyright © 2010 John Wiley and Sons Asia Pte Ltd and Chinese Automatic Control Society     

永磁直线电机基于ESO的速度辨识与控制

运用自抗扰控制技术,分别对永磁同步直线电机的直轴电流id和动子速度口设计了控制器．直轴电流的白抗扰控制器除完成对id控制外,还要借助于控制器中的扩张状态观测器(ESO),完成对动子速度的辨识．速度的辨识信号作为速度环自抗扰控制器的反馈信号,从而可设计出一种新型的无速度传感器永磁直线电机的控制系统．由于采用基于过程误差的非线性控制律,观测器受电机参数的影响极小,具有算法简单、辨识精度高等优点。     

快速路交通密度的自抗扰控制器设计及不同扰动情况下的性能评价

本文针对快速路主道交通密度的控制问题,提出了一种新的自抗扰匝道调节方法.该方法包括跟踪微分器(TD)、扩展状态观测器(ESO)和非线性输出误差反馈控制律(NLOEF)3个部分.通过微分跟踪环节安排的过渡过程,可有效降低系统的超调;而系统外部不确定性可通过ESO估计,并将估计信息用于NLOEF更新控制信号.本文分别基于宏观MATLAB和微观PARAMICS平台进行了仿真研究,验证了所提出方法抑制不同类型外部扰动的有效性.     

Extended state observer for uncertain lower triangular nonlinear systems

The extended state observer (ESO) is a key part of the active disturbance rejection control approach, a new control strategy in dealing with large uncertainty. In this paper, a nonlinear ESO is designed for a kind of lower triangular nonlinear systems with large uncertainty. The uncertainty may come from unmodeled system dynamics and external disturbance. We first investigate a nonlinear ESO with high constant gain and present a practical convergence. Two types of ESO are constructed with explicit error estimations. Secondly, a time varying gain ESO is proposed for reducing peaking value near the initial time caused by constant high gain approach. The numerical simulations are presented to show visually the peaking value reduction. The mechanism of peaking value reduction by time varying gain approach is analyzed.     

光伏三相并网系统的自抗扰控制

光伏三相并网发电系统是一个典型非线性系统,受电网和外部环境的影响,系统存在许多不确定性干扰.本文以三相光伏并网发电系统为对象,利用自抗扰控制器的扩张状态观测器,对系统模型中的不确定因素和外部干扰进行动态观测,设计一自抗扰控制器,使系统具有较好的适应能力,并对系统进行了仿真研究.结果表明所设计的控制器具有良好鲁棒性和较好的动、静态特性.     

Active disturbance rejection control approach to stabilization of lower triangular systems with uncertainty

In this paper, we apply the active disturbance rejection control (ADRC) to stabilization for lower triangular nonlinear systems with large uncertainties. We first design an extended state observer (ESO) to estimate the state and the uncertainty, in real time, simultaneously. The constant gain and the time‐varying gain are used in ESO design separately. The uncertainty is then compensated in the feedback loop. The practical stability for the closed‐loop system with constant gain ESO and the asymptotic stability with time‐varying gain ESO are proven. The constant gain ESO can deal with larger class of nonlinear systems but causes the peaking value near the initial stage that can be reduced significantly by time‐varying gain ESO. The nature of estimation/cancelation makes the ADRC very different from high‐gain control where the high gain is used in both observer and feedback. Copyright © 2015 John Wiley & Sons, Ltd.     

Altitude control for flexible wing unmanned aerial vehicle based on active disturbance rejection control and feedforward compensation

For achieving the accurate trajectory tracking of the flexible wing unmanned aerial vehicle in the complicated missions, especially the vertical component, a feedforward compensation unit–based active disturbance rejection control (ADRC) is proposed. In ADRC, the internal dynamics and complicated influence of the total disturbance will be estimated and dynamically compensated by extended state observer (ESO). It puts a very high request on the observation ability of ESO with the unpredictable external disturbance, complex internal coupling influence, and the strong nonlinear characteristic of the proposed system. For this reason, by deeply analyzing the model of this system, the varying attitude influence on the altitude control will be deduced. Then, this influence will be compensated previously by a feedforward compensation unit. Through the previous compensation of the calculable part of the internal dynamics and total disturbance, the burden of ESO can be reduced largely. In this way, it improves the control effect of the ADRC with better observation precision of ESO. After that, based on the hardware‐in‐the‐loop simulation, the effectiveness of the proposed method is verified completely with the complicated flight missions. The robustness of the control effect and observation ability of ESO are also verified by the Monte Carlo simulation. At last, the results of actual flight experiment prove the advancement and practicability of the proposed ADRC method.     

板宽板厚多变量系统的自抗扰控制

针对精轧板宽板厚多变量系统具有强耦合、不确定性、大时滞、干扰因素多、非线性等特点,应用ADRC静态解耦和ESO动态解耦技术,给出了一种全新的多变量ADRC设计及实现方案。解耦后各通道的ADRC可分别按常规的单变量时滞系统来设计。为满足快速性要求,各通道的ADRC改由ESO、NF两部分组成,而且这两部分没有采用常规的非线性函数,而是改用线性函数。改进后的ADRC由Simulink编程实现。仿真结果表明这种方法的有效性。     

基于神经网络的非线性扩张状态观测器

自抗扰控制方法是一种新型的非线性设计方法,在自抗扰控制器中主要存在着确定待定参数的问题;非线性扩张状态观测器是自抗扰控制器的核心,在研究非线性扩张观测器中的参数整定问题时,将神经网络的思想引入参数整定,提出了基于神经网络的非线性扩张状态观测器的设计方法,运用该方法可以对任意阶的非线性扩张状态观测器进行参数设计;大量仿真算例表明,设计出的观测器具有良好的鲁棒性,有一定工程应用参考价值.     

结晶器多变量耦合系统的自抗扰控制

主要研究新颖实用非线性自抗扰控制算法,在结晶器多变量耦合系统中的应用.自抗扰控制主要特性是实时估计对象模型摄动和外扰的总和作用量,并在控制信号中补偿掉,实现不确定性强非线性对象的实时动态反馈线性化.结合控制对象,建立了结晶器多变量耦合自抗扰控制系统.数值仿真试验表明自抗扰耦合控制的协调性、自适应跟随性和抗干扰性优于传统的PID解耦控制.     

On ADRC for non-minimum phase systems: canonical form selection and stability conditions

Active disturbance rejection control (ADRC), as proposed by Prof. Jingqing Han, reduces first the plant dynamics to its canonical form, normally in the form of cascade integrators, for which the standard controller can be employed to meet the design specifications. This paper concerns with the selection of the canonical form for non-minimum phase systems. In particular, it is shown that, by employing the well known controllable canonical form, the uncertainties of such systems can be divided into two terms in the state space model, one in the control channel and the other in the output channel. The necessary and sufficient condition is obtained for the stability of the closed-loop system with the proposed canonical form and ADRC. Also, by showing the necessity of the detectability of the extended system as well as certain information of the systemˉs “zeros”, we present the fundamental guidelines of design ADRC for non-minimum phase uncertain systems.     

无人直升机航向自抗扰控制

针对无人直升机系统航向通道扰动大等问题,本文设计了一种自抗扰控制算法来实现其高性能控制.首先分析了航向通道的动态模型,并通过数学变换,将其转化为一类二阶系统;在此基础上,本文设计了适用于无人机航向通道的自抗扰控制策略,它由跟踪微分器、扩展状态观测器、控制器3个环节构成.本文对所设计的自抗扰控制策略进行了仿真和实验测试,并与常见的串级控制方法进行了对比分析.仿真与实验结果表明:这种自抗扰控制策略具有对扰动抑制能力强、控制精度高等优点,其控制性能明显优于常规的串级比例–积分–微分控制方法.     

高动态离心机系统的自抗扰控制设计

针对传统PID在控制高速精密离心机系统时难以满足其高动态过程的要求,对系统目标过渡过程进行安排并设计了自抗扰控制器.所提出的自抗扰控制器包括3个部分:跟踪微分器、扩张状态观测器和误差反馈控制器.由于离心机在启动和制动阶段,系统状态会经历一个快速变化的过程,所以在离心机系统动态变化阶段采用跟踪微分器对目标函数进行过渡过程安排,防止系统出现过大超调;并且设计了扩张状态观测器对系统未知干扰进行估计和补偿;补偿后采用误差反馈控制器实现离心机系统高动态过程的跟踪控制.最后通过对自抗扰控制进行参数整定,使得系统满足所提出的各项性能指标要求.仿真结果验证了相比于传统PID控制,所提出的自抗扰控制器在超调量,调节时间以及稳态控制精度等性能指标上具有优越性.     

基于最小拍观测器的自抗扰控制器设计与性能分析

自抗扰控制器设计中,扩张状态观测器需要较高的观测带宽,才能更快的观测出状态变量.本文采用最小拍观测器,使得其具有最快的观测速度.以2阶系统为例,得到了离散系统下,基于最小拍观测器的自抗扰控制器的等价复合控制模型,其开环补偿器等价为超前校正器.仿真结果表明,基于最小拍观测器的自抗扰控制器可以最快的观测出系统状态变量,且控制器带宽的选取一般应小于采样周期的倒数.由于不再需要设计观测器带宽,从而简化了参数设计.     

基于ESO的船舶航向鲁棒自适应控制

针对具有内部未建模动态和外部不确定扰动的水面船舶设计一种鲁棒自适应航向控制器,并同时解决转向过程中的漂角补偿问题.基于二阶非线性Nomoto模型和一阶漂角模型,建立非积分链结构的漂角-航向非线性状态空间模型,将航向控制系统未建模动态与外部不确定扰动合并为复合扰动,应用扩张状态观测器估计模型中的未测量状态和系统复合扰动.基于Lyapunov稳定性理论和自适应反步法设计航向状态反馈控制规律,为避免反步法控制过程中的微分爆炸问题,采用动态面控制技术获取虚拟控制信号的近似导数.所提出的扩张状态观测器和航向控制算法能够保证闭环系统内所有误差信号一致最终有界,提高航向保持和转向过程中的航向跟踪精度.仿真结果验证了所提出的航向控制规律的有效性.     

含有非匹配干扰和未知动态的非仿射系统滑模控制算法

针对含有非匹配干扰和未知动态的非仿射系统控制问题,提出了一种基于扩张状态观测器(ESO)的改进滑模控制(SMC)方案.本文首先利用扩张状态观测器,将原系统转变为一个包含干扰的二阶积分级联系统,使含有未知动态的非仿射系统控制器设计问题转化为二阶积分级联系统的控制器设计问题,从而使得控制器在设计过程中不需要对对象模型完全已...