CN108062021B - Parameter self-tuning method of SISO full-format model-free controller based on partial derivative information - Google Patents

Parameter self-tuning method of SISO full-format model-free controller based on partial derivative information Download PDF

Info

Publication number
CN108062021B
CN108062021B CN201711316965.1A CN201711316965A CN108062021B CN 108062021 B CN108062021 B CN 108062021B CN 201711316965 A CN201711316965 A CN 201711316965A CN 108062021 B CN108062021 B CN 108062021B
Authority
CN
China
Prior art keywords
siso full
format model
parameters
free controller
neural network
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201711316965.1A
Other languages
Chinese (zh)
Other versions
CN108062021A (en
Inventor
卢建刚
李雪园
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhejiang University ZJU
Original Assignee
Zhejiang University ZJU
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zhejiang University ZJU filed Critical Zhejiang University ZJU
Priority to CN201711316965.1A priority Critical patent/CN108062021B/en
Publication of CN108062021A publication Critical patent/CN108062021A/en
Application granted granted Critical
Publication of CN108062021B publication Critical patent/CN108062021B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B13/00Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
    • G05B13/02Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
    • G05B13/0205Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric not using a model or a simulator of the controlled system
    • G05B13/024Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric not using a model or a simulator of the controlled system in which a parameter or coefficient is automatically adjusted to optimise the performance

Landscapes

  • Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • Artificial Intelligence (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Evolutionary Computation (AREA)
  • Medical Informatics (AREA)
  • Software Systems (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Feedback Control In General (AREA)

Abstract

The invention discloses a parameter self-tuning method of a SISO full-format model-free controller based on partial derivative information, which utilizes the partial derivative information as the input of a BP neural network, the BP neural network carries out forward calculation and outputs parameters to be tuned of controllers such as punishment factors, step length factors and the like through an output layer, the control algorithm of the controllers is adopted to calculate and obtain the control input aiming at a controlled object, the control input is calculated and respectively aims at the gradient information of each parameter to be tuned, the value minimization of a system error function is taken as the target, a gradient descent method is adopted, the system error back propagation calculation is carried out by combining the gradient information, the hidden layer weight coefficient and the output layer weight coefficient of the BP neural network are updated on line in real time, and the gradient information is stored as the partial derivative information and is used as the input of the BP neural network at the later moment. The parameter self-tuning method of the SISO full-format model-free controller based on the partial derivative information can effectively overcome the problem of tuning of the controller parameters and achieve good control effect.

Description

Parameter self-tuning method of SISO full-format model-free controller based on partial derivative information
Technical Field
The invention belongs to the field of automatic control, and particularly relates to a parameter self-tuning method of a SISO full-format model-free controller based on partial derivative information.
Background
The model-free controller is a novel data-driven control method, does not depend on any mathematical model information of a controlled object, only depends on input and output data measured by the controlled object in real time to analyze and design the controller, is simple and clear in realization, small in calculation burden and strong in robustness, can well control an unknown nonlinear time-varying system, and has a good application prospect.
There are various implementation methods for the modeless controller, wherein a SISO (Single Input and Single Output) full-format modeless controller is one of the main implementation methods for the modeless controller. The theoretical basis of the SISO full-format model-free controller is proposed by Houzhong and Jinshangtai in the 'model-free adaptive control-theory and application' (scientific publishing agency, 2013, pages 83-84) of the Hedame, and the control algorithm is as follows:
Figure BDA0001503660040000011
wherein u (k) is the control input at time k; Δ u (k) ═ u (k) — u (k-1); Δ y (k) ═ y (k) — y (k-1); e (k) is the system error at time k;
Figure BDA0001503660040000012
is a pseudo-gradient estimate for time k,
Figure BDA0001503660040000013
is composed of
Figure BDA0001503660040000014
The ith component of (i ═ 1, …, Ly + Lu); ly is a control output linearization length constant preset in the SISO full-format model-free controller and is an integer greater than or equal to 1; lu is a control input linearization length constant preset in the SISO full-format model-free controller and is an integer greater than or equal to 1; λ is a penalty factor; rho1,…,ρLy+LuIs the step size factor.
At present, the SISO full-format modeless controller needs to rely on empirical knowledge to set a penalty factor lambda and a step factor rho in advance before actual use1,…,ρLy+LuThe values of the isoparametric parameters have not realized a penalty factor lambda and a step factor rho in the actual application process1,…,ρLy+LuAnd (4) performing online self-tuning on the equal parameters. The lack of effective parameter setting means not only makes the using and debugging process of the SISO full-format model-free controller time-consuming and labor-consuming, but also can seriously affect the control effect of the SISO full-format model-free controller sometimes, and restricts the popularization and application of the SISO full-format model-free controller.
Therefore, in order to break the bottleneck of restricting the popularization and application of the SISO full-format model-free controller, the invention provides a parameter self-tuning method of the SISO full-format model-free controller based on partial derivative information.
Disclosure of Invention
In order to solve the problems in the background art, the invention aims to provide a parameter self-tuning method of a SISO full-format model-free controller based on partial derivative information.
To this end, the above object of the present invention is achieved by the following technical solution, comprising the steps of:
step (1): determining a control output linearization length constant Ly of the SISO full-format model-free controller, wherein the Ly is an integer greater than or equal to 1; determining a control input linearization length constant Lu of the SISO full-format model-free controller, wherein the Lu is an integer greater than or equal to 1; SISO full-format modeless controller parameters include a penalty factor λ and a step factor ρ1,…,ρLy+Lu(ii) a Determining parameters to be set of a SISO full-format model-free controller, wherein the parameters to be set of the SISO full-format model-free controller are part or all of the parameters of the SISO full-format model-free controller and comprise a penalty factor lambda and a step factor rho1,…,ρLy+LuAny one or any combination of the above; determining the number of input layer nodes, the number of hidden layer nodes and the number of output layer nodes of the BP neural network, wherein the number of the output layer nodes is not less than the number of parameters to be set of the SISO full-format modeless controller; initializing a hidden layer weight coefficient and an output layer weight coefficient of the BP neural network;
step (2): initializing partial derivative information of the previous moment as the input of a BP neural network;
and (3): recording the current moment as k moment, and calculating by adopting a system error calculation function to obtain a system error of the k moment based on a system output expected value and a system output actual value, and recording as e (k);
and (4): based on the input of the BP neural network, the BP neural network carries out forward calculation, and the calculation result is output through an output layer to obtain the value of the parameter to be set of the SISO full-format model-free controller;
and (5): calculating to obtain a control input u (k) of the SISO full-format model-free controller at the time k for the controlled object by adopting a control algorithm of the SISO full-format model-free controller based on the system error e (k) obtained in the step (3) and the value of the parameter to be set of the SISO full-format model-free controller obtained in the step (4);
and (6): based on the control input u (k) obtained in the step (5), calculating gradient information of the control input u (k) at the moment k for parameters to be set of each SISO full-format model-free controller, wherein the specific calculation formula is as follows:
when the parameters to be set of the SISO full-format model-free controller comprise a penalty factor lambda and Lu is 1, the control input u (k) is the gradient information of the penalty factor lambda at the time k:
Figure BDA0001503660040000031
when the parameters to be set of the SISO full-format model-free controller comprise penalty factors lambda and Lu >1, the control input u (k) is the gradient information at the k moment aiming at the penalty factors lambda:
Figure BDA0001503660040000032
when the parameters to be set of the SISO full-format model-free controller contain step length factors rhoiAnd 1 ≦ i ≦ Ly, the control input u (k) is for the step-size factor ρiThe gradient information at time k is:
Figure BDA0001503660040000033
when the parameters to be set of the SISO full-format model-free controller contain step length factors rhoLy+1The control input u (k) is for the step-size factor pLy+1The gradient information at time k is:
Figure BDA0001503660040000034
when the parameters to be set of the SISO full-format model-free controller contain step length factors rhoiAnd i is more than or equal to Ly +2 and less than or equal to Ly + Lu and Lu>1, the control input u (k) is for the step-size factor piThe gradient information at time k is:
Figure BDA0001503660040000041
wherein Δ u (k) (u (k)) -u (k-1), Δ y (k) (y (k)) -y (k-1),
Figure BDA0001503660040000042
is a pseudo-gradient estimate for time k,
Figure BDA0001503660040000043
is composed of
Figure BDA0001503660040000044
The ith component of (i ═ 1, …, Ly + Lu);
and (7): the value minimization of a system error function is taken as a target, a gradient descent method is adopted, the gradient information obtained in the step (6) is combined, the system error back propagation calculation is carried out, and the hidden layer weight coefficient and the output layer weight coefficient of the BP neural network are updated to be used as the hidden layer weight coefficient and the output layer weight coefficient when the BP neural network carries out forward calculation at the later moment;
and (8): and (3) recording the gradient information of the parameters to be set of each SISO full-format model-free controller at the time k, which is obtained by calculation in the step (6), of the control input u (k) as the partial derivative information of the previous time in sequence, namely: when the parameters to be set of the SISO full-format model-free controller contain a penalty factor lambda, one of the gradient information at the k moment
Figure BDA0001503660040000045
One of the partial derivatives recorded as the previous time
Figure BDA0001503660040000046
When the parameters to be set of the SISO full-format model-free controller contain step length factors rhoiAnd when i is more than or equal to 1 and less than or equal to Ly + Lu, one of gradient information at the k moment
Figure BDA0001503660040000047
One of the partial derivatives recorded as the previous time
Figure BDA0001503660040000048
The partial derivative information of the previous moment is used as the input of the BP neural network when the BP neural network carries out forward calculation at the next moment;
and (9): and (e) after the control input u (k) acts on the controlled object, obtaining a system output actual value of the controlled object at the later moment, returning to the step (3), and repeating the steps (3) to (9).
While adopting the above technical scheme, the present invention can also adopt or combine the following further technical schemes:
the independent variables of the system error calculation function in the step (3) comprise a system output expected value and a system output actual value.
The systematic error calculation function in the step (3) adopts e (k) y*(k) -y (k), wherein y*(k) The system output expected value is set for the time k, and y (k) is the system output actual value obtained by sampling at the time k; or using e (k) ═ y*(k +1) -y (k), wherein y*And (k +1) is a system output expected value at the moment of k +1, and y (k) is a system output actual value obtained by sampling at the moment of k.
The independent variable of the system error function in the step (7) comprises any one or any combination of a system error, a system output expected value and a system output actual value.
The system error function in the step (7) is e2(k)+ωΔu2(k) Where e (k) is a systematic error, Δ u (k) -u (k-1), and ω is a constant equal to or greater than 0.
The parameter self-tuning method of the SISO full-format model-free controller based on the partial derivative information can realize good control effect and effectively overcome penalty factor lambda and step factor rho1,…,ρLy+LuThe difficult problem of setting needs time and labor waste.
Drawings
FIG. 1 is a functional block diagram of the present invention;
FIG. 2 is a schematic diagram of a BP neural network structure employed in the present invention;
FIG. 3 shows penalty factor λ and step size factor ρ123Meanwhile, self-setting a timing control effect graph;
FIG. 4 shows penalty factor λ and step size factor ρ123Simultaneously self-timing control input diagram;
FIG. 5 shows penalty factor λ and step size factor ρ123Meanwhile, self-adjusting a punishment factor lambda change curve;
FIG. 6 shows penalty factor λ and step size factor ρ123Step size factor p while self-aligning123A change curve;
FIG. 7 shows a penalty factor λ fixed and a step size factor ρ123A self-timing control effect graph;
FIG. 8 shows a penalty factor λ fixed and a step size factor ρ123A self-timed control input map;
FIG. 9 shows a penalty factor λ fixed and a step size factor ρ123Step factor p at self-alignment123A curve of variation.
Detailed Description
The invention is further described with reference to the following figures and specific examples.
Fig. 1 shows a schematic block diagram of the present invention. Determining a control output linearization length constant Ly of the SISO full-format model-free controller, wherein the Ly is an integer greater than or equal to 1; determining a control input linearization length constant Lu of the SISO full-format model-free controller, wherein the Lu is an integer greater than or equal to 1; SISO full-format modeless controller parameters include a penalty factor λ and a step factor ρ1,…,ρLy+Lu(ii) a Determining parameters to be set of a SISO full-format model-free controller, wherein the parameters to be set of the SISO full-format model-free controller are part or all of the parameters of the SISO full-format model-free controller and comprise a penalty factor lambda and a step factor rho1,…,ρLy+LuAny one of orAny combination thereof; in FIG. 1, the parameters to be set by the SISO full-format model-less controller are penalty factor λ and step factor ρ1,…,ρLy+Lu(ii) a Determining the number of input layer nodes, the number of hidden layer nodes and the number of output layer nodes of the BP neural network, wherein the number of the output layer nodes is not less than the number of parameters to be set of the SISO full-format modeless controller; initializing a hidden layer weight coefficient and an output layer weight coefficient of the BP neural network; the current time is recorded as the time k, firstly, the system output actual value y (k) is obtained through sampling, and the system output expected value y*(k) Taking the difference with the system output actual value y (k) as the system error e (k) at the time k, and then taking the partial derivative information at the previous time as the input of the BP neural network; the BP neural network carries out forward calculation, and the calculation result is output through an output layer to obtain the value of the parameter to be set of the SISO full-format model-free controller; then, based on the value of the system error e (k) and the value of the parameter to be set, calculating to obtain the control input u (k) of the SISO full-format model-free controller aiming at the controlled object at the time k by adopting the control algorithm of the SISO full-format model-free controller; then calculating to obtain gradient information of control input u (k) at the time k aiming at each parameter to be set; combining the gradient information, targeting a value minimization of the systematic error function, denoted e in fig. 12(k) Minimizing as a target, updating the hidden layer weight coefficient and the output layer weight coefficient of the BP neural network, and taking the updated hidden layer weight coefficient and the output layer weight coefficient as the hidden layer weight coefficient and the output layer weight coefficient when the BP neural network carries out forward calculation at the later moment; information of gradient
Figure BDA0001503660040000061
Partial derivative information recorded as previous time in sequence
Figure BDA0001503660040000071
The partial derivative information of the previous moment is used as the input of the BP neural network when the BP neural network carries out forward calculation at the next moment; after the control input u (k) acts on the controlled object, the system output actual value of the controlled object at the next moment is obtained, then the process is repeated, and the parameter self-tuning process of the SISO full-format model-free controller at the next moment based on the partial derivative information is carried out。
Fig. 2 shows a schematic structural diagram of the BP neural network adopted in the present invention. The BP neural network may have a structure in which the hidden layer is a single layer, or may have a structure in which the hidden layer is a plurality of layers. In the schematic diagram of fig. 2, for the sake of simplicity, the BP neural network adopts a structure in which the hidden layer is a single layer, that is, a three-layer network structure composed of an input layer, a single-layer hidden layer, and an output layer, the number of nodes of the input layer is set as the number of parameters to be set (the number of parameters to be set is Ly + Lu +1 in fig. 2), the number of nodes of the hidden layer is 7, and the number of nodes of the output layer is set as the number of parameters to be set (the number of parameters to be set is Ly + Lu +1 in fig. 2). Ly + Lu +1 nodes of input layer, and partial derivative information
Figure BDA0001503660040000072
Respectively correspond to each other. Ly + Lu +1 nodes of the output layer, penalty factor lambda and step factor rho1,…,ρLy+LuRespectively correspond to each other. The update process of the hidden layer weight coefficient and the output layer weight coefficient of the BP neural network specifically comprises the following steps: targeting the minimization of the value of the systematic error function, denoted by e in FIG. 22(k) And (3) aiming at the minimization, performing system error back propagation calculation by adopting a gradient descent method and combining control input u (k) respectively aiming at the gradient information of each parameter to be set at the k moment, so as to update the weight coefficient of the hidden layer and the weight coefficient of the output layer of the BP neural network.
The following is a specific embodiment of the present invention.
The controlled object is a typical nonlinear system:
Figure BDA0001503660040000073
desired value y of system output*(k) The following were used:
y*(k)=5sin((k-1)π/50)+2cos((k-1)π/20)
the value of the control output linearization length constant Ly of the SISO full-format modeless controller is usually set according to the complexity of the controlled object and the actual control effect, and is generally between 1 and 5, and an excessively large value causes a large calculation amount, so that 1 or 3 is generally adopted, and Ly is taken as 1 in the specific embodiment; the value of the control input linearization length constant Lu of the SISO full-format modeless controller is also usually set according to the complexity of the controlled object and the actual control effect, and is generally between 1 and 10, where too small will affect the control effect, and too large will result in large calculation amount, so it is usually 2, 3 or 5, and Lu is 2 in this specific embodiment.
In this particular example, a total of two sets of experimental verifications were performed.
When the first group of tests verifies, the number of nodes of the input layer and the number of nodes of the output layer of the BP neural network in the graph 2 are preset to be 4, and a penalty factor lambda and a step factor rho are set123Performing simultaneous self-tuning, controlling effect diagram, controlling input diagram, punishment factor lambda change curve and step factor rho123The variation curves are shown in fig. 3, 4, 5 and 6, respectively. The result shows that the method of the invention carries out the punishment factor lambda and the step factor rho123The method has the advantages of realizing good control effect by carrying out self-tuning at the same time, and effectively overcoming the penalty factor lambda and the step factor rho123The difficult problem of setting needs time and labor waste.
When the second group of tests are verified, the penalty factor lambda is firstly fixed to be the average value of the penalty factor lambda when the first group of tests are verified, the number of nodes of an input layer and the number of nodes of an output layer of the BP neural network in the graph 2 are preset to be 3, and then the step factor rho is subjected to123Self-tuning, control effect diagram, control input diagram, step factor rho123The change curves are shown in fig. 7, 8, and 9, respectively. The results also show that the method of the invention is implemented by applying the step factor rho when the penalty factor lambda is fixed123Self-tuning is carried out, good control effect can be realized, and the step factor rho can be effectively overcome123The difficult problem of setting needs time and labor waste.
It should be particularly noted that, in the above-described specific embodiment,outputting the system to a desired value y*(k) The difference with the actual system output value y (k) is used as the system error e (k), i.e. e (k) y*(k) -y (k), only one method of calculating a function for the systematic error; the expected value y of the system output at the moment k +1 can also be used*The difference between (k +1) and the actual system output value y (k) at time k is taken as the system error e (k), i.e. e (k) y*(k +1) -y (k); the system error calculation function may also employ other calculation methods where the independent variables include a desired system output value and an actual system output value, for example,
Figure BDA0001503660040000091
Figure BDA0001503660040000092
for the controlled object of the above embodiment, good control effects can be achieved by using the different system error calculation functions.
It should be noted that, in the above specific embodiment, the input of the BP neural network includes the partial derivative information at the previous time, but is not limited to the partial derivative information at the previous time, and for example, according to the specific situation, the input may also include information such as a desired value of system output, an actual value of system output, and the like.
More particularly, in the above embodiment, when the hidden layer weight coefficient and the output layer weight coefficient of the BP neural network are updated with the goal of minimizing the value of the systematic error function, the systematic error function adopts e2(k) Only one of said systematic error functions; the system error function may also be other functions with independent variables including any one or any combination of system error, system output expected value and system output actual value, for example, the system error function may be (y)*(k)-y(k))2Or (y)*(k+1)-y(k))2I.e. using e2(k) Another functional form of (1); as another example, the systematic error function takes e2(k)+ωΔu2(k) Wherein Δ u (k) -u (k-1), ω is a constant greater than or equal to 0; obviously, when ω is equal toAt 0, the systematic error function only takes into account e2(k) The contribution of (1) shows that the aim of minimization is to minimize the system error, namely pursuing high precision; and when omega is greater than 0, the system error function considers e simultaneously2(k) Sum of contribution of (1) and Δ u2(k) The contribution of (1) indicates that the goal of minimization is to pursue small system errors and small control input variation, namely to pursue both high precision and stable steering. For the controlled object of the above embodiment, good control effect can be achieved by adopting the different system error functions; considering only e with the systematic error function2(k) Control effects in contribution to the system error function while considering e2(k) Sum of contribution of (1) and Δ u2(k) The contribution of (1) is that the control precision is slightly reduced and the operation stability is improved.
Finally, it should be noted that the parameters to be set by the SISO full-format model-free controller include a penalty factor λ and a step factor ρ1,…,ρLy+LuAny one or any combination of the above; in the above specific embodiment, the first set of trial validations is performed with a penalty factor λ and a step-size factor ρ123Realizes the simultaneous self-tuning, the punishment factor lambda is fixed and the step factor rho is adopted during the verification of the second group of tests123Self-tuning is realized; in practical application, any combination of parameters to be set can be selected according to specific conditions, for example, the step factor ρ12Fixed penalty factor lambda, step factor rho3Self-tuning is realized; in addition, the parameters to be set by the SISO full-format model-free controller include, but are not limited to, a penalty factor λ and a step factor ρ1,…,ρLFor example, the pseudo gradient estimation value can be included according to the specific situation
Figure BDA0001503660040000101
And the like.
The above-described embodiments are intended to illustrate the present invention, but not to limit the present invention, and any modifications, equivalents, improvements, etc. made within the spirit of the present invention and the scope of the claims fall within the scope of the present invention.

Claims (3)

  1. A parameter self-tuning method of a SISO full-format model-free controller based on partial derivative information is characterized by comprising the following steps:
    step (1): determining a control output linearization length constant Ly of the SISO full-format model-free controller, wherein the Ly is an integer greater than or equal to 1; determining a control input linearization length constant Lu of the SISO full-format model-free controller, wherein the Lu is an integer greater than or equal to 1; SISO full-format modeless controller parameters include a penalty factor λ and a step factor ρ1,…,ρLy+Lu(ii) a Determining parameters to be set of a SISO full-format model-free controller, wherein the parameters to be set of the SISO full-format model-free controller are part or all of the parameters of the SISO full-format model-free controller and comprise a penalty factor lambda and a step factor rho1,…,ρLy+LuAny one or any combination of the above; determining the number of input layer nodes, the number of hidden layer nodes and the number of output layer nodes of the BP neural network, wherein the number of the output layer nodes is not less than the number of parameters to be set of the SISO full-format modeless controller; initializing a hidden layer weight coefficient and an output layer weight coefficient of the BP neural network;
    step (2): initializing partial derivative information of the previous moment as the input of a BP neural network;
    and (3): recording the current moment as k moment, and calculating by adopting a system error calculation function to obtain a system error of the k moment based on a system output expected value and a system output actual value, and recording as e (k); the independent variables of the system error calculation function comprise a system output expected value and a system output actual value;
    and (4): based on the input of the BP neural network, the BP neural network carries out forward calculation, and the calculation result is output through an output layer to obtain the value of the parameter to be set of the SISO full-format model-free controller;
    and (5): calculating to obtain a control input u (k) of the SISO full-format model-free controller at the time k for the controlled object by adopting a control algorithm of the SISO full-format model-free controller based on the system error e (k) obtained in the step (3) and the value of the parameter to be set of the SISO full-format model-free controller obtained in the step (4);
    and (6): based on the control input u (k) obtained in the step (5), calculating gradient information of the control input u (k) at the moment k for parameters to be set of each SISO full-format model-free controller, wherein the specific calculation formula is as follows:
    when the parameters to be set of the SISO full-format model-free controller comprise a penalty factor lambda and Lu is 1, the control input u (k) is the gradient information of the penalty factor lambda at the time k:
    Figure FDA0002197380010000021
    when the parameters to be set of the SISO full-format model-free controller comprise penalty factors lambda and Lu >1, the control input u (k) is the gradient information at the k moment aiming at the penalty factors lambda:
    Figure FDA0002197380010000022
    when the parameters to be set of the SISO full-format model-free controller contain step length factors rhoiAnd 1 ≦ i ≦ Ly, the control input u (k) is for the step-size factor ρiThe gradient information at time k is:
    Figure FDA0002197380010000023
    when the parameters to be set of the SISO full-format model-free controller contain step length factors rhoLy+1The control input u (k) is for the step-size factor pLy+1The gradient information at time k is:
    Figure FDA0002197380010000024
    when the SISO full-format modeless controller is readyThe setting parameter comprises a step factor rhoiAnd i is more than or equal to Ly +2 and less than or equal to Ly + Lu and Lu>1, the control input u (k) is for the step-size factor piThe gradient information at time k is:
    Figure FDA0002197380010000031
    wherein Δ u (k) (u (k)) -u (k-1), Δ y (k) (y (k)) -y (k-1),
    Figure FDA0002197380010000032
    is a pseudo-gradient estimate for time k,
    Figure FDA0002197380010000033
    is composed of
    Figure FDA0002197380010000034
    The ith component of (i ═ 1, …, Ly + Lu);
    and (7): the value minimization of a system error function is taken as a target, a gradient descent method is adopted, the gradient information obtained in the step (6) is combined, the system error back propagation calculation is carried out, and the hidden layer weight coefficient and the output layer weight coefficient of the BP neural network are updated to be used as the hidden layer weight coefficient and the output layer weight coefficient when the BP neural network carries out forward calculation at the later moment; the independent variable of the system error function comprises any one or any combination of a system error, a system output expected value and a system output actual value;
    and (8): and (3) recording the gradient information of the parameters to be set of each SISO full-format model-free controller at the time k, which is obtained by calculation in the step (6), of the control input u (k) as the partial derivative information of the previous time in sequence, namely: when the parameters to be set of the SISO full-format model-free controller contain a penalty factor lambda, one of the gradient information at the k moment
    Figure FDA0002197380010000035
    One of the partial derivatives recorded as the previous time
    Figure FDA0002197380010000036
    When the parameters to be set of the SISO full-format model-free controller contain step length factors rhoiAnd when i is more than or equal to 1 and less than or equal to Ly + Lu, one of gradient information at the k moment
    Figure FDA0002197380010000037
    One of the partial derivatives recorded as the previous time
    Figure FDA0002197380010000038
    The partial derivative information of the previous moment is used as the input of the BP neural network when the BP neural network carries out forward calculation at the next moment;
    and (9): and (e) after the control input u (k) acts on the controlled object, obtaining a system output actual value of the controlled object at the later moment, returning to the step (3), and repeating the steps (3) to (9).
  2. 2. The SISO full format model-less controller parameter self-tuning method of claim 1, wherein the systematic error calculation function in step (3) adopts e (k) -y*(k) -y (k), wherein y*(k) The system output expected value is set for the time k, and y (k) is the system output actual value obtained by sampling at the time k; or using e (k) ═ y*(k +1) -y (k), wherein y*And (k +1) is a system output expected value at the moment of k +1, and y (k) is a system output actual value obtained by sampling at the moment of k.
  3. 3. The SISO full format model-less controller parameter self-tuning method of claim 1, wherein the systematic error function in step (7) is e2(k)+ωΔu2(k) Where e (k) is a systematic error, Δ u (k) -u (k-1), and ω is a constant equal to or greater than 0.
CN201711316965.1A 2017-12-12 2017-12-12 Parameter self-tuning method of SISO full-format model-free controller based on partial derivative information Active CN108062021B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711316965.1A CN108062021B (en) 2017-12-12 2017-12-12 Parameter self-tuning method of SISO full-format model-free controller based on partial derivative information

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711316965.1A CN108062021B (en) 2017-12-12 2017-12-12 Parameter self-tuning method of SISO full-format model-free controller based on partial derivative information

Publications (2)

Publication Number Publication Date
CN108062021A CN108062021A (en) 2018-05-22
CN108062021B true CN108062021B (en) 2020-06-09

Family

ID=62138253

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711316965.1A Active CN108062021B (en) 2017-12-12 2017-12-12 Parameter self-tuning method of SISO full-format model-free controller based on partial derivative information

Country Status (1)

Country Link
CN (1) CN108062021B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112015081B (en) * 2020-06-18 2021-12-17 浙江大学 Parameter self-tuning method of SISO (SISO) compact-format model-free controller based on PSO-LSTM (particle swarm optimization-least Square transform) cooperative algorithm
CN113093532B (en) * 2021-03-05 2022-04-15 哈尔滨工程大学 Full-format model-free self-adaptive control method of non-self-balancing system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5513098A (en) * 1993-06-04 1996-04-30 The Johns Hopkins University Method for model-free control of general discrete-time systems
CN1274435A (en) * 1997-10-06 2000-11-22 美国通控集团公司 Model-free adaptive process control
CN101957598A (en) * 2010-09-26 2011-01-26 上海电力学院 Gray model-free control method for large time lag system
CN102033492A (en) * 2010-12-29 2011-04-27 国核电力规划设计研究院 Linear neuron on-line learning adaptive control method and controller for passive system
CN103399487A (en) * 2013-07-30 2013-11-20 东北石油大学 Nonlinear MIMO (multiple input multiple output) system-based decoupling control method and device
CN105676632A (en) * 2016-01-26 2016-06-15 沈阳化工大学 Model-free adaptive optimized control method for PVC polymerization process

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5513098A (en) * 1993-06-04 1996-04-30 The Johns Hopkins University Method for model-free control of general discrete-time systems
CN1274435A (en) * 1997-10-06 2000-11-22 美国通控集团公司 Model-free adaptive process control
CN101957598A (en) * 2010-09-26 2011-01-26 上海电力学院 Gray model-free control method for large time lag system
CN102033492A (en) * 2010-12-29 2011-04-27 国核电力规划设计研究院 Linear neuron on-line learning adaptive control method and controller for passive system
CN103399487A (en) * 2013-07-30 2013-11-20 东北石油大学 Nonlinear MIMO (multiple input multiple output) system-based decoupling control method and device
CN105676632A (en) * 2016-01-26 2016-06-15 沈阳化工大学 Model-free adaptive optimized control method for PVC polymerization process

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
Neural-net-based model-free self-tuning controller with on-line self-learning ability for industrial furnace;Mingwang Zhao;《1994 Proceedings of IEEE International Conference on Control and Applications 》;20020806;全文 *
无模型控制器参数学习步长和惩罚因子的整定研究;马平;《仪器仪表学报》;20080430;第29卷(第4期);全文 *
无模型自适应控制参数整定方法研究;郭代银;《中国优秀硕士学位论文全文数据库信息科技辑》;20150215(第2期);全文 *

Also Published As

Publication number Publication date
CN108062021A (en) 2018-05-22

Similar Documents

Publication Publication Date Title
CN108287471B (en) Parameter self-tuning method of MIMO offset format model-free controller based on system error
CN108170029B (en) Parameter self-tuning method of MIMO full-format model-free controller based on partial derivative information
CN109472418B (en) Maneuvering target state prediction optimization method based on Kalman filtering
Xiao et al. Online optimal control of unknown discrete-time nonlinear systems by using time-based adaptive dynamic programming
CN108345213B (en) Parameter self-tuning method of MIMO (multiple input multiple output) compact-format model-free controller based on system error
CN108181809B (en) System error-based parameter self-tuning method for MISO (multiple input single output) compact-format model-free controller
CN108062021B (en) Parameter self-tuning method of SISO full-format model-free controller based on partial derivative information
CN107942655B (en) Parameter self-tuning method of SISO (SISO) compact-format model-free controller based on system error
CN104462015B (en) Process the fractional order linear discrete system state updating method of non-gaussian L é vy noises
CN107942654B (en) Parameter self-tuning method of SISO offset format model-free controller based on offset information
CN113934142B (en) Non-linear discrete system model-free self-adaptive sliding mode constraint event trigger control method
CN108153151B (en) Parameter self-tuning method of MIMO full-format model-free controller based on system error
CN101390024A (en) Operation control method, operation control device and operation control system
CN112818588B (en) Optimal power flow calculation method, device and storage medium of power system
CN108154231B (en) System error-based parameter self-tuning method for MISO full-format model-free controller
CN108073072B (en) Parameter self-tuning method of SISO (Single input Single output) compact-format model-free controller based on partial derivative information
CN105469142A (en) Neural network increment-type feedforward algorithm based on sample increment driving
CN108287470B (en) Parameter self-tuning method of MIMO offset format model-free controller based on offset information
CN108132600B (en) Parameter self-tuning method of MIMO (multiple input multiple output) compact-format model-free controller based on partial derivative information
US20110196819A1 (en) Method for approximation of optimal control for nonlinear discrete time systems
CN108107715B (en) Parameter self-tuning method of MISO full-format model-free controller based on partial derivative information
CN108008634B (en) Parameter self-tuning method of MISO partial-format model-free controller based on partial derivative information
CN108181808B (en) System error-based parameter self-tuning method for MISO partial-format model-free controller
CN107844051B (en) Parameter self-tuning method of SISO full-format model-free controller based on system error
CN108052006B (en) Decoupling control method for MIMO based on SISO full-format model-free controller and partial derivative information

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant