矿热炉电极调节系统的双闭环自抗扰控制

对矿热炉电极系统提出了一种自抗扰控制策略的控制方法。设计了一种不依赖于对象模型的电极自抗扰控制器,并对其参数进行了整定,自抗扰控制器的扩张状态观测器可以实时观测系统状态和扩张状态,从而实现全状态反馈及系统不确定性和外扰的补偿控制。该系统与传统的单闭环恒流控制系统比较,增加了电极位置环。仿真实验表明,该控制系统不仅具有较强的鲁棒性,对内外干扰具有较强的抑制能力,更具有较优的动态性能。     

模糊控制器在带钢活套控制中的应用

莱钢轧钢厂在带钢生产中，以模糊控制器代替ＰＩ调节器，对活套进行控制。文章介绍了模糊控制器的原理，设计方法，控制流程及应用效果等。     

集总干扰下六旋翼飞行器的轨迹跟踪控制

针对复杂集总干扰下六旋翼飞行器轨迹跟踪控制问题,给出了混合积分反步法控制与线性自抗扰控制的控制算法. 首先,通过牛顿-欧拉方程建立六旋翼飞行器的非线性动力学模型,并剖析系统输入输出的数学关系. 其次,根据六旋翼飞行器动力学模型的特点,将其分为位置与姿态两个控制环. 位置环采用积分反步法控制理论设计控制器,通过引入积分项来提高系统的抗干扰能力,消除轨迹跟踪的静态误差;姿态环采用线性自抗扰控制技术设计控制器,通过线性扩张观测器估计和补偿集总干扰影响,提高系统的鲁棒性. 最后,通过2组仿真算例和1组飞行试验验证了本文所提飞行控制算法的有效性. 研究结果表明:该控制算法对集总干扰有较好的抑制作用,能够使六旋翼飞行器既快又稳地跟踪上参考轨迹,具有一定的工程应用价值.      

GKD2型内燃机车司控器试验电路

以前对司控器逻辑关系的检测都是采取手工检测方法,即用万用表测量触头是处于闭合还是处于分断状态,存在着检测速度慢,检测效果不好及检测不可靠等缺点.为此设计了为辅修时对GKD2型内燃机车司机控制器动作进行检测的试验电路,并描述了试验电路的工作原理、主要功能及其实现方法.     

基于无线传感器扭矩检测的轧机扭振前馈控制

 针对轧机轧辊反复正反转咬钢抛钢受到突然强有力的冲击时扭振现象极为严重的情况,研究采用扭矩无线传感器实时采回负载干扰值,解决了现有的扭振抑制方法中采用扭振预估器计算扭振时容易出现偏差的问题;利用前馈能在扰动发生时提前做出干扰补偿的原理,在大型轧机交交变频调速系统定子转矩电流与转速双闭环的基础上,在转矩控制器的输入端加入负载扭矩扰动补偿,提前控制定子电流转矩分量而达到控制扭振的目的,并用Simulink对上述过程进行仿真。结果表明：基于无线传感的扭振前馈抑制方式对扭振的控制效果非常明显,几乎可以彻底消除扭振,更贴近实际。     

中厚板轧机自动厚度控制系统的鲁棒性研究

中厚板轧机液压厚度控制系统是一个具有抗扰性的控制系统,但系统响应速度过慢,轧机出口有较大厚度偏差。基于传递函数理论,建立了液压AGC系统的动态数学模型,对带有常规PID控制器和模糊自校正PID控制器的厚度控制系统进行了仿真研究。仿真结果表明,模糊自校正PID控制器具有更好的控制效果,系统具有更强的鲁棒性。     

Vibration Control of Wind-Excited Tall Buildings Using Sliding Mode Fuzzy Control

A sliding mode fuzzy control (SMFC) is proposed to design a controller for the third-generation benchmark problem on wind-excited buildings. A distinctive feature in vibration control of large civil infrastructure is the existence of large disturbances, such as wind, earthquake, and sea wave forces. Those disturbances govern the behavior of the structure; however, they cannot be precisely measured, especially for the case of wind excitations. Since the structural accelerations are measured only at a limited number of locations without the measurement of the wind forces, the structure of the conventional control may have the feedback loop only. The general structure of the SMFC, proposed herein, is composed of a compensation part and a convergent part. The compensation part prevents the system from diverging, and the convergent part directs the system to the sliding surface. The compensation part uses not only the structural response measurement but also the disturbance measurement, so the SMFC has a feedback loop and a feedforward loop. To realize the virtual feedforward loop for the wind-induced vibration control, a disturbance estimation filter is introduced. The structure of the filter is constructed based on an autoregressive model for the stochastic wind force. This filter estimates the wind force at each time instance based on the measured structural responses and the stochastic information of the wind force. For verification of the proposed algorithm, numerical simulation is carried out on the benchmark problem for wind-excited buildings. The results indicate that the present control algorithm is efficient for reducing the wind-induced vibration.     

Model and Control of Flexible Multibody Satellite

In order to estimate total disturbances including parametric uncertainties, unmodeled dynamics, and external disturbances, and achieve the dynamic feedback compensation of the estimated total disturbances, we design a double closed loop attitude active disturbance rejection controller (ADRC). By taking flexible vibrations of solar panels and a flexible antenna as an external disturbance, and using only the estimated transformation matrix of control input, a simplified dynamic model has been used to replace the accurate dynamic model of a rigid body in a flexible multibody satellite dynamics model. Simulation results indicate that the attitude ADRC designed still has the original dynamic response when large external disturbance acts on the system. Therefore, we come to the conclusion that the ADRC designed can be used to solve the problem of control systems with uncertainties in the process of modeling different flexible multibody systems.     

前馈厚度控制的外部自激励定量反馈调节

分析了板材轧制过程中出口厚度变化的成因.将不确定扰动的影响归结为轧机刚度系数摄动和轧件塑性系数摄动,建立了双摄动厚度控制模型.综合考虑轧机系统的外部不确定扰动,针对轧制道次间的不确定性,在频域内将板厚信息转化为轧机系统边界性能指标,设计抑制前馈扰动的外部自激励定量反馈控制器.仿真实验表明,设计的控制器能有效抑制轧制过程中的外部扰动,具有良好的鲁棒性能,并能直观保证系统调整时的鲁棒稳定性,适于工业生产.      

基于神经元模糊控制器的过热汽温控制

工业控制领域的普通模糊控制器都存在着控制精度不理想的问题，为此提出一种把神经元与模糊控制器相结合的方法，使控制系统控制精度得到提高．并应用于发电厂的主气压控制系统中，效果良好。     

集成PWM控制器在挤塑机上的使用

本文介绍了利用集成控制器SG1525组成PWM控制器在挤塑机上的使用,并分析介绍该系统的应用方式及技术特点.     

基于定量反馈控制的冷连轧机卷取张力控制器的设计

采用定量反馈理论(QFT),设计具有参数不确定性的卷取张力的鲁棒控制系统,给出了定量反馈理论的基本原理和设计方法。针对系统的不确定性采用QFT设计反馈控制器和前置滤波器,仿真结果表明,当系统参数发生变化时,系统仍然能够保持良好的跟踪性能。此外,与PID控制效果的对比结果表明,QFT控制对外部扰动也具有良好的抗干扰性。     

嵌入式液压控制器的实现

嵌入式液压控制器是在国内某大型钢铁公司的技术改造中开发的。控制器硬件采用德国MEN公司的A12高性能单板计算机,软件使用了VxWorks嵌入式实时操作系统。本文给出了液压控制器的设计方案,并介绍了VxWorks下多任务和精确周期的实现方法。     

基于有限时间滤波控制的电机驱动系统结构/控制一体化设计

针对电机驱动系统进行了基于有限时间控制器的结构/控制一体化设计.针对电机驱动系统跟踪控制问题,采用有限时间收敛方法设计了跟踪控制器.考虑系统状态信息不可测的情况,设计了有限时间滤波控制器,在估计系统速度信息的同时实现了有限时间跟踪控制.为进一步提升系统控制性能,考虑结构与控制之间存在的耦合问题,对电机驱动系统进行结构/控制一体化设计.首先针对电机驱动系统设计了同时考虑结构优化和控制器优化的一体化性能指标.所设计一体化性能指标能够在满足控制性能要求的同时,得到所能驱动的最大负载.同时优化系统的结构参数与控制器参数能够使控制系统达到全局最优,从而取得良好的控制效果.随后,采用嵌套优化策略对电机驱动系统的一体化设计问题进行简化,采用自适应步长的布谷鸟搜索算法对控制器参数优化问题进行求解,得到了一体化最优解.通过数值仿真验证了所提方法的有效性.      

基于CAN总线的分布式铝电解控制系统

介绍了基于CAN总线的分布式铝电解控制系统的设计和实现方法,给出了CAN总线的硬件接口电路设计和槽控机逻辑电路结构。     

基于智能控制的直进式拉丝机控制系统

针对直进式拉丝机的特点,设计研制了智能控制器,保持拉丝机拉拔过程中的反拉力恒定。结果表明,该系统能有效抑制反拉力的波动,实时检测出拉模的磨损。     

工控机在预熔颗粒保护渣物料配比中的应用

介绍了以研华工控机为核心，实现固体状物料自动称量配比系统的软、硬件设计及提高称量精度所采取的措施，经实践验证方案可行。     

集散型控制系统在黄磷电热炉生产中的应用

本文介绍了单回路调节器,并详细阐述了集散型控制系统在黄磷电热炉生产中的应用。     

Robust Backstepping Sliding Mode Attitude Tracking and Vibration Damping of Flexible Spacecraft with Actuator Dynamics

This paper presents a dual-stage control system design method for the attitude tracking control and vibration stabilization of a spacecraft with flexible appendages embedded with piezoceramics as sensor and actuator. In this design approach, attitude control system and vibration suppression were designed separately using a lower order model. Based on the sliding mode control (SMC) and backstepping technique, a new attitude controller in the form of the input voltage of the reaction wheel is derived to control the attitude motion of a spacecraft, in which the reaction wheel dynamics is also considered from the real applications point of view. Here the sliding mode technique is used to achieve an asymptotic convergence of the attitude and angular velocity tracking errors in the presence of parameter variation and disturbance by providing a virtual torque input at the rigid body while the backstepping technique is used to regulate the input voltage of the actuator to provide the required torque. The asymptotic stability is shown using a Lyapunov analysis. Furthermore, an adaptive version of the proposed attitude control law is also designed for adapting the unknown upper bounds of the lumped disturbance so that the limitation of knowing the bound of the disturbance in advance is released. For actively suppressing the induced vibration, strain rate feedback control methods are presented by using piezoelectric materials as additional sensors and actuators bonded on the surface of the flexible appendages. The performances of the hybrid control schemes are assessed in terms of attitude tracking and level of vibration reduction in comparison to the proportional-derivative and conventional SMC. Both analytical and numerical results are presented to show the theoretical and practical merit of this hybrid approach.     

可编程序控制器系统的设计

贵冶二期、三期工程使用了大量的可编程序控制器 ,本文从设计的角度阐述了可编程序控制器的使用