CN108573278A - A kind of multiple operating modes process modal identification method - Google Patents
A kind of multiple operating modes process modal identification method Download PDFInfo
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Abstract
The invention discloses a kind of multiple operating modes process modal identification methods, belong to automatic measurement technique field, including off-line training and online modal identification two parts;Off-line training calculates the weight of each mode using historic training data, and it is obtained by orthogonal transformation so that the conditional sampling degree of variable is maximum under different operating modes, its orthogonal matrix is obtained by numerical method solution optimization problem, Bayes classifier is trained using the off-line data after transformation, utilizes kernel function estimation conditional probability density function;Online modal identification carries out orthogonal transformation to sample first, and calculate the conditional probability density function under each operating mode, mode classification is determined by maximization conditional probability density function, compared with classical way naive Bayesian, it is independent it is assumed that having higher classification accuracy that institute's extracting method of the present invention relaxes data qualification.
Description
Technical field
The invention belongs to automatic measurement technique fields, and in particular to a kind of multiple operating modes process modal identification method.
Background technology
In actual industrial system, operating mode switching can occur because of several factors for the operating mode of production process.These factors include
The change of system feeding, the change of reactant ingredient, different production technologies, the variation of external environmental factor and production target
Change etc..In some cases, the change of process operating mode has label, as production target change or factory in
Operative employee changes charging or change set temperature etc. according to instruction.But the change of some operating modes is not no label, such as external rings
The variation of border factor.It is subsequent in this case it is necessary to measurement data analyze the mode of simultaneously on-line identification process
Process monitoring provides basis.
Invention content
For the above-mentioned technical problems in the prior art, the present invention proposes a kind of multiple operating modes process modal identification side
Method, reasonable design overcome the deficiencies in the prior art, have good effect.
To achieve the goals above, the present invention adopts the following technical scheme that:
A kind of multiple operating modes process modal identification method, specifically comprises the following steps:
Step 1:Off-line training is as follows:
Step 1.1:The historical data under d kind difference operating modes is collected, training dataset is established
Wherein, m is number of probes, niFor the number of samples under i-th of operating mode;
Step 1.2:Calculate the priori weight beta of each operating modei:
Step 1.3:Data under i-th of operating mode are pre-processed:
Wherein,Represent the measurement vector of k-th of sampling instant under i-th of operating mode;For corresponding zero averaging
Vector;μ{i}For the sample average of i-th of floor data, calculated by formula (3):
Step 1.4:Calculate the sample covariance Q of i-th of floor data{i}:
Wherein,ForTransposition;
Step 1.5:Enable j=1, and step-up error threshold value ∈;
Step 1.6:K=0 is enabled, random vector is generatedAnd it normalizes:
Wherein,It indicates2 norms;
Step 1.7:If j>1, then in formula (5)It is orthogonalized processing:
Wherein, wiIt is the i-th row of orthogonal matrix W to be optimized;Middle k is the kth step of iterative calculation, and T is transposition;
Step 1.8:Calculate function g (wj):
Wherein, wjIt is the jth row of orthogonal matrix W to be optimized;
Step 1.9:Calculate g (wj) Jacobian matrix J (wj):
Wherein, I is unit battle array;
Step 1.10:Newton iteration:
Step 1.11:If j>1, in formula 9It is orthogonalized processing:
Step 1.12:To in formula 10It is normalized:
Step 1.13:In judgment formula (11), ifEnable k=k+1, and jump to step 1.10 into
Row Newton iteration;
Step 1.14:J=j+1 is enabled, if j≤m, jumps to step 1.6;
Step 1.15:Orthogonal matrix W is obtained, the data of different operating modes are handled as follows:
z{i}=WTx{i}(27);
Wherein, z{i}For the data vector under i-th of operating mode;
Step 1.16:Kernel function K and bandwidth h is set;
Step 1.17:To i=1 ..., d, j=1 ..., m estimate conditional probability density function:
Wherein,Indicate z under i-th of operating mode{i}The value of k-th of sampling instant of j-th of sensor;
Step 2:Online modal identification
Step 2.1:Following orthogonal transformation is carried out to sample data:
zk=WTxk(29);
Step 2.2:To i=1 ..., d, design conditions probability density
Step 2.3:Mode classification is determined by maximal condition probability density:
Advantageous effects caused by the present invention:
It is compared based on Nae Bayesianmethod with classical, this method improves variable to measurand using orthogonal transformation
Conditional sampling degree so that be unsatisfactory for the measurement data of conditional independence assumption originally and to a certain extent more meet to assume.
Simultaneously as the shape feature of orthogonal transformation not change data, will not destroy the feature conducive to classification.This method can be used for multiplexing
The modal identification problem of condition process can relatively accurately judge unknown operating mode, facilitate subsequent fault detection and diagnosis.
Description of the drawings
Fig. 1 is the flow chart of off-line training according to an embodiment of the invention;
Fig. 2 is the flow chart of online modal identification according to an embodiment of the invention.
Specific implementation mode
Below in conjunction with the accompanying drawings and specific implementation mode invention is further described in detail:
A kind of multiple operating modes process modal identification method, specifically comprises the following steps:
Step 1:Off-line training, flow are as shown in Figure 1;It is as follows:
Step 1.1:The historical data under d kind difference operating modes is collected, training dataset is established
Wherein, m is number of probes, niFor the number of samples under i-th of operating mode;
Step 1.2:Calculate the priori weight beta of each operating modei:
Step 1.3:Data under i-th of operating mode are pre-processed:
Wherein,Represent the measurement vector of k-th of sampling instant under i-th of operating mode;For corresponding zero averaging
Vector;μ{i}For the sample average of i-th of floor data, calculated by formula (3):
Step 1.4:Calculate the sample covariance Q of i-th of floor data{i}:
Wherein,ForTransposition;
Step 1.5:Enable j=1, and step-up error threshold value ∈;
Step 1.6:K=0 is enabled, random vector is generatedAnd it normalizes:
Wherein,It indicates2 norms;
Step 1.7:If j>1, then in formula (5)It is orthogonalized processing:
Wherein, wi is the i-th row of orthogonal matrix W to be optimized;Middle k is the kth step of iterative calculation, and T is transposition;
Step 1.8:Calculate function g (wj):
Wherein, wjIt is the jth row of orthogonal matrix W to be optimized;
Step 1.9:Calculate g (wj) Jacobian matrix J (wj):
Wherein, I is unit battle array;
Step 1.10:Newton iteration:
Step 1.11:If j>1, in formula 9It is orthogonalized processing:
Step 1.12:To in formula 10It is normalized:
Step 1.13:In judgment formula (11), ifEnable k=k+1, and jump to step 1.10 into
Row Newton iteration;
Step 1.14:J=j+1 is enabled, if j≤m, jumps to step 1.6;
Step 1.15:Orthogonal matrix W is obtained, the data of different operating modes are handled as follows:
z{i}=WTx{i}(42);
Wherein, z{i}For the data vector under i-th of operating mode;
Step 1.16:Kernel function K and bandwidth h is set;
Step 1.17:To i=1 ..., d, j=1 ..., m estimate conditional probability density function:
Wherein,Indicate z under i-th of operating mode{i}The value of k-th of sampling instant of j-th of sensor;
Step 2:Online modal identification, flow are as shown in Figure 2;It is as follows:
Step 2.1:Following orthogonal transformation is carried out to sample data:
zk=WTxk(44);
Step 2.2:To i=1 ..., d, design conditions probability density
Step 2.3:Mode classification is determined by maximal condition probability density:
This method and Nae Bayesianmethod are applied to tool there are three in the modal identification of the multiple linear process of operating mode,
Compare its classification accuracy.Use 1000 Monte Carlo Experiments.This method and Nae Bayesianmethod classification accuracy it is equal
Value is respectively 0.931 and 0.879.Compared with Nae Bayesianmethod, the method for the present invention improves mode in multiple operating modes process and distinguishes
The accuracy rate of knowledge demonstrates the validity of proposition method of the present invention.
Certainly, above description is not limitation of the present invention, and the present invention is also not limited to the example above, this technology neck
The variations, modifications, additions or substitutions that the technical staff in domain is made in the essential scope of the present invention should also belong to the present invention's
Protection domain.
Claims (1)
1. a kind of multiple operating modes process modal identification method, which is characterized in that specifically comprise the following steps:
Step 1:Off-line training is as follows:
Step 1.1:The historical data under d kind difference operating modes is collected, training dataset is established
Wherein, m is number of probes, niFor the number of samples under i-th of operating mode;
Step 1.2:Calculate the priori weight beta of each operating modei:
Step 1.3:Data under i-th of operating mode are pre-processed:
Wherein,Represent the measurement vector of k-th of sampling instant under i-th of operating mode;For corresponding zero averaging to
Amount;μ{i}For the sample average of i-th of floor data, calculated by formula (3):
Step 1.4:Calculate the sample covariance Q of i-th of floor data{i}:
Wherein,ForTransposition;
Step 1.5:Enable j=1, and step-up error threshold value ∈;
Step 1.6:K=0 is enabled, random vector is generatedAnd it normalizes:
Wherein,It indicates2 norms;
Step 1.7:If j>1, then in formula (5)It is orthogonalized processing:
Wherein, wiIt is the i-th row of orthogonal matrix W to be optimized;Middle k is the kth step of iterative calculation, and T is transposition;
Step 1.8:Calculate function g (wj):
Wherein, wjIt is the jth row of orthogonal matrix W to be optimized;
Step 1.9:Calculate g (wj) Jacobian matrix J (wj):
Wherein, I is unit battle array;
Step 1.10:Newton iteration:
Step 1.11:If j>1, in formula 9It is orthogonalized processing:
Step 1.12:To in formula 10It is normalized:
Step 1.13:In judgment formula (11), ifK=k+1 is enabled, and jumps to step 1.10 and carries out newton
Iteration;
Step 1.14:J=j+1 is enabled, if j≤m, jumps to step 1.6;
Step 1.15:Orthogonal matrix W is obtained, the data of different operating modes are handled as follows:
z{i}=WTx{i}(12);
Wherein, z{i}For the data vector under i-th of operating mode;
Step 1.16:Kernel function K and bandwidth h is set;
Step 1.17:To i=1 ..., d, j=1 ..., m estimate conditional probability density function:
Wherein,Indicate z under i-th of operating mode{i}The value of k-th of sampling instant of j-th of sensor;
Step 2:Online modal identification
Step 2.1:Following orthogonal transformation is carried out to sample data:
zk=WTxk(14);
Step 2.2:To i=1 ..., d, design conditions probability density
Step 2.3:Mode classification is determined by maximal condition probability density:
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US20020180586A1 (en) * | 2001-05-30 | 2002-12-05 | Kitson Frederick Lee | Face and environment sensing watch |
US20030018459A1 (en) * | 2001-06-20 | 2003-01-23 | O' Riordan Donald J. | Method for debugging of analog and mixed-signal behavioral models during simulation |
CN104019799A (en) * | 2014-05-23 | 2014-09-03 | 北京信息科技大学 | Relative orientation method by using optimization of local parameter to calculate basis matrix |
CN105486474A (en) * | 2015-11-30 | 2016-04-13 | 上海卫星工程研究所 | Satellite flexible part on-orbit modal identification realization system and method |
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