CN114326406A - Coordination control method based on vector machine online identification prediction - Google Patents

Coordination control method based on vector machine online identification prediction Download PDF

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CN114326406A
CN114326406A CN202111669703.XA CN202111669703A CN114326406A CN 114326406 A CN114326406 A CN 114326406A CN 202111669703 A CN202111669703 A CN 202111669703A CN 114326406 A CN114326406 A CN 114326406A
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杜鸿飞
贾峰生
刘建辉
王建
吕建
张钦
李晓军
***
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Shanxi Century Pilot Power Science And Technology Co ltd
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Abstract

The invention belongs to the field of automatic control of thermal power generating units, and particularly relates to a coordination control method based on vector machine online identification prediction; the technical scheme is as follows: s1, acquiring and processing the online identification model data; s2, structural design and parameter optimization of the online identification model; s3, designing and calculating the output of the prediction controller; s4, repeating the steps from S1 to S3 at the next time point K + 1; the thermal power generating unit coordination control method solves the problem of mismatch between the transfer function model parameters and the actual object model, and fundamentally improves the control quality of a coordination control system in the process of participating in peak shaving of the thermal power generating unit.

Description

Coordination control method based on vector machine online identification prediction
Technical Field
The invention belongs to the field of automatic control of thermal power generating units, and particularly relates to a coordination control method based on vector machine online identification prediction.
Background
With the increasingly prominent global energy crisis and environmental protection problems, the global power development is moving towards the direction of low-carbon development, and in recent years, new energy is developed in China on a large scale, and in order to solve the problem of power generation and grid connection of a new energy unit, the participation of a thermal power unit in power grid deep peak shaving has become a normalized requirement.
In the peak shaving process of the thermal power generating unit, the response speed of the thermal power generating unit is greatly limited due to the differentiated dynamic response characteristics of the two sides of the boiler and the steam turbine, and a new control strategy research needs to be carried out for improving the response speed of the thermal power generating unit to the middle-shaving AGC instruction and improving the economy of the thermal power generating unit.
In the unit variable load process, on one hand, the characteristics of a controlled object in the unit furnace coordination control system continuously change, and the existing transfer function model parameters identified based on the rated working condition are mismatched with an actual object model, so that the control quality of the coordination control system is deteriorated; on the other hand, the response deviation of the unit in the variable load process is aggravated by the conventional fixed parameter PID control strategy, and in conclusion, under the existing control strategy, a satisfactory control effect is difficult to obtain in the unit deep peak shaving process.
Disclosure of Invention
The invention overcomes the defects in the prior art, and provides the thermal power unit coordination control method which can ensure that the thermal power unit boiler coordination system has better control quality and robustness in the unit wide load peak shaving process by using the support vector machine.
In order to solve the technical problems, the invention adopts the technical scheme that: a coordination control method based on vector machine online identification prediction is realized by the following steps:
s1, acquiring and processing the online identification model data;
setting a time K aiming at a main steam pressure control loop in a coordinated control system, and acquiring the input of a control modelA data set u (k) and an output data set y (k), wherein the sampling data set is set to be L groups to obtain an identification data set TL(ii) a Identifying data set TLA rolling time window determination is employed, which is expressed as:
TL={(uk-L+1,yk-L+1),(uk-L+2,yk-L+2),...,(uk,yk)},u∈R,y∈R
normalizing input data and output data used for model identification to an interval of [ -1,1] by adopting the following expression:
Figure BDA0003452621310000021
in the formula, x and x' represent values before and after data normalization, respectively.
Normalizing the input data set u (k) and the output data set y (k) of the control model;
randomly dividing the normalized data set to determine a model training data set and a model verification data set;
s2, structural design and parameter optimization of the online identification model;
giving initial values of a support vector machine model parameter hyperparametric error penalty factor gamma and a Gaussian kernel width parameter sigma;
searching optimal values of a parameter penalty factor gamma and a Gaussian kernel width parameter sigma by using the training data set and adopting a genetic algorithm, and verifying the generalization capability of the model through the verification data set;
s3, designing and calculating the output of the prediction controller;
setting a prediction time domain P and a control time domain M, and calculating the output of a prediction model;
calculating the error e between the system output value and the model output valuem(k);
Using said error em(k) Feedback correction is carried out on the output of the prediction model to obtain a corrected output value of the prediction model;
calculating a control sequence according to a quadratic optimization target of the output error and the control increment;
and S4, repeating the steps from S1 to S3 at the next time point K + 1.
The online identification model in the step S2 adopts a least square support vector machine model, and the calculation formula of the least square support vector machine model is as follows:
for a given datum D { (x)i,yi):i=1,2,...,l},
Wherein x isi∈RnIs an n-dimensional input vector, yiE is R as a target output vector;
by non-linearly mapping phi (x), yi=WTφ(xi)+b,W∈Rn、b∈R (1-1);
According to the principle of solving the target and minimizing the structural risk, the following conditions are satisfied in the above formula (1-1):
|yi-WTφ(xi)-b|≤X
Figure BDA0003452621310000022
defining an error loss function as a quadratic term of the error
Figure BDA0003452621310000023
The above formula (1-2) can be represented as:
Figure BDA0003452621310000024
wherein gamma is the error penalty factor (1-3);
optimizing the error problem:
Figure BDA0003452621310000031
in the formula, alphaiAnd e.g. R is a Lagrange multiplier, and the above formula (1-4) is optimized to obtain:
Figure BDA0003452621310000032
Figure BDA0003452621310000033
Figure BDA0003452621310000034
Figure BDA0003452621310000035
eliminating W, e, the following matrix equation can be obtained:
Figure BDA0003452621310000036
wherein:
y=[y1,y2,...,yl]T
l=[1,1,...,1]T∈Rl
α=[α12,...,αl]
Ω={Ωij}l×lij=φT(xi)φ(xj)=K(xi,xj)
where Ω is a symmetric matrix and K (,) is a kernel function.
The least squares support vector machine prediction function is represented as:
Figure BDA0003452621310000037
the radial basis function, as a kernel function in the prediction function, is expressed as follows:
Figure BDA0003452621310000041
where σ is a gaussian kernel width parameter.
In the process of searching the optimal values of the parameter penalty factor gamma and the Gaussian kernel width parameter sigma by the genetic algorithm, the fitness function is as follows:
Figure BDA0003452621310000042
the evaluation function of the generalization ability of the model adopts root mean square error and is expressed as follows:
Figure BDA0003452621310000043
the single-step prediction model calculation formula of the least square support vector machine at the time K in the step S3 is as follows:
ym(k+1)=fLS-SVM[yp(k),yp(k-1),u(k)] (2-1)
performing multi-step iteration on the basis of single-step prediction to realize multi-step prediction;
ym(k+j)=fLS-SVM[yp(k+j-1),yp(k+j-2),u(k+j-1)] (2-2)
j 1,2, P denotes a prediction time domain;
wherein u (k + M-1) ═ u (k + M) · u (k + P-1) (2-3)
M represents a control time domain, and M is less than or equal to P.
Calculating the error e between the system output value and the model output valuem(k),
em(k)=y(k)-ym(k) (2-4);
Using error em(k) For the predicted output ym(k + j) feedback correction is performed, and the corrected prediction model output value is expressed as follows:
yp(k+j)=ym(k+j)+he(k),j=1,2,...,P (2-5)
in the formula, h is an error correction coefficient;
finally, calculating a control sequence according to the quadratic optimization target of the output error and the control increment;
the quadratic objective function of the rolling optimization is expressed as follows:
Figure BDA0003452621310000044
in the formula, λiNon-negative weighting coefficient, y, for the control quantityr(k + i) is a reference trajectory;
the reference trajectory is generally defined as an exponential curve, expressed as follows:
Figure BDA0003452621310000051
in the formula (I), the compound is shown in the specification,
Figure BDA0003452621310000052
representing a smoothing factor, r representing an input to the system;
at the current k moment, a set of optimal control sequences is found from the allowable interval of the controlled variable by a quadratic optimization objective function
U, U ═ U (k), U (k + 1.., U (k + M-1) ], minimizes the objective function J.
The constraint of the equations (1-3) is yi=WTφ(xi)+b+ei,i=1,2,...,l。
Compared with the prior art, the invention has the beneficial effects that:
1. the thermal power generating unit coordinated control method solves the problem that the control quality of a coordinated control system is poor due to mismatching of the transfer function model parameters and the actual object model, and fundamentally improves the control quality of the coordinated control system in the process that the thermal power generating unit participates in peak shaving.
2. The method has the characteristics of small modeling sample, nonlinearity and simple calculation of the support vector machine, realizes online correction of the prediction model based on the genetic algorithm, and realizes the control optimization of the whole working condition of the unit.
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The invention is further described below with reference to the accompanying drawings.
Fig. 1 is a control schematic block diagram of the present invention.
Detailed Description
As shown in fig. 1, step one: data acquisition and processing for online identification models
And acquiring input and output data of the control model aiming at a main steam pressure control loop in the coordinated control system.
Let the current time point be k time point, and the input and output of the model are respectively represented by u (k) and y (k). And determining a model identification data set by adopting a rolling time window, and if a sampling data set is an L set, representing the identification data set as follows:
TL={(uk-L+1,yk-L+1),(uk-L+2,yk-L+2),...,(uk,yk)},u∈R,y∈R
normalizing the collected data set in the rolling time window, wherein the input and output data used by model identification are normalized to the range of [ -1,1] by adopting the following expression:
Figure BDA0003452621310000053
in the formula, x and x' represent values before and after data normalization, respectively.
And randomly dividing the normalized data set to determine a model training data set and a model verification data set. And randomly disordering the sequence pointed by the sample data set to generate a new sequence number, and sequentially selecting a training set and a verification set which meet the set number of samples from the new sequence number sample set.
Step two: and (5) carrying out online identification model structure design and parameter optimization.
In the method, an online identification model adopts a least square support vector machine model with strong generalization capability based on a small sample, and the least square support vector machine model is designed as follows:
for a given datum D { (x)i,yi) I 1, 2.. gtorel } wherein, xi∈RnIs an n-dimensional input vector, yiAnd e.R is the target output vector. And transforming the nonlinear estimation problem into a high-dimensional feature space linear function estimation problem by mapping the input vector from the input space to the feature space through nonlinear mapping phi (x), wherein the linear function is expressed as follows:
yi=WTφ(xi)+b,W∈Rn,b∈R (1-1)
according to the principle of solving the target and minimizing the structured risk, the following conditions are satisfied by the above formula:
|yi-WTφ(xi)-b|≤X
Figure BDA0003452621310000061
defining an error loss function as a quadratic term of the error
Figure BDA0003452621310000062
The above formula can be represented as
Figure BDA0003452621310000063
Wherein gamma is an error penalty factor (1-3);
the equality constraints of the above equation are: y isi=WTφ(xi)+b+ei,i=1,2,...,l
Solving the optimization problem by using a Lagrange method, wherein the Lagrange function is quoted as follows:
Figure BDA0003452621310000064
in the formula, alphaiE, taking R as Lagrange multiplier, and optimizing the formula to obtain:
Figure BDA0003452621310000065
Figure BDA0003452621310000066
Figure BDA0003452621310000067
Figure BDA0003452621310000071
eliminating W, e, the following matrix equation can be obtained:
Figure BDA0003452621310000072
wherein:
y=[y1,y2,...,yl]T
l=[1,1,...,1]T∈Rl
α=[α12,...,αl]
Ω={Ωij}l×lij=φT(xi)φ(xj)=K(xi,xj)
where Ω is a symmetric matrix and K (,) is a kernel function.
The least squares support vector machine prediction function is represented as:
Figure BDA0003452621310000073
the radial basis function is used herein as a kernel function in the prediction function, and is expressed as follows:
Figure BDA0003452621310000074
where σ is a gaussian kernel width parameter.
In a support vector machine model, an error penalty factor gamma and a Gaussian kernel width parameter sigma greatly influence the performance of the model, a training data set is utilized, a genetic algorithm is adopted to search the optimal values of the two parameters, and the generalization capability of the model is verified through a verification data set.
In the genetic algorithm parameter optimizing process, the fitness function adopts the following form:
Figure BDA0003452621310000075
the evaluation function of the generalization ability of the model adopts root mean square error and is expressed as follows:
Figure BDA0003452621310000081
step three: predictive controller design and output calculation
The output of the predictive model is first calculated. In the control method, a least square support vector machine model is used as a prediction model, and a single-step prediction model mathematical expression based on the least square support vector machine at the time k is as follows:
ym(k+1)=fLS-SVM[yp(k),yp(k-1),u(k)] (2-1)
and performing multi-step iteration on the basis of single-step prediction to realize multi-step prediction.
ym(k+j)=fLS-SVM[yp(k+j-1),yp(k+j-2),u(k+j-1)] (2-2)
j 1,2, P denotes a prediction time domain;
wherein u (k + M-1) ═ u (k + M) · u (k + P-1) (2-3)
M represents a control time domain, and M is less than or equal to P.
Then calculating the error e between the system output value and the model output valuem(k),em(k)=y(k)-ym(k)。
Using the error pair to predict output ym(k + j) feedback correction is performed, and the corrected prediction model output value is expressed as follows:
yp(k+j)=ym(k+j)+he(k),j=1,2,...,P
in the formula, h is an error correction coefficient;
and finally, calculating a control sequence according to the quadratic optimization target of the output error and the control increment.
The quadratic objective function of the rolling optimization is expressed as follows:
Figure BDA0003452621310000082
in the formula, λiNon-negative weighting coefficient, y, for the control quantityr(k + i) is a reference trajectory.
The reference trajectory is generally defined as an exponential curve, expressed as follows:
Figure BDA0003452621310000083
in the formula (I), the compound is shown in the specification,
Figure BDA0003452621310000084
representing the smoothing factor and r representing the input to the system.
At the current time k, a set of optimal control sequences U is found from the control quantity tolerance interval by using a quadratic optimization objective function, wherein the optimal control sequences U are [ U (k), U (k + 1..), U (k + M-1) ] enable the objective function J to be minimum.
Step four: and returning to the step one when the next time point k +1 is the time point.
The above embodiments are merely illustrative of the principles of the present invention and its effects, and do not limit the present invention. It will be apparent to those skilled in the art that modifications and improvements can be made to the above-described embodiments without departing from the spirit and scope of the invention. Accordingly, it is intended that all equivalent modifications or changes be made by those skilled in the art without departing from the spirit and technical spirit of the present invention, and be covered by the claims of the present invention.

Claims (6)

1. A coordination control method based on vector machine online identification prediction is characterized by comprising the following steps:
s1, acquiring and processing the online identification model data;
setting a time K aiming at a main steam pressure control loop in a coordinated control system, acquiring an input data set u (K) and an output data set y (K) of the control model, setting a sampling data set into an L group, and obtaining an identification data set TL
Normalizing the input data set u (k) and the output data set y (k) of the control model;
randomly dividing the normalized data set to determine a model training data set and a model verification data set;
s2, structural design and parameter optimization of the online identification model;
giving initial values of a support vector machine model parameter hyperparametric error penalty factor gamma and a Gaussian kernel width parameter sigma;
searching optimal values of a parameter penalty factor gamma and a Gaussian kernel width parameter sigma by using the training data set and adopting a genetic algorithm, and verifying the generalization capability of the model through the verification data set;
s3, designing and calculating the output of the prediction controller;
setting a prediction time domain P and a control time domain M, and calculating the output of a prediction model;
calculating the error e between the system output value and the model output valuem(k);
Using said error em(k) Feedback correction is carried out on the output of the prediction model to obtain a corrected output value of the prediction model;
calculating a control sequence according to a quadratic optimization target of the output error and the control increment;
and S4, repeating the steps from S1 to S3 at the next time point K + 1.
2. The method as claimed in claim 1, wherein the online identification model in step S2 adopts a least square support vector machine model, and the calculation formula of the least square support vector machine model is as follows:
for a given datum D { (x)i,yi):i=1,2,...,l},
Wherein x isi∈RnIs an n-dimensional input vector, yiE is R as a target output vector;
by non-linearly mapping phi (x), yi=WTφ(xi)+b,W∈Rn、b∈R (1-1);
According to the principle of solving the target and minimizing the structural risk, the following conditions are satisfied in the above formula (1-1):
|yi-WTφ(xi)-b|≤X
Figure FDA0003452621300000011
defining an error loss function as a quadratic term of the error
Figure FDA0003452621300000029
The above formula (1-2) can be represented as:
Figure FDA0003452621300000021
wherein gamma is the error penalty factor (1-3);
optimizing the error problem:
Figure FDA0003452621300000022
in the formula, alphaiAnd e.g. R is a Lagrange multiplier, and the above formula (1-4) is optimized to obtain:
Figure FDA0003452621300000023
Figure FDA0003452621300000024
Figure FDA0003452621300000025
Figure FDA0003452621300000026
eliminating W, e, the following matrix equation can be obtained:
Figure FDA0003452621300000027
wherein:
y=[y1,y2,...,yl]T
l=[1,1,...,1]T∈Rl
α=[α12,...,αl]
Ω={Ωij}l×lij=φT(xi)φ(xj)=K(xi,xj)
where Ω is a symmetric matrix and K (,) is a kernel function.
The least squares support vector machine prediction function is represented as:
Figure FDA0003452621300000028
the radial basis function, as a kernel function in the prediction function, is expressed as follows:
Figure FDA0003452621300000031
where σ is a gaussian kernel width parameter.
3. The coordination control method based on vector machine online identification prediction as claimed in claim 2, wherein in the process of searching the optimal values of the parameter penalty factor γ and the gaussian kernel width parameter σ by the genetic algorithm, the fitness function is as follows:
Figure FDA0003452621300000032
the evaluation function of the generalization ability of the model adopts root mean square error and is expressed as follows:
Figure FDA0003452621300000033
4. the method as claimed in claim 1, wherein the calculation formula of the single-step prediction model of the least-squares support vector machine at time K in step S3 is as follows:
ym(k+1)=fLS-SVM[yp(k),yp(k-1),u(k)] (2-1)
performing multi-step iteration on the basis of single-step prediction to realize multi-step prediction;
ym(k+j)=fLS-SVM[yp(k+j-1),yp(k+j-2),u(k+j-1)] (2-2)
j 1,2, P denotes a prediction time domain;
wherein u (k + M-1) ═ u (k + M) · u (k + P-1) (2-3)
M represents a control time domain, and M is less than or equal to P.
5. The method of claim 4, wherein the error e between the system output value and the model output value is calculatedm(k),
em(k)=y(k)-ym(k) (2-4);
Using error em(k) For the predicted output ym(k + j) feedback correction is performed, and the corrected prediction model output value is expressed as follows:
yp(k+j)=ym(k+j)+he(k),j=1,2,...,P (2-5)
in the formula, h is an error correction coefficient;
finally, calculating a control sequence according to the quadratic optimization target of the output error and the control increment;
the quadratic objective function of the rolling optimization is expressed as follows:
Figure FDA0003452621300000041
in the formula, λiNon-negative weighting coefficient, y, for the control quantityr(k + i) is a reference trajectory;
the reference trajectory is generally defined as an exponential curve, expressed as follows:
Figure FDA0003452621300000042
in the formula (I), the compound is shown in the specification,
Figure FDA0003452621300000043
representing a smoothing factor, r representing an input to the system;
at the current time k, a set of optimal control sequences U is found from the control quantity tolerance interval by using a quadratic optimization objective function, wherein the optimal control sequences U are [ U (k), U (k + 1..), U (k + M-1) ] enable the objective function J to be minimum.
6. The method for coordination control based on vector machine online identification prediction as claimed in claim 2, wherein the constraint condition of formula (1-3) is yi=WTφ(xi)+b+ei,i=1,2,...,l。
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