CN108964544B - Double-time scale sliding mode control system and method for permanent magnet linear synchronous motor - Google Patents

Double-time scale sliding mode control system and method for permanent magnet linear synchronous motor Download PDF

Info

Publication number
CN108964544B
CN108964544B CN201810817650.3A CN201810817650A CN108964544B CN 108964544 B CN108964544 B CN 108964544B CN 201810817650 A CN201810817650 A CN 201810817650A CN 108964544 B CN108964544 B CN 108964544B
Authority
CN
China
Prior art keywords
sliding mode
subsystem
permanent magnet
fast
synchronous motor
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
CN201810817650.3A
Other languages
Chinese (zh)
Other versions
CN108964544A (en
Inventor
周林娜
沈乐萍
程豪琪
陈黎明
汪芸
刘金浩
王众
赵建国
杨春雨
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.)
China University of Mining and Technology CUMT
Original Assignee
China University of Mining and Technology CUMT
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 China University of Mining and Technology CUMT filed Critical China University of Mining and Technology CUMT
Priority to CN201810817650.3A priority Critical patent/CN108964544B/en
Publication of CN108964544A publication Critical patent/CN108964544A/en
Application granted granted Critical
Publication of CN108964544B publication Critical patent/CN108964544B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P21/00Arrangements or methods for the control of electric machines by vector control, e.g. by control of field orientation
    • H02P21/0003Control strategies in general, e.g. linear type, e.g. P, PI, PID, using robust control
    • H02P21/0007Control strategies in general, e.g. linear type, e.g. P, PI, PID, using robust control using sliding mode control
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P21/00Arrangements or methods for the control of electric machines by vector control, e.g. by control of field orientation
    • H02P21/14Estimation or adaptation of machine parameters, e.g. flux, current or voltage
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P25/00Arrangements or methods for the control of AC motors characterised by the kind of AC motor or by structural details
    • H02P25/02Arrangements or methods for the control of AC motors characterised by the kind of AC motor or by structural details characterised by the kind of motor
    • H02P25/022Synchronous motors
    • H02P25/024Synchronous motors controlled by supply frequency
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P2207/00Indexing scheme relating to controlling arrangements characterised by the type of motor
    • H02P2207/05Synchronous machines, e.g. with permanent magnets or DC excitation

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Control Of Ac Motors In General (AREA)
  • Linear Motors (AREA)

Abstract

The invention discloses a double-time scale sliding mode control system and method for a permanent magnet linear synchronous motor, and belongs to the field of linear motor control. Firstly, establishing a mathematical model of a permanent magnet linear synchronous motor in a two-phase rotation orthogonal coordinate system; secondly, establishing the model as a permanent magnet linear synchronous motor double-time scale model; then, in order to improve the robustness of the system to external disturbance, sliding mode control laws corresponding to the fast subsystem and the slow subsystem are respectively designed by adopting a quasi-sliding mode method and an approach law method, and then the time scales of the two subsystems are unified to synthesize the combined control law of the permanent magnet linear synchronous motor. And finally, analyzing the stability of the system by applying the Lyapunov stability theory. The most important characteristic of the invention is that the designed double-time scale sliding mode controller enables the controlled system of the permanent magnet linear synchronous motor to have better static performance and good and rapid dynamic performance, and enables the system to have strong robustness to external disturbance.

Description

Double-time scale sliding mode control system and method for permanent magnet linear synchronous motor
Technical Field
The invention relates to a double-time scale sliding mode control system and method for a permanent magnet linear synchronous motor, and belongs to the technical field of linear synchronous motor control.
Background
The permanent magnet linear synchronous motor, as a linear induction motor, has the advantages of low rotational inertia, small volume and weight, high efficiency, easy maintenance, high reliability and the like besides the excellent advantages of the linear motor, and is generally applied to high-precision alternating current servo systems. Although the linear motor has special advantages compared with the conventional rotating motor, the linear motor is similar to the rotating motor, is a complex control object with high coupling, multivariable, nonlinearity and time-varying property, is influenced by nonlinear factors such as thrust fluctuation and friction in practical application, has weak resistance to external interference of different degrees, and brings great difficulty to the research of a control strategy. In order to greatly improve the control performance and the control precision of the permanent magnet linear synchronous motor, the traditional control strategy is difficult to meet the performance requirement of a permanent magnet linear synchronous motor control system, so that the research of a new control method is very meaningful, at present, the most common control strategy is PID closed-loop control in the classical control field, and the traditional control system is low in dynamic response speed and poor in control precision.
Disclosure of Invention
Aiming at the problems in the prior art, the invention provides a double-time scale sliding mode control system and method for a permanent magnet linear synchronous motor, which can effectively improve the high dynamic response speed of the control system, have strong robustness on parameter perturbation and external disturbance, and are easy to design and implement.
In order to achieve the purpose, the invention adopts the technical scheme that: a permanent magnet linear synchronous motor double-time scale sliding mode control system comprises a slow subsystem sliding mode surface module and a fast subsystem sliding mode surface module, wherein the slow subsystem sliding mode surface module is connected with a combined control law module through a slow subsystem sliding mode control law module; the fast subsystem sliding mode surface module is connected with a combined control law module through the fast subsystem sliding mode control law module; the combined control law module is connected with a permanent magnet linear synchronous motor, the permanent magnet linear synchronous motor is also connected with an external interference signal, the permanent magnet linear synchronous motor is connected to the slow subsystem sliding mode surface module, and an error signal of the actual speed and the given speed of the permanent magnet linear synchronous motor is transmitted to the slow subsystem sliding mode surface module; the permanent magnet linear synchronous motor is connected to the fast subsystem sliding mode surface module through the fast variable estimation module, the currents id and iq of the permanent magnet linear synchronous motor are transmitted to the fast variable estimation module, and the fast variable current components idf and iqf obtained by subtracting the slow variable current components ids and iqs through the fast variable estimation module are transmitted to the fast subsystem sliding mode surface module.
A control method of a permanent magnet linear synchronous motor double-time scale sliding mode control system comprises the following steps:
A. establishing a mathematical model;
B. establishing a double-time scale model;
C. designing a sliding mode control law;
D. synthesizing a combined controller;
E. and (5) analyzing the stability.
The invention has the beneficial effects that: the control system has strong robustness to interference and can realize accurate tracking of a given speed signal; the permanent magnet linear synchronous motor model is decomposed into a fast-slow subsystem through singular perturbation, a sliding mode controller respectively adopts a quasi-sliding mode method and an approach law method, the inherent buffeting phenomenon of sliding mode control is greatly improved, and the control quantity is close to zero after the control system enters a stable state.
Drawings
FIG. 1 is a basic operation diagram of a permanent magnet linear synchronous motor according to the present invention;
FIG. 2 is a block diagram of a dual time scale sliding mode control system of a permanent magnet linear synchronous motor;
FIG. 3 is a comparison of the speed response curves of the dual time scale sliding mode control and PID control of the present invention;
FIG. 4 is a comparison of the speed response curves of the dual time scale control of the present invention and a general sliding mode control;
FIG. 5 is a schematic diagram of an electromagnetic wave thrust curve of the dual time scale sliding mode control of the present invention;
FIG. 6 is an electromagnetic thrust of a general sliding mode control;
fig. 7 is a schematic diagram of three-phase currents of the motor under the control of the double-time scale sliding mode according to the invention.
In the figure: 1. the system comprises a slow subsystem sliding mode surface module, a fast subsystem sliding mode surface module, a 3 slow subsystem sliding mode control law module, a 4 fast subsystem sliding mode control law module, a 5 combined control law module, a 6 permanent magnet linear synchronous motor, 7 interference and 8 fast variable estimation module.
Detailed Description
The invention will be further explained with reference to the drawings.
As shown in fig. 2, the dual-time scale sliding mode control system of the permanent magnet linear synchronous motor comprises a slow subsystem sliding mode surface module 1 and a fast subsystem sliding mode surface module 2, wherein the slow subsystem sliding mode surface module 1 is connected with a combined control law module 5 through a slow subsystem sliding mode control law module 3; the fast subsystem sliding mode surface module 2 is connected with a combined control law module 5 through a fast subsystem sliding mode control law module 4; the combined control law module 5 is connected with a permanent magnet linear synchronous motor 6, the permanent magnet linear synchronous motor 6 is also connected with external interference 7, the permanent magnet linear synchronous motor 6 is connected to the slow subsystem sliding mode surface module 1, and error signals of the actual speed and the given speed of the permanent magnet linear synchronous motor 6 are transmitted to the slow subsystem sliding mode surface module 1; the permanent magnet linear synchronous motor 6 is connected to the fast subsystem sliding mode surface module 2 through the fast variable estimation module 8, and the current i of the permanent magnet linear synchronous motor 6 is converted into the current id、iqTransmitted to a fast variable estimation module 8, passes through the fast variable estimation module 8 and a slow variable current component ids、iqsFast varying current component i obtained by subtractiondf、iqfAnd transmitting to the sliding mode surface module 2 of the quick subsystem.
A control method of a permanent magnet linear synchronous motor double-time scale sliding mode control system comprises the following steps:
A. establishing a mathematical model;
basic working principle of the permanent magnet linear synchronous motor: with reference to the rotating synchronous motor, the rotating synchronous motor is cut along the radius direction of the rotating synchronous motor, and then the circumference of the rotating synchronous motor is horizontally laid along the linear direction, so that a mechanical structure similar to that of the linear motor can be obtained, and therefore, the permanent magnet linear synchronous motor can be regarded as developed by the rotating synchronous motor. The permanent magnet linear synchronous motor is mainly divided into a primary part and a secondary part, wherein the former corresponds to a stator part of the rotary synchronous motor, and the latter corresponds to a rotor part of the rotary synchronous motor. In order to generate an excitation magnetic field, N, S permanent magnets which are longitudinally magnetized are sequentially and evenly distributed at intervals along the secondary stage. In order to generate an air gap magnetic field, tooth grooves provided with three-phase armature windings are distributed on the primary iron core, and when the linear motor is connected with a power supply, a traveling wave magnetic field is generated to drive the linear motor to horizontally move along the guide rail; the basic working principle is shown in figure 1;
a.1, establishing a dynamic model:
the dynamic equation of the permanent magnet linear synchronous motor is composed of a voltage equation, a flux linkage equation, an electromagnetic thrust equation and a motion equation; the idea of applying vector control to a mathematical model of a permanent magnet linear synchronous motor on a two-phase synchronous rotation orthogonal coordinate system is obtained through coordinate transformation, so that the electromagnetic thrust is in direct proportion to a quadrature axis current component iqIs given by a given value i of the direct-axis current componentdSetting the value to zero, and obtaining a dynamic model of the simplified permanent magnet linear synchronous motor on a dq coordinate system as shown in the following formula (1):
Figure BDA0001739758720000041
wherein id、iq、ud、uqThe current and voltage values of d and q axes are respectively, L is inductance, R is resistance value of rotor winding, ω ═ π v/τ is angular velocity of rotor, v is velocity, τ is polar distance of magnetic pole,
Figure BDA0001739758720000044
is a permanent magnet flux linkage, Fe is electromagnetic thrust, M is carrier mass, B is viscous friction coefficient, FLFor load torque, KFIs an electromagnetic thrust coefficient, and is expressed by the following formula (2)) Shown in the figure:
Figure BDA0001739758720000042
wherein p is the magnetic pole pair number of the motor;
a.2, establishing a state equation:
rewriting the dynamic model of the permanent magnet linear synchronous motor obtained in the step A.1 into a state equation form, as shown in the following formula (3):
Figure BDA0001739758720000043
wherein the state variables are v and i ═ id iq]TThe controlled variable is u ═ ud uq]T
A.3, standard form of singular perturbation:
the mathematical model under the two-phase rotation orthogonal coordinate system shows that the nonlinear coupling degree between the current and between the current and the speed is very large, so that a corresponding method is required to realize linear decoupling; considering that the value of the electrical time constant L/R is far less than that of the mechanical time constant M/B, the standard form of the motor singular perturbation can be obtained by taking σ ═ LB/MR as a perturbation parameter with a small value in the singular perturbation system as shown in formula (4):
Figure BDA0001739758720000051
B. establishing a double-time scale model;
b.1, establishing a slow subsystem model:
since the value of σ is very small, assuming perturbation parameter σ → 0, the full-order system model of the original permanent magnet linear synchronous motor is shown as the following formula (5):
Figure BDA0001739758720000052
wherein v iss,ids,iqs,uds,uqsRespectively representing slow-varying components corresponding to v, i and u; substituting the current value obtained by solving the second fraction in the formula (5) into the first fraction to obtain an expression of the slow subsystem model as shown in the formula (6):
Figure BDA0001739758720000053
wherein the content of the first and second substances,
Figure BDA0001739758720000054
udsand uqsFor the slow subsystem control signal, KFIs the electromagnetic thrust coefficient, M is the carrier mass,
Figure BDA0001739758720000057
is a permanent magnet flux linkage, FLThe rotor is a load torque, tau is the polar distance of a magnetic pole, B is a viscous friction coefficient, L is inductance, and R is the resistance value of a rotor winding;
b.2, establishing a fast subsystem model:
compared with the slow subsystem, let v be constant,
Figure BDA0001739758720000055
the available fast-changing current component is as shown in equation (7):
Figure BDA0001739758720000056
and (3) taking the fast time scale gamma as t/sigma, and finally obtaining a mathematical model of the fast subsystem as shown in formula (8):
Figure BDA0001739758720000061
wherein if=[idf iqf]T,udf、uqfIs a control signal of the fast subsystem, KFIs the electromagnetic thrust coefficient, M is the carrier mass,
Figure BDA0001739758720000066
is a permanent magnet flux linkage, FLThe rotor is a load torque, tau is the polar distance of a magnetic pole, B is a viscous friction coefficient, L is inductance, and R is the resistance value of a rotor winding;
and B.3, obtaining a double-time scale model:
by the formulas (6) and (8), a permanent magnet linear synchronous motor double-time scale model is obtained as shown in the formula (9):
Figure BDA0001739758720000062
C. designing a sliding mode control law;
c.1 slow subsystem sliding mode function:
will give a given velocity vsActual speed v of linear synchronous motor with permanent magnetsObtaining a speed error signal esAnd sending the data to a sliding mode surface module of the slow subsystem; the slow subsystem sliding mode surface module is used for generating a speed error signal e according to the speed error signalsObtaining a sliding mode function value S of the slow subsystem as shown in the formula (10)s(es):
Figure BDA0001739758720000063
Wherein, CsIs a speed error coefficient, and Cs>0; and a speed error es=v*-vsV is a given velocity signal;
c.2 slow subsystem equivalent control law:
the slow subsystem sliding mode control law module outputs a sliding mode function value S according to the sliding mode surfaces(es) Calculating to obtain a control signal us(ii) a In the formula (10), the external disturbance d is not consideredsAnd is and
Figure BDA0001739758720000064
Figure BDA0001739758720000065
at 0, the sliding mode function is derived to obtain the form shown in equation (11):
Figure BDA0001739758720000071
obtaining the equivalent control law of the slowness subsystem as shown in the formula (12):
Figure BDA0001739758720000072
after considering the applied disturbance ds, the switching robustness term is designed as shown in the following equation (13):
uss=Kssign(Ss) (13);
the joint vertical type (12) and the formula (13) can obtain the sliding mode control law of the slowness sub-system as shown in the formula (14):
Figure BDA0001739758720000073
in order to effectively reduce the chattering phenomenon, the sign function may be replaced by a saturation function, so that the slow subsystem control law equation (14) is rewritten as shown in the following equation (15):
Figure BDA0001739758720000074
wherein δ is the boundary layer thickness;
c.3, a sliding mode function of a fast subsystem:
the fast variable estimation module is used for converting the current id、iqRespectively with slowly varying current component ids、iqsSubtracting to obtain a fast-changing current component idf、iqfAnd sending the data to a fast subsystem sliding mode surface module; the fast subsystem sliding mode surface module is used for generating a fast variable current signal i according to the fast variable current signal idf、iqfObtaining a sliding mode function value S of the fast subsystem as shown in the formula (16)f
Figure BDA0001739758720000075
Wherein, CfIs a slip form surface coefficient of the fast subsystem, and Cf>0;
C.4 equivalent control law of the fast subsystem:
the sliding mode control law module of the fast subsystem outputs a sliding mode function value S according to the sliding mode functionfCalculating to obtain a control signal uf(γ); in order to weaken buffeting phenomenon existing in the system, an approach law design is adopted
Figure BDA0001739758720000081
Wherein epsilonf=diag(εdfqf),Sf=[S1f S2f]T,Kf=diag(Kdf,Kqf);
Solving the formula (17) to obtain the sliding mode control law of the fast subsystem as shown in the formula (18):
Figure BDA0001739758720000082
wherein the content of the first and second substances,
Figure BDA0001739758720000083
ufa control signal representing the fast subsystem, M is the carrier mass,
Figure BDA0001739758720000085
is a permanent magnet flux linkage, KFIs the electromagnetic thrust coefficient, tau is the polar distance of magnetic pole, B is the viscous friction coefficient, L is inductance, R is the resistance value of rotor winding, SfIs a sliding mode surface function of the fast subsystem;
D. synthesizing a combined controller;
will control signal usControl signal uf(gamma) sending to the combinationThe control law module is combined into a combined controller; the combined controller sends a control signal of the full-order system to the permanent magnet linear synchronous motor;
the joint type (14) and the formula (18) are combined, the system mainly plays a role in a slow subsystem, and the time scale can be unified into a slow-variable subsystem time scale t; and then adding the control laws shown in the formula (14) and the formula (18) to finally obtain a control signal of the full-order system shown in the formula (19):
u=us+uf (19);
E. and (3) stability analysis:
for the slowness sub-system (6), a lyapunov function is defined as (20):
Figure BDA0001739758720000084
to LsTaking the derivative of time, one can obtain:
Figure BDA0001739758720000091
wherein the content of the first and second substances,
Figure BDA0001739758720000092
satisfy the requirement of
Figure BDA0001739758720000093
The available slowness subsystem is stable;
for the promiscuous system (8), a lyapunov function is defined as formula (22):
Figure BDA0001739758720000094
to LfTaking the derivative of time to obtain
Figure BDA0001739758720000095
For inequality
Figure BDA0001739758720000096
Is solved as
Figure BDA0001739758720000097
It can be seen that Lf(t) exponential convergence to 0, the rate of convergence depending on KfThe fast subsystem is known to be numerically stable.
According to the method, stable control laws are respectively designed according to the speed system and the slow system according to the singular perturbation principle, and the obtained combined control law is stable.
In this embodiment, in order to verify the effectiveness and advantages of the designed system, the embodiment builds a model and performs simulation for a dual-time scale sliding mode control system and method for a permanent magnet linear synchronous motor: the parameters of the permanent magnet linear synchronous motor are set as follows, the viscous friction coefficient B is 0.22, the carrier mass M is 100kg, the pole pitch tau of the magnetic pole is 3.6cm, the pole pair p of the motor in the permanent magnet flux linkage is 3, and the parameters of the controller of the slow subsystem are set as follows Cs=[0.4 0.4]T,KsBiag (0,81), δ 0.01; parameter settings for the fast subsystem controller are as follows Cf=diag(1,1),εf=diag(30,30),KfDiag (300); inputting a step signal with the speed of 1r/s, starting the permanent magnet linear synchronous motor in an idle load mode, and suddenly adding load disturbance of TL 100N when t is 0.5 s; the simulation results of the permanent magnet linear synchronous motor double-time scale sliding mode control system are shown in fig. 3 to 7; fig. 3 to 7 are speed response curves of double-time scale sliding mode control and PID control, speed response curves of double-time scale control and general sliding mode control, electromagnetic wave thrust curves of double-time scale sliding mode control, electromagnetic thrust curves of general sliding mode control, and three-phase current schematic curves of a motor under double-time scale sliding mode control, respectively; as can be seen from fig. 3, compared with PID control, the dual-time scale sliding mode control has faster dynamic response speed, better dynamic performance, and better robustness to external disturbance; as can be seen from fig. 4, compared with the general equivalent sliding mode control, the quasi-sliding mode method and the approach law method are adopted, the dynamic quality of the system is better, and the robustness to external interference is stronger; drawing(s)Compared with fig. 6, it can be known that compared with the general equivalent sliding mode control, the dual-time scale sliding mode control designed by the quasi-sliding mode method and the approach law method has stronger buffeting restraining capability, reduces the influence caused by thrust fluctuation, and simultaneously, when external load disturbance occurs, the electromagnetic thrust can overcome the interference of the electromagnetic thrust on the performance of the motor system; the schematic curve of the three-phase current of the motor under the double-time scale sliding mode control is shown in fig. 7, and the buffeting phenomenon of the system can be improved. It should be noted that the excellent performance exhibited by the present example is illustrative of the present invention and not limiting.
The design process and the idea of the permanent magnet linear synchronous motor double-time scale sliding mode control system and method are explained above. The method is established as a double-time scale model of the permanent magnet linear synchronous motor, sliding mode control laws corresponding to a fast subsystem and a slow subsystem are respectively designed by adopting a quasi-sliding mode method and an approach law method, then time scales of the two subsystems are unified, a combined controller of the permanent magnet linear synchronous motor is synthesized, and meanwhile, the stability of the system is analyzed by applying the Lyapuloff stability theory. Simulation results show that the control system not only has high dynamic response speed, but also has strong robustness to external disturbance, and can realize accurate tracking of given speed signals. In addition, the buffeting phenomenon of the sliding mode control is greatly improved.

Claims (1)

1. A permanent magnet linear synchronous motor double-time scale sliding mode control method is characterized by comprising a slow subsystem sliding mode surface module and a fast subsystem sliding mode surface module, wherein the slow subsystem sliding mode surface module is connected with a combined control law module through a slow subsystem sliding mode control law module; the fast subsystem sliding mode surface module is connected with a combined control law module through the fast subsystem sliding mode control law module; the combined control law module is connected with a permanent magnet linear synchronous motor, the permanent magnet linear synchronous motor is also connected with external interference, and the permanent magnet linear synchronous motor is connected to the slow subsystem sliding mode surface module; the permanent magnet linear synchronous motor is connected to the fast subsystem sliding mode surface module through the fast variable estimation module;
and comprises the steps of:
A. establishing a mathematical model;
a.1, establishing a dynamic model:
the dynamic equation of the permanent magnet linear synchronous motor is composed of a voltage equation, a flux linkage equation, an electromagnetic thrust equation and a motion equation; the idea of applying vector control to a mathematical model of a permanent magnet linear synchronous motor on a two-phase synchronous rotation orthogonal coordinate system is obtained through coordinate transformation, so that the electromagnetic thrust is in direct proportion to a quadrature axis current component iqSetting the given value of the direct-axis current component as zero, and obtaining a dynamic model of the simplified permanent magnet linear synchronous motor on a dq coordinate system as shown in the following formula (1):
Figure FDA0003333446940000011
wherein id、iq、ud、uqThe current and voltage values of d and q axes respectively, L is inductance, R is resistance value of rotor winding, ω ═ π v/τ is angular velocity of rotor, v is velocity, τ is polar distance of magnetic pole,
Figure FDA0003333446940000012
is a permanent magnet flux linkage, Fe is electromagnetic thrust, M is carrier mass, B is viscous friction coefficient, FLFor load torque, KFThe expression of the electromagnetic thrust coefficient is shown in the following formula (2):
Figure FDA0003333446940000013
wherein p is the magnetic pole pair number of the motor;
a.2, establishing a state equation:
rewriting the dynamic model of the permanent magnet linear synchronous motor obtained in the step A.1 into a state equation form, as shown in the following formula (3):
Figure FDA0003333446940000014
wherein the state variables are v and i ═ id iq]TThe controlled variable is u ═ ud uq]T
A.3, standard form of singular perturbation:
taking sigma-LB/MR as perturbation parameters in a singular perturbation system, and obtaining a standard form of the singular perturbation of the motor as shown in a formula (4):
Figure FDA0003333446940000021
B. establishing a double-time scale model;
b.1, establishing a slow subsystem model:
since the value of σ is very small, assuming perturbation parameter σ → 0, the full-order system model of the original permanent magnet linear synchronous motor is shown as the following formula (5):
Figure FDA0003333446940000022
wherein v iss,ids,iqs,uds,uqsRespectively representing slow-varying components corresponding to v, i and u; substituting the current value obtained by solving the second fraction in the formula (5) into the first fraction to obtain an expression of the slow subsystem model as shown in the formula (6):
Figure FDA0003333446940000023
wherein the content of the first and second substances,
Figure FDA0003333446940000024
udsand uqsFor the slow subsystem control signal, KFIs the electromagnetic thrust coefficient, M is the carrier mass,
Figure FDA0003333446940000025
is a permanent magnet flux linkage, FLThe rotor is a load torque, tau is the polar distance of a magnetic pole, B is a viscous friction coefficient, L is inductance, and R is the resistance value of a rotor winding;
b.2, establishing a fast subsystem model:
compared with the slow subsystem, let v be constant,
Figure FDA0003333446940000026
the available fast-changing current component is as shown in equation (7):
Figure FDA0003333446940000027
and (3) taking the fast time scale gamma as t/sigma, and finally obtaining a mathematical model of the fast subsystem as shown in formula (8):
Figure FDA0003333446940000031
wherein if=[idf iqf]T,udf、uqfIs a control signal of the fast subsystem, KFIs the electromagnetic thrust coefficient, M is the carrier mass,
Figure FDA0003333446940000032
is a permanent magnet flux linkage, FLThe rotor is a load torque, tau is the polar distance of a magnetic pole, B is a viscous friction coefficient, L is inductance, and R is the resistance value of a rotor winding;
and B.3, obtaining a double-time scale model:
by the formulas (6) and (8), a permanent magnet linear synchronous motor double-time scale model is obtained as shown in the formula (9):
Figure FDA0003333446940000033
C. designing a sliding mode control law;
c.1 slow subsystem sliding mode function:
will give a given velocity vsActual speed v of linear synchronous motor with permanent magnetsObtaining a speed error signal esAnd sending the data to a sliding mode surface module of the slow subsystem; the slow subsystem sliding mode surface module is used for generating a speed error signal e according to the speed error signalsObtaining a sliding mode function value S of the slow subsystem as shown in the formula (10)s(es):
Figure FDA0003333446940000034
Wherein, CsIs a speed error coefficient, and Cs>0; and a speed error es=v*-vsV is a given velocity signal;
S1s、S2sfor slow subsystem sliding mode function value SsTwo components written in the form of column vectors;
c.2 slow subsystem equivalent control law:
the slow subsystem sliding mode control law module outputs a sliding mode function value S according to the sliding mode surfaces(es) Calculating to obtain a control signal us(ii) a In the formula (10), the external disturbance d is not consideredsAnd is and
Figure FDA0003333446940000035
Figure FDA0003333446940000036
at 0, the sliding mode function is derived to obtain the form shown in equation (11):
Figure FDA0003333446940000037
wherein, C1s、C2sIs a speed error coefficient CsTwo components written in the form of column vectors; f (v)s) To relate to vsA function of (a);
obtaining the equivalent control law of the slowness subsystem as shown in the formula (12):
Figure FDA0003333446940000041
after considering the external disturbance ds, the designed switching robustness term is shown as the formula (13): u. ofss=Kssign(Ss) (13);
Wherein, KsRepresenting the sliding mode switching control gain of the slow subsystem;
the joint vertical type (12) and the formula (13) can obtain the sliding mode control law of the slowness sub-system as shown in the formula (14):
Figure FDA0003333446940000042
c.3, a sliding mode function of a fast subsystem:
the fast variable estimation module is used for converting the current id、iqRespectively with slowly varying current component ids、iqsSubtracting to obtain a fast-changing current component idf、iqfAnd sending the data to a fast subsystem sliding mode surface module; the fast subsystem sliding mode surface module is used for generating a fast variable current signal i according to the fast variable current signal idf、iqfObtaining a sliding mode function value S of the fast subsystem as shown in the formula (16)f
Figure FDA0003333446940000043
Wherein, CfIs a slip form surface coefficient of the fast subsystem, and Cf>0;S1f、S2fFor the sliding mode function value S of the express subsystemfTwo components written in the form of column vectors;
c.4 equivalent control law of the fast subsystem:
the sliding mode control law module of the fast subsystem outputs a sliding mode function value S according to the sliding mode functionfCalculating to obtain a control signal uf(γ); in order to weaken buffeting phenomenon existing in the system, an approach law design is adopted
Figure FDA0003333446940000044
Wherein epsilonf=diag(εdfqf),Sf=[S1f S2f]T,Kf=diag(Kdf,Kqf);εdf、εqfIs epsilonfTwo components on d-and q-axes, Kdf、KqfIs KfTwo components on the d-axis and q-axis; epsilonfAnd KfParameters of an approach law;
solving the formula (17) to obtain the sliding mode control law of the fast subsystem as shown in the formula (18):
Figure FDA0003333446940000045
wherein the content of the first and second substances,
Figure FDA0003333446940000046
ufa control signal representing the fast subsystem, M is the carrier mass,
Figure FDA0003333446940000047
is a permanent magnet flux linkage, KFIs the electromagnetic thrust coefficient, tau is the polar distance of magnetic pole, B is the viscous friction coefficient, L is inductance, R is the resistance value of rotor winding, SfIs a sliding mode surface function of the fast subsystem;
D. synthesizing a combined controller;
will control signal usControl signal uf(gamma) sending to a combination control law module to combine the combination controller; the combined controller sends a control signal of the full-order system to the permanent magnet linear synchronous motor;
the joint type (14) and the formula (18) are combined, the system mainly plays a role in a slow subsystem, and the time scales are unified into a slow-variable subsystem time scale t; then adding the control laws shown in the formula (14) and the formula (18) to obtain the formula(19) Control signals for the full-order system shown; u-us+uf (19);
E. And (3) stability analysis:
for the slowness sub-system (6), a lyapunov function is defined as (20):
Figure FDA0003333446940000051
to LsTaking the derivative of time, one can obtain:
Figure FDA0003333446940000052
wherein the content of the first and second substances,
Figure FDA0003333446940000053
satisfy the requirement of
Figure FDA0003333446940000054
The slowness system is known to be stable;
Kds、Kqsis KsTwo components on the d-axis and q-axis;
for the promiscuous system (8), a lyapunov function is defined as formula (22):
Figure FDA0003333446940000055
to LfTaking the derivative of time, one can obtain:
Figure FDA0003333446940000056
for inequality
Figure FDA0003333446940000057
Is solved as
Figure FDA0003333446940000058
It can be seen that Lf(t) exponential convergence to 0, the rate of convergence depending on KfThe fast subsystem is known to be numerically stable; respectively designing stable control laws according to the speed system and the slow system according to the singular perturbation principle, wherein the obtained combined control law is stable, and Lf(t0) Represents the initial value, t, of the Lyapunov function of the fast subsystem0Indicating the initial time.
CN201810817650.3A 2018-07-23 2018-07-23 Double-time scale sliding mode control system and method for permanent magnet linear synchronous motor Active CN108964544B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810817650.3A CN108964544B (en) 2018-07-23 2018-07-23 Double-time scale sliding mode control system and method for permanent magnet linear synchronous motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810817650.3A CN108964544B (en) 2018-07-23 2018-07-23 Double-time scale sliding mode control system and method for permanent magnet linear synchronous motor

Publications (2)

Publication Number Publication Date
CN108964544A CN108964544A (en) 2018-12-07
CN108964544B true CN108964544B (en) 2022-05-03

Family

ID=64463553

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810817650.3A Active CN108964544B (en) 2018-07-23 2018-07-23 Double-time scale sliding mode control system and method for permanent magnet linear synchronous motor

Country Status (1)

Country Link
CN (1) CN108964544B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110011583B (en) * 2019-04-12 2020-11-17 中国矿业大学 Permanent magnet synchronous motor sliding mode control system based on singular perturbation theory and modeling method
CN112068431B (en) * 2020-09-03 2023-03-24 广州大学 Control method, system and device for double time scales and storage medium
CN112468044B (en) * 2020-11-10 2022-09-06 东南大学 Model prediction control system and method for permanent magnet synchronous linear motor
CN113541537B (en) * 2021-07-22 2023-06-09 东南大学 Moment control system and test method for rotary linear magnetic screw
CN115933383B (en) * 2022-11-21 2023-05-30 中国矿业大学 Nonlinear double-time-scale industrial system H infinite combination control method based on reinforcement learning
CN115933410B (en) * 2023-01-09 2023-07-07 中国矿业大学 Optimal tracking control method for double-time-scale coal-fired power generation system based on Q learning

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20060035838A (en) * 2004-10-20 2006-04-27 (주)세다 Apparatus for compensating straightness error of linear motor stage and sliding mode control method for the same
CN104038133A (en) * 2014-06-20 2014-09-10 福州大学 Permanent magnet synchronous linear motor translation slip plane sliding mode position control method
CN105591524A (en) * 2016-02-24 2016-05-18 江苏大学 Permanent magnet rotating speed difference clutch and self-adaption nonsingular terminal slip form rotating speed control method thereof
CN106849795A (en) * 2017-03-14 2017-06-13 中国矿业大学 A kind of permanent magnet linear synchronous motor System with Sliding Mode Controller based on linear extended state observer
CN107947646A (en) * 2017-12-22 2018-04-20 中国矿业大学 It is a kind of to coordinate control optimization method based on the double permanent magnet synchronous motors for having mechanical attachment

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20060035838A (en) * 2004-10-20 2006-04-27 (주)세다 Apparatus for compensating straightness error of linear motor stage and sliding mode control method for the same
CN104038133A (en) * 2014-06-20 2014-09-10 福州大学 Permanent magnet synchronous linear motor translation slip plane sliding mode position control method
CN105591524A (en) * 2016-02-24 2016-05-18 江苏大学 Permanent magnet rotating speed difference clutch and self-adaption nonsingular terminal slip form rotating speed control method thereof
CN106849795A (en) * 2017-03-14 2017-06-13 中国矿业大学 A kind of permanent magnet linear synchronous motor System with Sliding Mode Controller based on linear extended state observer
CN107947646A (en) * 2017-12-22 2018-04-20 中国矿业大学 It is a kind of to coordinate control optimization method based on the double permanent magnet synchronous motors for having mechanical attachment

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
Design of sliding mode controller for linear vernier permanent magnet motor;Hongyu Tang et al.;《 2016 IEEE Advanced Information Management, Communicates, Electronic and Automation Control Conference (IMCEC)》;20170302;第648-652页 *
基于奇异摄动的永磁直线同步电动机滑模控制;袁晓磊;《中国优秀硕士学位论文全文数据库(工程科技Ⅱ辑)》;20090215(第2期);正文第11页第2段-第13页最后1段、第26页第1段-第36页最后1段 *

Also Published As

Publication number Publication date
CN108964544A (en) 2018-12-07

Similar Documents

Publication Publication Date Title
CN108964544B (en) Double-time scale sliding mode control system and method for permanent magnet linear synchronous motor
CN110429881B (en) Active-disturbance-rejection control method of permanent magnet synchronous motor
Jiang et al. Improved deadbeat predictive current control combined sliding mode strategy for PMSM drive system
CN106849795B (en) A kind of permanent magnet linear synchronous motor System with Sliding Mode Controller
Khater et al. Selection of flux level in field-oriented induction machine controllers with consideration of magnetic saturation effects
CN110247585B (en) Multi-axis servo variable-proportion cooperative control method based on sliding mode variable structure
Han et al. Improved online maximum-torque-per-ampere algorithm for speed controlled interior permanent magnet synchronous machine
CN110247592B (en) Multivariable second-order nonsingular terminal sliding mode current control method introducing approach law
CN110995102A (en) Direct torque control method and system for permanent magnet synchronous motor
CN111969912B (en) Sensorless control method and system for permanent magnet synchronous motor
CN111211717B (en) IPMSM (intelligent power management system) position-sensorless motor closed-loop control method of nonsingular sliding mode structure
CN104300864A (en) Decoupling control method for permanent magnet synchronous motor
Han et al. Nonlinear magnetic field vector control with dynamic-variant parameters for high-power electrically excited synchronous motor
Zhang et al. Maximum torque per ampere control for IPMSM traction system based on current angle signal injection method
Wen et al. Sensorless control of segmented PMLSM for long-distance auto-transportation system based on parameter calibration
CN109194224B (en) Permanent magnet synchronous motor sensorless control method based on extended state observer
CN114337426A (en) Permanent magnet synchronous motor deviation decoupling control method under d-q axis static coordinate system
CN114567226A (en) PMSM speed regulation system variable approach law sliding mode control method considering iron loss
CN108306566A (en) Line inductance electromotor secondary flux linkage estimation method based on extended state observer
Liu et al. Speed estimation with parameters identification of PMSM based on MRAS
Yan et al. Disturbance Observer‐Based Backstepping Control of PMSM for the Mine Traction Electric Locomotive
CN115459667B (en) Permanent magnet synchronous motor sensorless sliding mode control method based on improved approach law
Matsuki et al. High‐Response Torque Control of IPMSM Based on a New Coordinate System Suitable for Voltage Amplitude and Phase Control
CN115102443A (en) Control method and device for permanent magnet synchronous linear motor and storage medium
CN110011583B (en) Permanent magnet synchronous motor sliding mode control system based on singular perturbation theory and modeling method

Legal Events

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