CN110007605A - A robust predictive control method for a repulsive magnetic levitation device - Google Patents

A robust predictive control method for a repulsive magnetic levitation device Download PDF

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CN110007605A
CN110007605A CN201910419115.7A CN201910419115A CN110007605A CN 110007605 A CN110007605 A CN 110007605A CN 201910419115 A CN201910419115 A CN 201910419115A CN 110007605 A CN110007605 A CN 110007605A
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周锋
朱培栋
谢明华
陈俊东
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Abstract

本发明公开了一种排斥式磁悬浮装置的鲁棒预测控制方法,采集排斥式磁悬浮装置的输入电压、输出距离的历史数据N组,建立非线性模型;基于非线性模型,建立排斥式磁悬浮装置的凸多面体状态空间模型;基于所述凸多面体状态空间模型,获得排斥式磁悬浮装置鲁棒控制的优化目标函数,求解所述目标函数,得到t时刻作用于排斥式磁悬浮装置绕组的输入电压值。本发明在控制器设计中考虑了系统建模误差和不确定干扰的影响,是一种鲁棒稳定、适用性强的控制方法。

The invention discloses a robust predictive control method for a repelling magnetic levitation device, which collects N groups of historical data of the input voltage and output distance of the repulsive magnetic levitation device, and establishes a nonlinear model; Convex polyhedron state space model; based on the convex polyhedron state space model, obtain the optimal objective function of the robust control of the repulsive magnetic levitation device, solve the objective function, and obtain the input voltage value acting on the winding of the repulsive magnetic levitation device at time t. The present invention considers the influence of system modeling error and uncertain disturbance in the controller design, and is a robust, stable and highly applicable control method.

Description

一种排斥式磁悬浮装置的鲁棒预测控制方法A robust predictive control method for a repulsive magnetic levitation device

技术领域technical field

本发明涉及自动控制领域,特别是涉及一种针对排斥式磁悬浮装置的鲁棒预测控制方法。The invention relates to the field of automatic control, in particular to a robust predictive control method for a repelling magnetic levitation device.

背景技术Background technique

磁悬浮技术是一种机电一体化技术,其通过利用高频磁场在金属表面形成涡流,进而产生洛伦磁力使得金属设备悬浮起来,有效避免了设备之间的接触、减小了相互摩擦,具有广阔的应用前景。磁悬浮系统是一个集电磁力、气隙、电流等控制为一体的复杂非线性系统,实际应用中难以获取其精确的数学模型。基于数据驱动的辨识建模方法是一类不依赖于系统物理机理的数学建模方法,仅利用对象的输入输出数据来进行建模,被广泛应用于复杂非线性系统的建模中。Magnetic levitation technology is an electromechanical integration technology. It uses a high-frequency magnetic field to form eddy currents on the metal surface, thereby generating Loren magnetic force to suspend metal equipment, effectively avoiding contact between equipment and reducing mutual friction. application prospects. The magnetic levitation system is a complex nonlinear system that integrates the control of electromagnetic force, air gap, and current. It is difficult to obtain its accurate mathematical model in practical applications. The data-driven identification modeling method is a kind of mathematical modeling method that does not depend on the physical mechanism of the system. It only uses the input and output data of the object for modeling, and is widely used in the modeling of complex nonlinear systems.

PID控制器因其控制算法结构简单,并且不依赖于被控对象精确的数学模型,在磁悬浮控制中得到了较广泛的应用。但PID控制器针对复杂非线性对象的全局控制特性较差,特别是对于稳定性要求极高的磁悬浮球控制系统,在临近边界的较大范围极易出现悬浮球瞬间失控跌落的情况。线性二次型调节器是一种基于被控对象状态空间模型的控制算法,也较广泛的应用于复杂系统的控制中。但因其高度依赖被控对象模型的精确性,其控制的鲁棒性和稳定性还是有待提高。模型预测控制是一种在工业过程控制实践中产生的先进计算机控制算法,被广泛应用于复杂工业系统的控制中。通过对已有文献的检索发现,专利“一种基于模型预测控制的风电磁悬浮偏航电机控制方法”(申请号:201810076334.5),提出了一种基于磁悬浮系统物理机理模型设计的预测控制方法。专利“一种磁悬浮球位置控制方法”(申请号:201510180614.7),提出了一种基于带函数权系数型自回归模型的预测控制方法。但上述两类方法在预测控制器设计过程中并未考虑系统建模误差和不确定干扰的影响,算法的稳定性和鲁棒性无法得到有效保证。同时,专利“201510180614.7”在建立用于后续预测控制器设计的系统状态空间模型过程中,直接用系统当前时刻的状态量来近似替代系统未来的状态量,对系统未来的状态空间模型进行了直接单点线性化近似处理,该方法本身会对模型的精度造成较大影响。PID controller has been widely used in magnetic levitation control because of its simple control algorithm structure and no dependence on the precise mathematical model of the controlled object. However, the PID controller has poor global control characteristics for complex nonlinear objects, especially for the magnetic levitation ball control system with extremely high stability requirements. The linear quadratic regulator is a control algorithm based on the state space model of the controlled object, and is also widely used in the control of complex systems. However, because it is highly dependent on the accuracy of the controlled object model, the robustness and stability of its control still need to be improved. Model predictive control is an advanced computer control algorithm produced in the practice of industrial process control, and is widely used in the control of complex industrial systems. Through the retrieval of existing literature, it is found that the patent "A Wind Electromagnetic Suspension Yaw Motor Control Method Based on Model Predictive Control" (application number: 201810076334.5) proposes a predictive control method based on the design of the physical mechanism model of the magnetic levitation system. The patent "A Magnetic Levitation Ball Position Control Method" (application number: 201510180614.7) proposes a predictive control method based on an autoregressive model with a function weight coefficient. However, the above two methods do not consider the influence of system modeling errors and uncertain disturbances in the process of predictive controller design, and the stability and robustness of the algorithms cannot be effectively guaranteed. At the same time, the patent "201510180614.7" in the process of establishing the system state space model for the subsequent predictive controller design, directly uses the state quantity of the system at the current moment to approximate the future state quantity of the system, and directly analyzes the future state space model of the system. Single-point linearization approximation, the method itself will have a greater impact on the accuracy of the model.

发明内容SUMMARY OF THE INVENTION

本发明所要解决的技术问题是,针对现有技术不足,提供一种排斥式磁悬浮装置的鲁棒预测控制方法,考虑系统建模误差和不确定干扰的影响,提高控制方法的鲁棒性和适用性。The technical problem to be solved by the present invention is to provide a robust predictive control method for a repelling magnetic levitation device in view of the deficiencies of the prior art, which improves the robustness and applicability of the control method by considering the influence of system modeling errors and uncertain disturbances. sex.

为解决上述技术问题,本发明所采用的技术方案是:一种排斥式磁悬浮装置的鲁棒预测控制方法,包括以下步骤:In order to solve the above-mentioned technical problems, the technical scheme adopted in the present invention is: a robust predictive control method of a repelling magnetic levitation device, comprising the following steps:

1)采集排斥式磁悬浮装置的输入电压、输出距离的历史数据N组,建立如下非线性模型:1) Collect N groups of historical data of the input voltage and output distance of the repelling magnetic levitation device, and establish the following nonlinear model:

其中,y(t)为t时刻排斥式磁悬浮装置地球仪底部与红外反射位置传感器之间的距离,即排斥式磁悬浮装置的输出量;u(t)为t时刻排斥式磁悬浮装置控制板施加给绕组的电压大小,即排斥式磁悬浮装置的输入量;ξ(t+1)为包含建模误差和不确定扰动的项,且|ξ(t+1)|≤1;{a0,t,a1,t,b1,t,a2,t,b2,t}为关于y(t)的逆二次函数型时变系数,且||·||2代表二范数运算;非线性模型的相关参数均通过R-SNPOM优化方法优化计算得到;Among them, y(t) is the distance between the bottom of the globe of the repulsive magnetic levitation device and the infrared reflection position sensor at time t, that is, the output of the repulsive magnetic levitation device; u(t) is the time t The control board of the repulsive magnetic levitation device applies to the windings , that is, the input of the repelling magnetic levitation device; ξ(t+1) is a term that includes modeling errors and uncertain disturbances, and |ξ(t+1)|≤1; {a 0,t ,a 1,t ,b 1,t ,a 2,t ,b 2,t } are time-varying coefficients of inverse quadratic function with respect to y(t), and ||·|| 2 represents two-norm operation; nonlinear The relevant parameters of the model All are optimized and calculated by the R-SNPOM optimization method;

2)基于上述非线性模型,建立排斥式磁悬浮装置的凸多面体状态空间模型;2) Based on the above nonlinear model, establish a convex polyhedron state space model of the repelling magnetic levitation device;

3)基于所述凸多面体状态空间模型,获得排斥式磁悬浮装置鲁棒控制的优化目标函数,求解所述目标函数,得到t时刻作用于排斥式磁悬浮装置绕组的输入电压值。3) Based on the convex polyhedron state space model, obtain the optimal objective function of the robust control of the repulsive magnetic levitation device, solve the objective function, and obtain the input voltage value acting on the winding of the repulsive magnetic levitation device at time t.

步骤2)的具体实现过程包括:The specific implementation process of step 2) includes:

1)定义排斥式磁悬浮装置的输入增量和输出增量如下:1) Define the input increment and output increment of the repelling magnetic levitation device as follows:

其中,y(t+j)为t+j时刻排斥式磁悬浮装置的输出;yset为t时刻排斥式磁悬浮装置的期望值;u(t+j)为t+j时刻排斥式磁悬浮装置的输入,u(t+j-1)为t+j-1时刻排斥式磁悬浮装置的输入;j为小于或等于零的整数;Among them, y(t+j) is the output of the repulsive magnetic levitation device at time t+j; y set is the expected value of the repulsive magnetic levitation device at time t; u(t+j) is the input of the repulsive magnetic levitation device at time t+j, u(t+j-1) is the input of the repelling magnetic levitation device at time t+j-1; j is an integer less than or equal to zero;

2)排斥式磁悬浮装置的一步向前预测多项式模型结构如下:2) One-step forward prediction polynomial model of repulsive magnetic levitation device The structure is as follows:

其中,θ(t)为推导过程中产生的中间量;ξ(t+1|t)为包含系统建模误差和不确定干扰的量,且|ξ(t+1|t)|≤1;where θ(t) is the derivation The intermediate quantity generated in the process; ξ(t+1|t) is the quantity including the system modeling error and uncertain disturbance, and |ξ(t+1|t)|≤1;

3)基于上述一步向前预测多项式模型和系统的输入增量、输出增量的定义,推导出排斥式磁悬浮装置的多项式模型对应的状态空间模型如下:3) Based on the above-mentioned one-step forward prediction polynomial model and the definition of the input increment and output increment of the system, the state space model corresponding to the polynomial model of the repulsive magnetic levitation device is derived as follows:

其中,排斥式磁悬浮装置的一步向前预测状态向量X(t+1|t)的系数矩阵At,Bt和X(t|t)分别为t时刻非线性模型计算出的参数和状态;为t时刻排斥式磁悬浮装置的输入增量;Ξ(t)的变化范围在向量之间;At+g|t,Bt+g|t为排斥式磁悬浮装置未来g步向前预测状态向量X(t+g+1|t)的系数矩阵。Among them, the coefficient matrix A t , B t and X(t|t) of the one-step forward prediction state vector X(t+1|t) of the repelling magnetic levitation device are the parameters and states calculated by the nonlinear model at time t, respectively; is the input increment of the repelling magnetic levitation device at time t; the variation range of Ξ(t) is in the vector and between; A t+g|t , B t+g|t are the coefficient matrix of the future g-step forward prediction state vector X(t+g+1|t) of the repulsive magnetic levitation device.

所述系数矩阵At+g|t,Bt+g|t变化范围在如下凸多面体范围内:The coefficient matrices A t+g|t and B t+g|t vary in the range of the following convex polyhedron:

其中,{λt+g|t,μ|μ=1,2,3,4}为凸多面体的线性系数;凸多面体的4个顶点为(A1,B1),(A2,B2),(A3,B3)和(A4,B4),且:Among them, {λ t+g|t, μ |μ=1, 2, 3, 4} is the linear coefficient of the convex polyhedron; the four vertices of the convex polyhedron are (A 1 , B 1 ), (A 2 , B 2 ), (A 3 , B 3 ) and (A 4 , B 4 ), and:

其中,分别为关于y(t)的函数的最大值和最小值;分别为关于y(t)的函数的最大值和最小值。in, and respectively as a function of y(t) the maximum and minimum values; and respectively as a function of y(t) the maximum and minimum values.

步骤3)中,所述优化目标函数设计如下:In step 3), the optimization objective function is designed as follows:

其中,I2为单位阵;X(t+g|t)为t时刻模型预测的t+g步系统状态量;为t时刻预测的t+g步排斥式磁悬浮装置输入控制增量;g≥1,Ft为t时刻排斥式磁悬浮装置未来的反馈控制率。in, I 2 is the unit matrix; X(t+g|t) is the t+g step system state quantity predicted by the model at time t; Input control increment for the t+g step repelling magnetic levitation device predicted at time t; g≥1, F t is the future feedback control rate of the repelling magnetic levitation device at time t.

通过以下不等式组求解所述优化目标函数:The optimization objective function is solved by the following set of inequalities:

其中,符号*代表矩阵的对称结构;{Qμ|μ=1,2,3,4}为求解上述不等式组,即凸优化问题而产生的中间矩阵变量;γ0+γ为上述凸优化问题的优化目标值{(Aμ,Bμ)|μ=1,2,3,4}为凸多面体模型的顶点;γ、γ0、{Y,G,Qμ|μ=1,2,3,4}和均为最小化变量γ0+γ求解过程中得到的中间变量;在求解最小化问题时,优化函数根据上述不等式组约束条件自动寻找满足使的γ0+γ最小的中间变量γ、γ0、{Y,G,Qμ|μ=1,2,3,4}和当上述不等式组有可行解时,则优化过程结束,此时得到的即为t时刻作用于磁悬浮系统绕组的输入电压值。Among them, the symbol * represents the symmetric structure of the matrix; {Q μ |μ=1, 2, 3, 4} is the intermediate matrix variable generated by solving the above inequality group, that is, the convex optimization problem; γ 0 +γ is the above convex optimization problem The optimization objective value of {(A μ ,B μ )|μ=1,2,3,4} is the vertex of the convex polyhedron model; γ, γ 0 , {Y,G,Q μ |μ=1,2,3 ,4} and are intermediate variables obtained during the solution process of minimizing variables γ 0 +γ; in solving the minimization problem When , the optimization function automatically finds the intermediate variables γ, γ 0 , {Y,G,Q μ |μ=1,2,3,4} that satisfy the minimum γ 0 When the above inequality group has a feasible solution, the optimization process ends, and the obtained That is, the input voltage value acting on the winding of the magnetic suspension system at time t.

与现有技术相比,本发明所具有的有益效果为:本发明考虑到实际磁悬浮系统无法避免的会受到外界干扰的影响,本发明利用一种基于数据驱动的时变系数准线性回归结构模型对磁悬浮系统进行建模,在建模过程中考虑了系统的建模误差和外界不确定干扰的影响。为了克服一般预测控制方法难以保证算法稳定性和鲁棒性的缺点,本发明基于建立的磁悬浮系统时变系数回归模型提出了一种可通过求解线性矩阵不等式组实现的鲁棒预测控制方法,在控制器设计中考虑了系统建模误差和不确定干扰的影响,是一种鲁棒稳定、适用性强的控制方法。Compared with the prior art, the present invention has the following beneficial effects: the present invention takes into account that the actual magnetic levitation system is unavoidably affected by external interference, and the present invention utilizes a data-driven time-varying coefficient quasi-linear regression structure model. The magnetic levitation system is modeled, and the modeling error of the system and the influence of external uncertain interference are considered in the modeling process. In order to overcome the shortcomings that the general predictive control method is difficult to guarantee the stability and robustness of the algorithm, the present invention proposes a robust predictive control method that can be realized by solving the linear matrix inequality group based on the established time-varying coefficient regression model of the magnetic levitation system. The influence of system modeling errors and uncertain disturbances is considered in the design of the controller, which is a robust, stable and applicable control method.

附图说明Description of drawings

图1为本发明所针对的排斥式磁悬浮装置结构图。FIG. 1 is a structural diagram of a repelling magnetic levitation device aimed at by the present invention.

具体实施方式Detailed ways

本发明所针对的排斥式磁悬浮装置结构如图1所示,其中:1为地球仪外壳(半径为20厘米),3为方柱形磁铁,2为地球仪外壳1与方柱形磁铁3之间支架,4为红外反射位置传感器(型号为ST178H),5为铁心(截面半径为2.5厘米),6为绕组(匝数为3500),7为基于单片机的控制电路板。该系统通过调节控制板7施加给绕组6的电压大小(输出电压范围为0V~20V),来控制地球仪2底部与红外反射位置传感器4之间的距离(控制距离范围为5cm~25cm)。本发明所述一种排斥式磁悬浮装置的鲁棒控制方法的具体实施例包含以下步骤:The structure of the repelling magnetic levitation device targeted by the present invention is shown in Figure 1, wherein: 1 is the globe shell (radius is 20 cm), 3 is a square cylindrical magnet, and 2 is a bracket between the globe shell 1 and the square cylindrical magnet 3 , 4 is the infrared reflection position sensor (model ST178H), 5 is the iron core (section radius is 2.5 cm), 6 is the winding (the number of turns is 3500), and 7 is the control circuit board based on the microcontroller. The system controls the distance between the bottom of the globe 2 and the infrared reflection position sensor 4 by adjusting the voltage applied to the winding 6 by the control board 7 (the output voltage range is 0V-20V) (the control distance is 5cm-25cm). A specific embodiment of the robust control method for a repelling magnetic levitation device according to the present invention includes the following steps:

步骤1:针对图1所示的排斥式磁悬浮装置,采集系统的输入电压、输出距离的历史数据2500组,建立系统如下非线性模型:Step 1: For the repulsive magnetic levitation device shown in Figure 1, collect 2500 sets of historical data of the input voltage and output distance of the system, and establish the following nonlinear model of the system:

上式中,y(t)为t时刻地球仪2底部与红外反射位置传感器4之间的距离,即系统的输出量;u(t)为t时刻控制板7施加给绕组6的电压大小,即系统的输入量;ξ(t+1)为包含建模误差和不确定扰动的项,且|ξ(t+1)|≤1;{a0,t,a1,t,b1,t,a2,t,b2,t}为关于y(t)的逆二次函数型时变系数,且||·||2代表二范数运算;模型的相关参数均通过R-SNPOM优化方法优化计算得到(R-SNPOM优化方法详见文献:Zeng X.,Peng H.,Zhou F.,2018,A regularized SNPOM for stableparameter estimation of RBF-AR(X)model,IEEE Transactions on Neural Networksand Learning Systems,29,No.4,779-791.),优化得到的具体参数值为: In the above formula, y(t) is the distance between the bottom of the globe 2 and the infrared reflection position sensor 4 at time t, that is, the output of the system; u(t) is the voltage applied by the control board 7 to the winding 6 at time t, that is, The input quantity of the system; ξ(t+1) is the term including modeling error and uncertain disturbance, and |ξ(t+1)|≤1; {a 0,t ,a 1,t ,b 1,t ,a 2,t ,b 2,t } is the inverse quadratic function time-varying coefficient about y(t), and ||·|| 2 represents the two-norm operation; the relevant parameters of the model All are calculated by the R-SNPOM optimization method (see the literature for the R-SNPOM optimization method: Zeng X., Peng H., Zhou F., 2018, A regularized SNPOM for stableparameter estimation of RBF-AR(X)model, IEEE Transactions on Neural Networksand Learning Systems,29,No.4,779-791.), the specific parameter values obtained by optimization are:

步骤2:基于步骤1建立的磁悬浮系统逆二次函数型时变系数回归模型(1),建立系统的凸多面体状态空间模型,具体过程如下:Step 2: Based on the inverse quadratic function time-varying coefficient regression model (1) of the magnetic levitation system established in Step 1, a convex polyhedron state space model of the system is established. The specific process is as follows:

定义磁悬浮系统的输入增量和输出增量如下:The input increment and output increment of the maglev system are defined as follows:

上式中,y(t+j)为t+j时刻系统的输出;yset∈[5,25]为t时刻系统的期望值;u(t+j)为t+j时刻系统的输入,u(t+j-1)为t+j-1时刻系统的输入;j=0,-1,-2,...。由上述定义,可推导出模型的一步向前预测结构如下:In the above formula, y(t+j) is the output of the system at time t+j; y set ∈ [5,25] is the expected value of the system at time t; u(t+j) is the input of the system at time t+j, u (t+j-1) is the input of the system at time t+j-1; j=0,-1,-2,.... From the above definition, the one-step forward prediction of the model can be derived The structure is as follows:

上式中,θ(t)为推导过程中产生的中间量,可由系统的输出期望和历史数据计算得到;ξ(t+1|t)为包含系统建模误差和不确定干扰的量,且|ξ(t+1|t)|≤1。In the above formula, θ(t) is the derivation The intermediate quantity generated in the process can be calculated from the output expectation and historical data of the system; ξ(t+1|t) is the quantity including the system modeling error and uncertain disturbance, and |ξ(t+1|t)| ≤1.

定义磁悬浮系统的状态向量如下:The state vector that defines the magnetic levitation system is as follows:

则基于上述一步向前预测多项式模型和系统的输入输出偏差量的定义,可推到出系统的多项式模型对应的状态空间模型如下:Based on the above-mentioned definition of the one-step forward prediction polynomial model and the input and output deviation of the system, the state space model corresponding to the polynomial model of the system can be deduced as follows:

上式中,系统的一步向前预测状态向量X(t+1|t)的系数矩阵At,Bt和X(t|t)分别为t时刻可通过步骤S1辨识得到的模型计算出的参数和状态;为t时刻系统的输入增量,为算法待优化的量;Ξ(t)在t时刻无法准确获得,因为Ξ(t)中包含系统的未知干扰项ξ(t+1|t),但因ξ(t+1|t)|≤1可知,Ξ(t)的变化范围在向量之间;系统未来g步向前预测状态向量X(t+g+1|t)的系数矩阵At+g|t,Bt+g|t在t时刻无法直接计算出,但其变化范围在如下凸多面体范围内:In the above formula, the coefficient matrix A t , B t and X(t|t) of the one-step forward prediction state vector X(t+1|t) of the system are calculated by the model identified by step S1 at time t, respectively. parameters and status; is the input increment of the system at time t, and is the amount to be optimized by the algorithm; Ξ(t) cannot be accurately obtained at time t, because Ξ(t) contains the unknown interference term ξ(t+1|t) of the system, but due to ξ(t+1|t)|≤1, it can be seen that the variation range of Ξ(t) is in the vector and between; the coefficient matrix A t+g|t and B t+g|t of the system’s future g step forward prediction state vector X(t+g+1|t) cannot be directly calculated at time t, but its variation range In the range of the following convex polyhedra:

上式中,{λt+g|t,μ|μ=1,2,3,4}为多面体的线性系数;多面体的4个顶点为(A1,B1),(A2,B2),(A3,B3)和(A4,B4),且In the above formula, {λ t+g|t, μ |μ=1,2,3,4} is the linear coefficient of the polyhedron; the four vertices of the polyhedron are (A 1 , B 1 ), (A 2 , B 2 ), (A 3 , B 3 ) and (A 4 , B 4 ), and

其中, 因y(t)∈[5,25],则 因此可计算出凸多面体集(9)的4个顶点(A1,B1),(A2,B2),(A3,B3)和(A4,B4)。in, Because y(t)∈[5,25], then Therefore, the 4 vertices (A 1 , B 1 ), (A 2 , B 2 ), (A 3 , B 3 ) and (A 4 , B 4 ) of the convex polyhedron set (9) can be calculated.

步骤3:基于步骤2中建立的系统凸多面体状态空间模型(7-8),本发明所述的一种针对排斥式磁悬浮装置的鲁棒控制方法的优化目标函数设计如下:Step 3: Based on the system convex polyhedron state space model (7-8) established in step 2, the optimization objective function of the robust control method for the repelling magnetic levitation device according to the present invention is designed as follows:

上式中,I为单位阵;X(t+g|t)为t时刻模型预测的t+g步系统状态量;为t时刻预测的t+g步系统输入控制增量。本发明鲁棒预测控制器的未来控制率结构设计如下:g≥1,Ft为t时刻系统未来的反馈控制率。In the above formula, I is the unit matrix; X(t+g|t) is the state quantity of the t+g step system predicted by the model at time t; Enter the control increment for the t+g step system predicted at time t. The future control rate structure design of the robust predictive controller of the present invention is as follows: g≥1, F t is the future feedback control rate of the system at time t.

基于上述设计的控制器优化目标函数,本发明所述的一种针对排斥式磁悬浮装置的鲁棒控制方法的最优控制率通过求解如下线性矩阵不等式组得到:Based on the controller optimization objective function of the above design, the optimal control rate of the robust control method for the repelling magnetic levitation device according to the present invention is obtained by solving the following linear matrix inequalities:

上式中,符号*代表矩阵的对称结构;Ft=YG-1为t时刻系统未来的反馈控制率;{Qμ|μ=1,2,3,4}为求解上述凸优化问题而产生的中间矩阵变量;γ0+γ为上述凸优化问题(12)的优化目标值,同时γ和γ0也是上述优化过程中产生的中间量;系数矩阵At、BtX(t|t)是t时刻已知的参数矩阵;{(Aμ,Bμ)|μ=1,2,3,4}为步骤2中的系统多面体模型(8)的顶点。γ、γ0、{Y,G,Qμ|μ=1,2,3,4}和均为最小化变量γ0+γ求解过程中得到的中间变量。在求解最小化问题(12)时,优化函数会根据上述不等式约束条件(13-16)自动寻找满足使的γ0+γ最小的中间变量γ、γ0、{Y,G,Qμ|μ=1,2,3,4}和当上述优化问题(12-16)有可行解时,则优化过程结束。此时,得到的即为t时刻作用于磁悬浮系统绕组的输入电压值。In the above formula, the symbol * represents the symmetric structure of the matrix; F t = YG -1 is the future feedback control rate of the system at time t; {Q μ | μ = 1, 2, 3, 4} is generated to solve the above convex optimization problem The intermediate matrix variable of X(t|t) is the known parameter matrix at time t; {(A μ ,B μ )|μ=1,2,3,4} is the vertex of the system polyhedron model (8) in step 2. γ, γ 0 , {Y, G, Q μ | μ = 1, 2, 3, 4} and Both are intermediate variables obtained during the solution process of minimizing the variable γ 0 +γ. When solving the minimization problem (12), the optimization function will automatically find the intermediate variables γ, γ 0 , {Y,G,Q μ |μ that satisfy the minimum γ 0 +γ according to the above inequality constraints (13-16) =1,2,3,4} and When the above optimization problem (12-16) has a feasible solution, the optimization process ends. At this time, the obtained That is, the input voltage value acting on the winding of the magnetic suspension system at time t.

Claims (5)

1. A robust prediction control method of a repulsive magnetic suspension device is characterized by comprising the following steps:
1) acquiring historical data N groups of input voltage and output distance of the repulsion type magnetic suspension device, and establishing a nonlinear model as follows:
wherein y (t) is the distance between the bottom of a globe of the repulsion type magnetic suspension device and the infrared reflection position sensor at the time t, namely the output quantity of the repulsion type magnetic suspension device, u (t) is the voltage applied to a winding by a control board of the repulsion type magnetic suspension device at the time t, namely the input quantity of the repulsion type magnetic suspension device, ξ (t +1) is a term containing modeling error and uncertain disturbance, and | ξ (t +1) | is less than or equal to 1; { a%0,t,a1,t,b1,t,a2,t,b2,tIs an inverse quadratic time-varying coefficient with respect to y (t), and | L | · | | survival of the electrically non-woven hair2Representing a two-norm operation; relevant parameters of non-linear modelAre obtained by optimization calculation through an R-SNPOM optimization method;
2) establishing a convex polyhedron state space model of the repelling magnetic suspension device based on the nonlinear model;
3) and obtaining an optimized objective function for the robust control of the repelling magnetic suspension device based on the convex polyhedron state space model, and solving the objective function to obtain an input voltage value acting on a winding of the repelling magnetic suspension device at the moment t.
2. The robust predictive control method for a repulsive magnetic levitation device as recited in claim 1, wherein the step 2) is implemented by the following steps:
1) the input increment and the output increment of the repulsive magnetic levitation device are defined as follows:
wherein y (t + j) is the output of the repulsive magnetic suspension device at the moment t + j; y issetThe expected value of the repulsive magnetic suspension device at the time t is shown; u (t + j) is the input of the repulsion type magnetic suspension device at the moment t + j, and u (t + j-1) is the input of the repulsion type magnetic suspension device at the moment t + j-1; j is an integer less than or equal to zero;
2) one-step forward prediction polynomial model of repelling magnetic suspension deviceThe structure is as follows:
wherein,to deriveξ (t +1| t) is the quantity containing system modeling error and uncertain disturbance, and | ξ (t +1| t) | is less than or equal to 1;
3) based on the one-step forward prediction polynomial model and the definition of the input increment and the output increment of the system, the state space model corresponding to the polynomial model of the repulsive magnetic suspension device is deduced as follows:
wherein, one of the repulsion type magnetic suspension deviceCoefficient matrix A of forward-step prediction state vector X (t +1| t)t,BtAnd X (t | t) are respectively a parameter and a state calculated by the nonlinear model at the time t;is the input increment of the repulsion type magnetic suspension device at the time t; xi (t) in a vectorAndto (c) to (d); a. thet+g|t,Bt+g|tAnd predicting a coefficient matrix of a state vector X (t + g +1| t) for the repelling magnetic suspension device in the future g steps.
3. The robust predictive control method for repelling magnetic levitation devices according to claim 2, wherein the coefficient matrix at+g|t,Bt+g|tThe variation range is within the following convex polyhedron range:
wherein, { lambda ]t+g|t,μ1,2,3,4 is the linear coefficient of the convex polyhedron; the 4 vertexes of the convex polyhedron are (A)1,B1),(A2,B2),(A3,B3) And (A)4,B4) And, and:
wherein,andare functions relating to y (t), respectivelyMaximum and minimum values of;andare functions relating to y (t), respectivelyMaximum and minimum values of.
4. The robust predictive control method for repelling magnetic levitation devices according to claim 3, wherein in step 3), the optimization objective function is designed as follows:
wherein,I2is a unit array; x (t + g | t) is the system state quantity of the step t + g predicted by the model at the moment t;inputting a control increment for the t + g step repulsion type magnetic suspension device predicted at the t moment;g≥1,Ftthe future feedback control rate of the repulsion type magnetic suspension device at the time t.
5. The robust predictive control method for repelling magnetic levitation devices as recited in claim 4, wherein the optimization objective function is solved by the following set of inequalities:
wherein, the symbol represents the symmetric structure of the matrix; { Qμ1,2,3,4 is an intermediate matrix variable generated by solving the inequality set, namely the convex optimization problem; gamma ray0+ gamma is the optimized target value { (A) of the convex optimization problemμ,Bμ) 1,2,3,4 is the vertex of the convex polyhedron model; gamma, gamma0、{Y,G,Qμ1,2,3,4 |, andare all the minimized variable gamma0+ gamma solving intermediate variables obtained in the process; in solving the minimization problemThen, the optimization function automatically searches for the gamma satisfying the constraint conditions of the inequality set0+ gamma minimum intermediate variables gamma, gamma0、{Y,G,Qμ1,2,3,4 |, andwhen the above is mentionedWhen the inequality group has feasible solution, the optimization process is ended, and the obtained solution is obtainedI.e. the value of the input voltage acting on the windings of the magnetic levitation system at time t.
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