# Patent

## Title
Device and method for plasticization control of electric injection molding machine

## Abstract

{Problem} The exact method with small time-lag of detecting screw back pressure for controlling the screw back pressure in the plasticizing process of an electric-motor driven injection molding machine without using a pressure detector has been asked for because the pressure detector is very expensive, necessitates troublesome works for mounting, an electric protection against noise and the works for zero-point and span adjustings and causes a complicate mechanical structure.
{Solution} The present invention uses a high-gain observer which contains the discrete-time arithmetic expressions derived from a mathematical model of a plasticizing mechanism in an electric-motor driven injection molding machine consisting of a state equation and an output equation and outputs an estimate of screw back pressure, which is one of the state variables of the above state equation, by using a screw backward velocity signal, a motor current demand signal applied to a servomotor for injection or actual motor current signal and a screw revolution speed signal as inputs. The high-gain observer obtains the exact screw back pressure estimate with very small time-lag without using a pressure detector. Thus the estimate of screw back pressure fed by the high-gain observer can be adopted as a feedback signal of actual screw back pressure for controlling the screw back pressure in the plasticizing process.

## Background
TECHNICAL FIELD
This invention is concerning an apparatus and a method for controlling a plasticizing capability in an electric-motor driven injection molding machine.
BACKGROUND ART
AC servomotors are becoming used for middle-sized injection molding machines heretofore driven by hydraulic actuators (clamping force>3.5 MN) that have high precision, quick response and higher power which are obtained by performance improvements of permanent magnets and cost reductions.
An injection molding machine consists of a plasticizer in which resin pellets are melted by friction heat generated by plasticizing screw revolution and stored at the end of a barrel, an injector in which an amount of melted polymer is injected into a metal mold at a given velocity and a given dwell pressure is applied, and a clamper in which the metal mold is clamped and opened, all using AC servomotors drive system. FIG. 2 is a view which shows an existing plasticizing mechanism by AC servomotors.
On an injection machine base which is fixed on the ground, a movable base is located which moves on a linear slider and both the bases are not shown in FIG. 2. All parts except a metal mold 1 shown in FIG. 2 are mounted on the movable base. By sliding the movable base, the top of a barrel 2 is clamped on the metal mold 1 and vice versa the top of the barrel 2 is separated from the metal mold 1. FIG. 2 shows a mode in which the resin pellets are melted by the screw revolution in the plasticizing process.
On the movable base, a barrel 2, a servomotor for injection 3, a reduction gear 4, a ball screw 5, a bearing 6 and a hopper 16 are fixed. A nut 7 of the ball screw 5, a moving part 8, a screw 9, a reduction gear 10, a servomotor for plasticization 11 and a pressure detector 12 such as a load cell consist of an integral structure. The moving part 8 is mounted on a linear slider 13 so that the integral structure is moved back and forth by the movement of the nut 7.
Rotation of the servomotor for injection 3 is transferred to the ball screw 5 which magnifies a linear force through the reduction gear 4 and the rotation of the ball screw 5 is converted to a linear motion of the nut 7 of the ball screw 5 and through the moving part 8, a linear motion of the screw 9 and pressure application to the stored melted polymer are realized. Pressure applied to the melted polymer by the screw 9 in the plasticizing process is hereinafter referred to as a screw back pressure. Position of the screw 9 is detected by a rotary encoder 14 mounted on the servomotor for injection 3. Screw back pressure to the melted polymer stored at the end of the barrel 2 is detected by the pressure detector 12 such as a load cell mounted between the nut 7 and the moving part 8. The screw 9 is rotated by the servomotor for plasticization 11 through the reduction gear 10 in the plasticizing process in which resin pellets are melted and kneaded and a rotary encoder 15 is mounted on the servomotor for plasticization 11.
Explaining an injection molding process with referent to FIG. 2, resin pellets are fed to the screw 9 through the hopper 16 and are melted by the screw 9 rotated by the servomotor for plasticization 11 and the melted polymer is pushed out from the top of the screw 9 and the screw 9 is moved back by the generated screw back pressure. The screw back pressure is a linear force applied to the melted polymer decided by a generated motor torque of the servomotor for injection 3. The servomotor for plasticization 11 continues to rotate until a given amount of melted polymer necessary for molding a product is stored at the end of the barrel 2 and then the plasticizing process is finished with the stop of the screw revolution.
Next the screw 9 is moved forward rapidly by a high-speed revolution of the servomotor for injection 3 and the stored melted polymer at the end of the barrel 2 is injected into a cavity 17 as fast as possible and a given pressure is applied for a given duration at the polymer in the cavity 17 and then the injection process is finished and a molding product with a given figure is taken out from the metal mold 1.
It is necessary to get the melted polymer of homogeneous property in the plasticizing process in order to manufacture good-quality molding products. But as the stored melted polymer at the end of the barrel 2 increases in the plasticizing process, an effective length of the screw 9 for plasticizing the resin pellets decreases as the result of the backward movement of the screw 9 in the barrel 2. Therefore, the decrease of the effective length of the screw brings about a variation in the property of the melted polymer, that is, the property of the melted polymer generated at the initial stage of plasticization is different from that of the melted polymer generated at the final stage. To make up for this defect, some methods are applied in which a given pattern of screw back pressure corresponding to the backward movement of the screw 9 is realized in the plasticizing process in order to get a homogeneous property of the melted polymer.
In patent literatures PTL 1 and PTL 2, a given screw revolution is realized by a servomotor for plasticization and the speed control of a screw backward movement by a servomotor for injection realizes a given pattern of screw back pressure.
In patent literatures PTL 3 and PTL 4, a constant speed or a given speed pattern of a screw backward movement is realized by a servomotor for injection and the rotation speed control of a screw by a servomotor for plasticization realizes a given pattern of screw back pressure.
In patent literatures PTL 5 and PTL 6, a given pattern of screw back pressure is realized by a motor current (torque) limit control or a motor current (torque) control of a servomotor for injection.
In patent literatures PTL 7 and PTL 8, the position control of a screw by a servomotor for injection realizes a given pattern of screw back pressure.
In patent literatures PTL 9 and PTL 10, a given revolution speed of a screw is realized by a servomotor for plasticization and a speed control of the screw backward movement by a servomotor for injection realizes a given pattern of screw back pressure and in the speed control of the screw backward movement a set value of screw backward speed modified by a control deviation of the screw back pressure is used.
In patent literature PTL 11, the control mode transfer from the first control mode to the second control mode is carried out. In the first control mode a screw revolution control is carried out by a servomotor for plasticization and a screw back pressure control is carried out by a servomotor for injection. In the second control mode a screw back pressure control is carried out by a servomotor for plasticization and a speed control of screw backward movement is carried out by a servomotor for injection.
In patent literatures PTL 1 ̃PTL 11, a screw back pressure control is absolutely necessary in the plasticizing process and a pressure detector is required to realize an accurate control of screw back pressure.
In patent literature PTL 12, a pressure detector with a small dynamic range (0 ̃15.2 MPa) is used for plasticization and a pressure detector with a large dynamic range (15.2 ̃304 MPa) is used for injection and pressure application. The control accuracy of screw back pressure in the plasticizing process is improved by using a pressure detector with a smaller dynamic range.
FIG. 3 is an explanation drawing which shows a block diagram of an existing plasticizing controller. The plasticizing controller consists of a back pressure controller 20, a motor controller (servoamplifier) for injection 30, a screw revolution speed controller 40, a motor controller (servoamplifier) for plasticization 50 and a pressure detector 12.
The back pressure controller 20 executes a control algorithm at a constant time interval and a discrete-time control is used. The back pressure controller 20 consists of a screw back pressure setting device 21, a subtracter 22, an analog/digital (A/D) converter 23, a pressure controller 24 and a digital/analog (D/A) converter 25. The pressure detector 12 is connected to the A/D converter 23.
The screw back pressure setting device 21 feeds a time sequence of screw back pressure command P*b to the subtracter 22. The pressure detector 12 feeds an actual screw back pressure signal Pb to the subtracter 22 through the A/D converter 23. The subtracter 22 calculates a back pressure control deviation ΔPb=P*b−Pb and the control deviation ΔPb is fed to the pressure controller 24. The pressure controller 24 calculates a motor current demand i*m for the servomotor for injection 3 from ΔPb by using PID (Proportional+Integral+Derivative) control algorithm and feeds the demand i*m to the motor controller for injection 30 through the D/A converter 25.
The motor controller for injection 30 consists of an analog/digital (A/D) converter 31 and a PWM (Pulse Width Modulation) device 32. The motor controller for injection 30 is connected to the servomotor for injection 3 equipped with a rotary encoder 14. The A/D converter 31 feeds the motor current demand i*m from the D/A converter 25 to the PWM device 32. The PWM device 32 applies three-phase voltage to the servomotor for injection 3 so that the servomotor for injection 3 is driven by the motor current i*m. A linear force by the screw 9 applied to the melted polymer stored at the end of the barrel 2 decided by a generated motor current i*m (motor torque) realizes a given screw back pressure P*b.
The screw revolution speed controller 40 consists of a screw revolution speed setting device 41. The screw revolution speed setting device 41 feeds a time sequence of screw revolution speed command N*s to the motor controller for plasticization 50.
The motor controller for plasticization 50 consists of a subtracter 51, a differentiator 52, a speed controller 53 and a PWM device 54. The motor controller for plasticization 50 is connected to the servomotor for plasticization 11 equipped with a rotary encoder 15. The screw revolution speed command N*s from the screw revolution speed controller 40 is fed to the subtracter 51. The rotary encoder 15 mounted on the servomotor for plasticization 11 feeds a pulse train to the differentiator 52. The differentiator 52 detects an actual screw revolution speed Ns and feeds the speed signal Ns to the subtracter 51. The subtracter 51 calculates a screw speed control deviation ΔNs=N*s−Ns and feeds the control deviation ΔNs to the speed controller 53. The speed controller 53 calculates a motor current demand i* for the servomotor for plasticization 11 from ΔNs by using PID control algorithm and feeds the demand i* to the PWM device 54. The PWM device 54 applies three-phase voltage to the servomotor for plasticization 11 so that the servomotor for plasticization 11 is driven by the motor current i* and a given screw revolution speed N*s is realized.
But the usage of the pressure detector in the plasticizing process brings about the following disadvantages.

    (1) A highly reliable pressure detector is very expensive under high pressure circumstances.
    (2) Mounting a pressure detector in the cavity or the barrel nozzle part necessitates the troublesome works and the working cost becomes considerable.
    (3) Mounting a load cell in an injection shafting alignment from a servomotor for injection to a screw complicates the mechanical structure and degrades the mechanical stiffness of the structure.
    (4) A load cell which uses strain gauges as a detection device necessitates an electric protection against noise for weak analog signals. Moreover the works for zero-point and span adjustings of a signal amplifier are necessary (patent literature PTL 13).
    (5) For the improvement of the control accuracy of screw back pressure, the usage of two kinds of pressure detectors with different dynamic ranges brings about the cost increase (patent literature PTL 12).


CITATION LIST 
Patent Literature 
PTL 1: Patent 61-37409
PTL 2: Patent 61-217227
PTL 3: Patent 61-72512
PTL 4: Patent 2005-35132
PTL 5: Patent 61-258722
PTL 6: Patent 3-58818
PTL 7: Patent 2-130117
PTL 8: Patent 4-249129
PTL 9: Patent 2-120020
PTL 10: Patent 7-9513
PTL 11: Patent 2002-321264
PTL 12: Patent 2000-351139
PTL 13: Patent 2003-211514
Non Patent Literature 
NPL 1: H. K. Khalil, Nonlinear Systems, 14.5 High-Gain Observer, Prentice-Hall, (2002), pp. 610-625
NPL 2: B. D. O. Anderson and J. B. Moore, Optimal Control, Linear Quadratic Methods, 7.2 Deterministic Estimator Design, Prentice-Hall, (1990), pp. 168-178
NPL 3: A. M. Dabroom and H. K. Khalil, Discrete-time implementation of high-gain observers for numerical differentiation, Int. J. Control, Vol. 72, No. 17, (1999), pp. 1523-1537
NPL 4: A. M. Dabroom and H. K. Khalil, Output Feedback Sampled-Data Control of Nonlinear Systems Using High-Gain Observers, IEEE trans. Automat. Contr., Vol. 46, No. 11, (2001), pp. 1712-1725
SUMMARY OF INVENTION
Technical Problem
The problem that starts being solved is to realize a plasticizing controller of electric-motor driven injection molding machines which satisfies the requirement that an adequate screw back pressure is applied to the melted polymer stored at the end of the barrel during the plasticizing process without using a pressure detector in order to avoid the five disadvantages described in Background Art resulted by using a pressure detector.
Solution to Problem
A control of screw back pressure is an effective means to obtain the homogeneous property of melted polymer and to improve the metering accuracy in the plasticizing process. In order to realize an accurate control of screw back pressure without using a pressure detector, a detecting means of screw back pressure which satisfies the following two requirements (A) and (B) is required. (A) The detection means is high-precision. (B) The detection means has very small time-lag. The method of a high-gain observer (non patent literature NPL 1) is used as a pressure detecting means which satisfies the above two requirements. The high-gain observer estimates all state variables by using detected variables and satisfies the above two requirements (A) and (B). This is explained by using a simple mathematical model as follows. Equation (1) shows a state equation and an output equation of a simple model.




  
    
      
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where x1, x2: State variables, u: Input variable, y: Output variable, φ(x, u): Nonlinear function of variables x, u. For example x1 is position variable, x2 is velocity variable and u is motor current variable. Output variable y and input variable u are supposed to be measurable. The high-gain observer which estimates state x is given by equation (2).





  
    
      
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where {circumflex over (x)}1, {circumflex over (x)}2: Estimates of state variables x1, x2, H1, H2: Gain constants of the high-gain observer which are larger than 1, φ0: Nominal function of φ used in high-gain observer computing. Estimation errors {tilde over (x)}1, {tilde over (x)}2 by using the high-gain observer equation (2) are given by equation (3) from equations (1) and (2).





  
    
      
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where δ: Model error between the nominal model φ0 and the true but actually unobtainable function φ. Introducing a positive parameter ε much smaller than 1, H1, H2 are given by equation (5).





  
    
      
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As H1, H2 in equation (5) are large gain constants, equation (2) is called by a high-gain observer. By using equation (5), equation (3) is rewritten as equation (6).




  
    
      
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The estimation errors {tilde over (x)}1, {tilde over (x)}2 are replaced by new variables η1, η2 as written in equation (7).




  
    
      
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By using equation (7), equation (6) is rewritten as equation (8).




  
    
      
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As the parameter ε is much smaller than 1, the effects of model error δ on the estimation errors η1, η2 can be made small enough by equation (8). Thus by using the high-gain observer for a model which has screw back pressure as a state variable, the above requirement (A) “High-precision detection” for a pressure detecting means (paragraph{0028}) is satisfied.
When the effects of the model error δ on the estimation errors η1, η2 are neglected, equation (8) is rewritten as equation (9).




  
    
      
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When K1, K2 are decided so that conjugate complex eigenvalues λ1, λ1 of matrix A have a negative real part, that is, Re(λ1)=Re( λ1)<0, the estimate errors η1, η2 are given by equation (11) with initial values η10, η20.




  
    
      
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        11
        )
      
    
  




where t: Time variable, C1(t) ̃C4(t): Sinusoidal components with constant amplitudes and constant frequency decided by K1, K2. As Re(λ1)<0 and ε is much smaller than 1, equation (11) reveals that the time responses η1(t), η2(t) of estimation errors tend to zero rapidly. In other words, by using high-gain observer equation (2), the above requirement (B) “Detection with small time-lag” for a pressure detecting means can be satisfied.

Although estimates {circumflex over (x)}1, {circumflex over (x)}2 of all state variables are obtained by equation (2), it is sufficient to get only the estimate {circumflex over (x)}2 because x1 is detected as output y. Then the high-gain observer is given by equation (12) (non patent literature NPL 2).
{Math. 10}

{circumflex over ({dot over (x)}2=−H{circumflex over (x)}2+H{dot over (y)}+φ0({circumflex over (x)}2, y, u)   (12)

where H: Gain constant of the high-gain observer which is larger than 1. As time-derivative term of output y is included in the right-hand side of equation (12), equation (12) cannot be used as computing equation by itself. But it can be shown that the high-gain observer by equation (12) satisfies the above two requirements (A) and (B). Equation (13) is given from the third equation in equation (1).

{Math. 11}

{dot over (y)}={dot over (x)}1=x2   (13)

Equation (14) is given by using equations (12) and (13).
{Math. 12}

{circumflex over ({dot over (x)}2=−H{circumflex over (x)}2+Hx2+φ0({circumflex over (x)}2, y, u)   (14)

By using the second equation of equation (1), equation (15) is given from equation (14).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          13
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            x
            
              ~
              .
            
          
          2
        
        =
        
          
            
              -
              H
            
            ⁢
            
              
                x
                ~
              
              2
            
          
          +
          
            δ
            ⁡
            
              (
              
                x
                ,
                
                  
                    x
                    ~
                  
                  2
                
                ,
                y
                ,
                u
              
              )
            
          
        
      
    
    
      
        (
        15
        )
      
    
  
  
    
      
        
          
            
              
                
                  
                    x
                    ~
                  
                  2
                
                =
                
                  
                    x
                    2
                  
                  -
                  
                    
                      x
                      ^
                    
                    2
                  
                
              
            
          
          
            
              
                
                  δ
                  ⁡
                  
                    (
                    
                      x
                      ,
                      
                        
                          x
                          ~
                        
                        2
                      
                      ,
                      y
                      ,
                      u
                    
                    )
                  
                
                =
                
                  
                    φ
                    ⁡
                    
                      (
                      
                        x
                        ,
                        u
                      
                      )
                    
                  
                  -
                  
                    
                      φ
                      0
                    
                    ⁡
                    
                      (
                      
                        
                          
                            x
                            ^
                          
                          2
                        
                        ,
                        y
                        ,
                        u
                      
                      )
                    
                  
                
              
            
          
        
        }
      
    
    
      
        (
        16
        )
      
    
  




Gain constant H is given by equation (17) by introducing a positive parameter ε much smaller than 1.




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          14
        
        }
      
    
    
      
        
      
    
  
  
    
      
        H
        =
        
          
            K
            ɛ
          
          ⁢
          
            
          
          ⁢
          
            (
            
              K
              >
              0
            
            )
          
        
      
    
    
      
        (
        17
        )
      
    
  




By using equation (17), equation (15) is rewritten as equation (18).
{Math. 15}

ε{tilde over ({dot over (x)}2=−K{tilde over (x)}2+εδ(x, {tilde over (x)}2, y, u)   (18)

As ε is much smaller than 1, the effect of model error δ on the estimation error {tilde over (x)}2 can be made small enough from equation (18). Therefore by using the high-gain observer for a model which has screw back pressure as a state variable, the above requirement (A) “High-precision detection” for a pressure detecting means can be satisfied.
When the effect of model error δ on the estimation error {tilde over (x)}2 is neglected, equation (18) is rewritten as equation (19).
{Math. 16}

ε{tilde over ({dot over (x)}2=−K{tilde over (x)}2   (19)

The estimation error {tilde over (x)}2 is given by equation (20) from equation (19).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          17
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            
              x
              ~
            
            2
          
          ⁡
          
            (
            t
            )
          
        
        =
        
          
            exp
            ⁡
            
              (
              
                
                  -
                  
                    K
                    ɛ
                  
                
                ⁢
                t
              
              )
            
          
          ⁢
          
            
              x
              ~
            
            20
          
        
      
    
    
      
        (
        20
        )
      
    
  




where {tilde over (x)}20: Initial value of {tilde over (x)}2. As ε is much smaller than 1, equation (20) reveals that the time response {tilde over (x)}2(t) of estimation error tends to zero rapidly. In other words, by using high-gain observer equation (12), the above requirement (B) “Detection with small time-lag” for a pressure detecting means can be satisfied. As in equation (12) the minimum number of state variables to be estimated are included and the measurable state variables are excluded, equation (12) is called by a reduced-order high-gain observer because the order of observer equation (12) is lower than that of observer equation (2).

Then a procedure to modify equation (12) is shown so that the time-derivative term of output y is not appeared. A new variable ŵ is given by equation (21).
{Math. 18}

ŵ={circumflex over (x)}2−Hy   (21)

By using equation (21), equation (12) is rewritten as equation (22).
{Math. 19}

{circumflex over ({dot over (w)}=−H(ŵ+Hy)+φ0(ŵ, y, u)   (22)

Variable ŵ is calculated by equation (22) and estimate {circumflex over (x)}2 is obtained by equation (23).
{Math. 20}

{circumflex over (x)}2=ŵ+Hy   (23)

Procedures of applying a high-gain observer for a model of electric-motor driven injection molding machines which has screw back pressure as a state variable are described in detail in Example to be hereinafter described.
Advantageous Effects of Invention
By applying a high-gain observer for a model of electric-motor driven injection molding machines which has screw back pressure as a state variable, a high-precision pressure detection with small time-lag becomes possible without using a pressure detector. By using the high-gain observer the requirement for a plasticizing controller of electric-motor driven injection molding machines that an adequate screw back pressure is applied to the melted polymer stored at the end of the barrel during the plasticizing process can be satisfied without using a pressure detector and also the five disadvantages described in Background Art can be avoided.



BRIEF DESCRIPTION OF DRAWINGS
FIG. 1 is an explanation drawing of a working example which shows a block diagram of a plasticizing controller for an electric-motor driven injection molding machine according to an embodiment of the present invention.
FIG. 2 is a view which shows an existing plasticizing mechanism of an electric-motor driven injection molding machine.
FIG. 3 is an explanation drawing which shows a block diagram of an existing plasticizing controller for an electric-motor driven injection molding machine.
FIG. 4 is a view which shows a plasticizing mechanism of an electric-motor driven injection molding machine according to an embodiment of the present invention.
FIG. 5 is an explanation drawing of a working example which shows computer simulation conditions of the plasticizing process according to an embodiment of the present invention.
FIG. 6 is an explanation drawing of a working example which shows computer simulation results of screw back pressure estimation by the high-gain observer according to an embodiment of the present invention.



DESCRIPTION OF EMBODIMENT
Hereinafter, the embodiment of the present invention on the plasticizing controller of electric-motor driven injection molding machines is described based on the drawings.
Example
FIG. 4 is a view which shows a plasticizing mechanism of an electric-motor driven injection molding machine without using a pressure detector. As the mechanism in FIG. 4 consists of the parts with the same reference signs as in FIG. 2 except a pressure detector 12, explanations of FIG. 4 are replaced by those of FIG. 2 described in Background Art.
FIG. 1 is an example of a plasticizing controller of an electric-motor driven injection molding machine using a high-gain observer as a screw back pressure detecting means according to an embodiment of the present invention and shows a block diagram of a system configuration for the plasticizing controller. The plasticizing controller consists of a back pressure controller 60 which contains a high-gain observer 27, a motor controller (servoamplifier) for injection 70, a screw revolution speed controller 40 and a motor controller (servoamplifier) for plasticization 50.
The back pressure controller 60 executes a control algorithm at a constant time interval and feeds a discrete-time control demand to the motor controller for injection 70. The back pressure controller 60 consists of a screw back pressure setting device 21, a subtracter 22, a pressure controller 24, a digital/analog (D/A) converter 25, an analog/digital (A/D) converter 26 and a high-gain observer 27.
The screw back pressure setting device 21 feeds a time sequence of screw back pressure command P*b to the subtracter 22.
The actual motor current im detected in the motor controller for injection 70 is fed to the high-gain observer 27 through the A/D converter 26. The backward velocity signal v of the screw 9 is fed to the high-gain observer 27 from the motor controller for injection 70. The signal v is detected by the pulse train from the rotary encoder 14 mounted on the servomotor for injection 3. The screw revolution speed Ns from the motor controller for plasticization 50 is fed to the high-gain observer 27. The high-gain observer 27 executes discrete-time arithmetic expressions which are obtained from a mathematical model of a plasticizing mechanism and outputs an estimate of screw back pressure {circumflex over (P)}b by using the input signals im, v and Ns.
The estimate of screw back pressure {circumflex over (P)}b is fed to the subtracter 22. The subtracter 22 calculates the control deviation ΔPb from screw back pressure command P*b by equation (24).
{Math. 21}

ΔPb=P*b−{circumflex over (P)}b   (24)

The subtracter 22 feeds the control deviation ΔPb to the pressure controller 24.
The pressure controller 24 calculates a motor current demand i*m from ΔPb by using PID control algorithm and feeds the demand i*m to the motor controller for injection 70 through the D/A converter 25.
The motor controller for injection 70 consists of an analog/digital (A/D) converter 31, a PWM device 32, a current transducer 33 of the servomotor for injection 3 and a differentiator 34. The motor controller for injection 70 is connected to the servomotor for injection 3 equipped with the rotary encoder 14.
The motor current demand i*m for the servomotor for injection 3 from the back pressure controller 60 is fed to the A/D converter 31 and the A/D converter 31 feeds the demand i*m to the PWM device 32.
The PWM device 32 applies three-phase voltage to the servomotor for injection 3 so that the servomotor for injection 3 is driven by the motor current demand i*m. The current transducer 33 of the servomotor 3 detects an actual motor current im and the motor current im is fed to the A/D converter 26 in the back pressure controller 60.
The differentiator 34 receives the pulse train from the rotary encoder 14 mounted on the servomotor for injection 3, detects the backward velocity signal v of the screw 9 and feeds the signal v to the high-gain observer 27 in the back pressure controller 60.
The compositions and functions of the screw revolution speed controller 40 and the motor controller for plasticization 50 are already described in detail in Background Art. However, in FIG. 1 the screw revolution speed Ns is fed to the high-gain observer 27 from the differentiator 52 in the motor controller for plasticization 50.
The high-gain observer 27 outputs an estimate {circumflex over (P)}b of screw back pressure by using an actual motor current signal im of the servomotor for injection 3, a screw backward velocity signal v and a screw revolution speed Ns. The mathematical model of a plasticizing mechanism shown in FIG. 4 is derived as follows, which is necessary to design the high-gain observer 27. A motion equation of the servomotor for injection 3 axis is given by equation (25).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          22
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            (
            
              
                J
                M
              
              +
              
                J
                
                  G
                  ⁢
                  
                    
                  
                  ⁢
                  1
                
              
            
            )
          
          ⁢
          
            
              d
              
                ω
                m
              
            
            
              d
              t
            
          
        
        =
        
          
            T
            M
          
          -
          
            
              r
              1
            
            ⁢
            F
          
        
      
    
    
      
        (
        25
        )
      
    
  




where JM: Moment of inertia of motor itself, JG1: Moment of inertia of motor-side gear, wm: Angular velocity of motor, TM: Motor torque, r1: Radius of motor-side gear, F: Transmission force of reduction gear, t: Time variable. A motion equation of the ball screw 5 axis is given by equation (26).





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          23
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            (
            
              
                J
                S
              
              +
              
                J
                
                  G
                  ⁢
                  
                    
                  
                  ⁢
                  2
                
              
            
            )
          
          ⁢
          
            
              d
              
                ω
                s
              
            
            
              d
              t
            
          
        
        =
        
          
            
              r
              2
            
            ⁢
            F
          
          -
          
            T
            a
          
        
      
    
    
      
        (
        26
        )
      
    
  




where JS: Moment of inertia of ball screw axis, JG2: Moment of inertia of load-side gear, ws: Angular velocity of ball screw axis, r2: Radius of load-side gear, Ta: Ball screw drive torque. A motion equation of the moving part 8 is given by equations (27) and (28).





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          24
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            W
            g
          
          ⁢
          
            
              d
              v
            
            
              d
              t
            
          
        
        =
        
          
            F
            a
          
          -
          
            F
            L
          
          -
          
            μ
            ⁢
            
              
            
            ⁢
            W
            ⁢
            
              v
              
                
                v
                
              
            
          
        
      
    
    
      
        (
        27
        )
      
    
  
  
    
      
        
          
            d
            
              x
              s
            
          
          
            d
            t
          
        
        =
        v
      
    
    
      
        (
        28
        )
      
    
  




where W: Weight of the moving part 8, g: Gravity acceleration, v: Backward velocity of the screw (the moving part), xs: Screw position(initial position xs=0), Fa: Drive force of the ball screw, FL: Applied force by polymer to the screw, μ: Friction coefficient at the slider. A relation between ball screw drive force Fa and ball screw drive torque Ta is given by equation (29).





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          25
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          T
          a
        
        =
        
          
            l
            
              2
              ⁢
              
                
              
              ⁢
              π
            
          
          ⁢
          
            1
            η
          
          ⁢
          
            F
            a
          
        
      
    
    
      
        (
        29
        )
      
    
  




where l: Ball screw lead, η: Ball screw efficiency. Equations among v, ws and wm are given by equation (30).





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          26
        
        }
      
    
    
      
        
      
    
  
  
    
      
        v
        =
        
          
            
              l
              
                2
                ⁢
                
                  
                
                ⁢
                π
              
            
            ⁢
            
              ω
              s
            
          
          =
          
            
              l
              
                2
                ⁢
                
                  
                
                ⁢
                π
              
            
            ⁢
            
              
                r
                1
              
              
                r
                2
              
            
            ⁢
            
              ω
              m
            
          
        
      
    
    
      
        (
        30
        )
      
    
  




Applied force to the screw FL is given by equation (31).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          27
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          F
          L
        
        =
        
          
            
              A
              s
            
            ⁢
            
              P
              b
            
          
          +
          
            
              C
              
                m
                ⁢
                
                  
                
                ⁢
                t
              
            
            ⁢
            
              v
              
                
                v
                
              
            
            ⁢
            
              
                
                v
                
              
              γ
            
          
        
      
    
    
      
        (
        31
        )
      
    
  




where As: Screw section area, Pb: Screw back pressure, Cmt: Friction coefficient between the screw and the barrel surface, γ: Velocity power coefficient. A dynamic equation of screw back pressure Pb is given by equations (32) and (33).





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          28
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            
              V
              b
            
            β
          
          ⁢
          
            
              d
              
                P
                b
              
            
            
              d
              t
            
          
        
        =
        
          
            
              A
              s
            
            ⁢
            v
          
          +
          
            Q
            f
          
        
      
    
    
      
        (
        32
        )
      
    
  




Vb=Vb0−Asxs   (33)

where Vb: Polymer volume at the end of a barrel, Vb0: Initial volume of Vb at the start of plasticizing process, Qf: Plasticizing rate (supply flow rate of melted polymer from the screw to the stored polymer at the end of a barrel), β: Bulk modulus of polymer. The characteristics of the servomotor for injection 3 is given by equation (34).

{Math. 29}

TM=KTim   (34)

where KT: Motor torque coefficient of the servomotor for injection 3, im: Motor current of the servomotor for injection 3. By using equations (25), (26) and (30) and deleting ws and F, equation (35) is derived.





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          30
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            {
            
              
                J
                M
              
              +
              
                J
                
                  G
                  ⁢
                  
                    
                  
                  ⁢
                  1
                
              
              +
              
                
                  (
                  
                    
                      J
                      S
                    
                    +
                    
                      J
                      
                        G
                        ⁢
                        
                          
                        
                        ⁢
                        2
                      
                    
                  
                  )
                
                ⁢
                
                  
                    (
                    
                      
                        r
                        1
                      
                      
                        r
                        2
                      
                    
                    )
                  
                  2
                
              
            
            }
          
          ⁢
          
            
              d
              
                ω
                m
              
            
            
              d
              t
            
          
        
        =
        
          
            T
            M
          
          -
          
            
              
                r
                1
              
              
                r
                2
              
            
            ⁢
            
              T
              a
            
          
        
      
    
    
      
        (
        35
        )
      
    
  




By using equations (27), (29), (30) and (35) and deleting Ta and Fa, equation (36) is derived.




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          31
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            J
            eq
          
          ⁢
          
            
              d
              
                ω
                m
              
            
            
              d
              t
            
          
        
        =
        
          
            T
            M
          
          -
          
            
              l
              
                2
                ⁢
                
                  
                
                ⁢
                π
              
            
            ⁢
            
              1
              η
            
            ⁢
            
              
                r
                1
              
              
                r
                2
              
            
            ⁢
            
              (
              
                
                  F
                  L
                
                +
                
                  μ
                  ⁢
                  
                    
                  
                  ⁢
                  W
                  ⁢
                  
                    v
                    
                      
                      v
                      
                    
                  
                
              
              )
            
          
        
      
    
    
      
        (
        36
        )
      
    
  
  
    
      
        
          J
          eq
        
        =
        
          
            J
            M
          
          +
          
            J
            
              G
              ⁢
              
                
              
              ⁢
              1
            
          
          +
          
            
              (
              
                
                  J
                  S
                
                +
                
                  J
                  
                    G
                    ⁢
                    
                      
                    
                    ⁢
                    1
                  
                
              
              )
            
            ⁢
            
              
                (
                
                  
                    r
                    1
                  
                  
                    r
                    2
                  
                
                )
              
              2
            
          
          +
          
            
              W
              g
            
            ⁢
            
              
                (
                
                  
                    r
                    1
                  
                  
                    r
                    2
                  
                
                )
              
              2
            
            ⁢
            
              
                (
                
                  l
                  
                    2
                    ⁢
                    
                      
                    
                    ⁢
                    π
                  
                
                )
              
              2
            
            ⁢
            
              1
              η
            
          
        
      
    
    
      
        (
        37
        )
      
    
  




where Jeq: Reduced moment of inertia at motor axis. Equation (36) is the motion equation of a total plasticizing mechanism converted to the motor axis. From equations (28) and (30), equation (38) is derived.





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          32
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            d
            
              x
              s
            
          
          
            d
            t
          
        
        =
        
          
            
              r
              1
            
            
              r
              2
            
          
          ⁢
          
            l
            
              2
              ⁢
              
                
              
              ⁢
              π
            
          
          ⁢
          
            ω
            m
          
        
      
    
    
      
        (
        38
        )
      
    
  




From equations (31), (34) and (36), the motion equation of a linear motion of the screw is given by equation (39).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          33
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            J
            eq
          
          ⁢
          
            
              d
              
                ω
                m
              
            
            
              d
              t
            
          
        
        =
        
          
            
              K
              T
            
            ⁢
            
              i
              m
            
          
          -
          
            
              l
              
                2
                ⁢
                
                  
                
                ⁢
                π
              
            
            ⁢
            
              1
              η
            
            ⁢
            
              
                r
                1
              
              
                r
                2
              
            
            ⁢
            
              {
              
                
                  
                    A
                    s
                  
                  ⁢
                  
                    P
                    b
                  
                
                +
                
                  
                    C
                    
                      m
                      ⁢
                      
                        
                      
                      ⁢
                      t
                    
                  
                  ⁢
                  
                    v
                    
                      
                      v
                      
                    
                  
                  ⁢
                  
                    
                      
                      v
                      
                    
                    γ
                  
                
                +
                
                  μ
                  ⁢
                  
                    
                  
                  ⁢
                  W
                  ⁢
                  
                    v
                    
                      
                      v
                      
                    
                  
                
              
              }
            
          
        
      
    
    
      
        (
        39
        )
      
    
  




Equation (33) is rewritten as equation (40).
{Math. 34}

Vb=Vb0−Asxs=As(x0−xs)   (40)

where x0: Initial length of the stored melted polymer at the end of the barrel at the start of plasticizing process. By using equations (30) and (40), equation (32) is rewritten as equation (41).





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          35
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            
              
                A
                s
              
              ⁡
              
                (
                
                  
                    x
                    0
                  
                  -
                  
                    x
                    s
                  
                
                )
              
            
            β
          
          ⁢
          
            
              d
              
                P
                b
              
            
            
              d
              t
            
          
        
        =
        
          
            
              A
              s
            
            ⁢
            
              l
              
                2
                ⁢
                
                  
                
                ⁢
                π
              
            
            ⁢
            
              
                r
                1
              
              
                r
                2
              
            
            ⁢
            
              ω
              m
            
          
          +
          
            Q
            f
          
        
      
    
    
      
        (
        41
        )
      
    
  




The variables in the above equations are made dimensionless. By using dimensionless variables, equation (38) is rewritten as equation (42).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          36
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            d
            
              d
              t
            
          
          ⁡
          
            [
            
              
                x
                s
              
              
                x
                max
              
            
            ]
          
        
        =
        
          
            
              l
              
                2
                ⁢
                
                  
                
                ⁢
                π
              
            
            ⁢
            
              
                r
                1
              
              
                r
                2
              
            
            ⁢
            
              
                
                  ω
                  max
                
                
                  x
                  max
                
              
              ⁡
              
                [
                
                  
                    ω
                    m
                  
                  
                    ω
                    max
                  
                
                ]
              
            
          
          =
          
            
              
                v
                max
              
              
                x
                max
              
            
            ⁡
            
              [
              
                
                  ω
                  m
                
                
                  ω
                  max
                
              
              ]
            
          
        
      
    
    
      
        (
        42
        )
      
    
  




As a positive rotation of the servomotor for injection 3 corresponds to an injection direction of the screw 9, screw position xs and screw backward velocity v become negative in the plasticizing process. vmax(>0) is the maximum velocity of screw backward movement in the plasticizing process. wmax(>0) is the maximum revolution speed of the servomotor for injection corresponding to vmax·xmax(>0) is the maximum stroke of screw backward movement in the plasticizing process.
By using dimensionless variables, equation (39) is rewritten as equation (43).




  
    
      
        
          
        
        ⁢
        
          {
          
            Math
            .
            
              
            
            ⁢
            37
          
          }
        
      
    
    
      
        
      
    
  
  
    
      
        
          
            J
            eq
          
          ⁢
          
            ω
            max
          
          ⁢
          
            
              d
              
                d
                t
              
            
            ⁡
            
              [
              
                
                  ω
                  m
                
                
                  ω
                  max
                
              
              ]
            
          
        
        =
        
          
            
              K
              T
            
            ⁢
            
              
                i
                max
              
              ⁡
              
                [
                
                  
                    i
                    m
                  
                  
                    i
                    max
                  
                
                ]
              
            
          
          -
          
            
              l
              
                2
                ⁢
                π
              
            
            ⁢
            
              1
              η
            
            ⁢
            
              
                r
                1
              
              
                r
                2
              
            
            ⁢
            
              A
              s
            
            ⁢
            
              
                P
                max
              
              ⁡
              
                [
                
                  
                    P
                    b
                  
                  
                    P
                    max
                  
                
                ]
              
            
          
          -
          
            
              l
              
                2
                ⁢
                π
              
            
            ⁢
            
              1
              η
            
            ⁢
            
              
                r
                1
              
              
                r
                2
              
            
            ⁢
            
              
                [
                
                  
                    ω
                    m
                  
                  
                    ω
                    max
                  
                
                ]
              
              
                
                
                  [
                  
                    
                      ω
                      m
                    
                    
                      ω
                      max
                    
                  
                  ]
                
                
              
            
            ⁢
            
              {
              
                
                  
                    C
                    mt
                  
                  ⁢
                  
                    υ
                    max
                    γ
                  
                  ⁢
                  
                    
                      
                      
                        [
                        
                          
                            ω
                            m
                          
                          
                            ω
                            max
                          
                        
                        ]
                      
                      
                    
                    γ
                  
                
                +
                
                  μ
                  ⁢
                  
                    
                  
                  ⁢
                  W
                
              
              }
            
          
        
      
    
    
      
        (
        43
        )
      
    
  




where imax: Motor current rating of the servomotor for injection 3, Pmax: Maximum screw back pressure. In deriving equation (43), equation (44) is used.





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          38
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          [
          
            υ
            
              υ
              max
            
          
          ]
        
        =
        
          [
          
            
              ω
              m
            
            
              ω
              max
            
          
          ]
        
      
    
    
      
        (
        44
        )
      
    
  




Equation (43) is rewritten as equation (45).




  
    
      
        
          
        
        ⁢
        
          {
          
            Math
            .
            
              
            
            ⁢
            39
          
          }
        
      
    
    
      
        
      
    
  
  
    
      
        
          
            d
            
              d
              t
            
          
          ⁡
          
            [
            
              
                ω
                m
              
              
                ω
                max
              
            
            ]
          
        
        =
        
          
            
              
                T
                Mmax
              
              
                
                  J
                  eq
                
                ⁢
                
                  ω
                  max
                
              
            
            ⁡
            
              [
              
                
                  i
                  m
                
                
                  i
                  max
                
              
              ]
            
          
          -
          
            
              l
              
                2
                ⁢
                π
              
            
            ⁢
            
              1
              η
            
            ⁢
            
              
                r
                1
              
              
                r
                2
              
            
            ⁢
            
              
                
                  
                    A
                    s
                  
                  ⁢
                  
                    P
                    max
                  
                
                
                  
                    J
                    eq
                  
                  ⁢
                  
                    ω
                    max
                  
                
              
              ⁡
              
                [
                
                  
                    P
                    b
                  
                  
                    P
                    max
                  
                
                ]
              
            
          
          -
          
            
              l
              
                2
                ⁢
                π
              
            
            ⁢
            
              1
              η
            
            ⁢
            
              
                r
                1
              
              
                r
                2
              
            
            ⁢
            
              1
              
                
                  J
                  eq
                
                ⁢
                
                  ω
                  max
                
              
            
            ⁢
            
              
                [
                
                  
                    ω
                    m
                  
                  
                    ω
                    max
                  
                
                ]
              
              
                
                
                  [
                  
                    
                      ω
                      m
                    
                    
                      ω
                      max
                    
                  
                  ]
                
                
              
            
            ⁢
            
              {
              
                
                  
                    C
                    mt
                  
                  ⁢
                  
                    υ
                    max
                    γ
                  
                  ⁢
                  
                    
                      
                      
                        [
                        
                          
                            ω
                            m
                          
                          
                            ω
                            max
                          
                        
                        ]
                      
                      
                    
                    γ
                  
                
                +
                
                  μ
                  ⁢
                  
                    
                  
                  ⁢
                  W
                
              
              }
            
          
        
      
    
    
      
        (
        45
        )
      
    
  




where TMmax=KTimax: Motor rating torque of the servomotor for injection 3.

By using dimensionless variables, equation (41) is rewritten as equation (46).




  
    
      
        
          
        
        ⁢
        
          {
          
            Math
            .
            
              
            
            ⁢
            40
          
          }
        
      
    
    
      
        
      
    
  
  
    
      
        
          
            1
            β
          
          ⁢
          
            A
            s
          
          ⁢
          
            x
            max
          
          ⁢
          
            P
            max
          
          ⁢
          
            {
            
              
                [
                
                  
                    x
                    0
                  
                  
                    x
                    max
                  
                
                ]
              
              -
              
                [
                
                  
                    x
                    s
                  
                  
                    x
                    max
                  
                
                ]
              
            
            }
          
          ⁢
          
            
              d
              
                d
                t
              
            
            ⁡
            
              [
              
                
                  P
                  b
                
                
                  P
                  max
                
              
              ]
            
          
        
        =
        
          
            A
            s
          
          ⁢
          
            υ
            max
          
          ⁢
          
            {
            
              
                [
                
                  
                    ω
                    m
                  
                  
                    ω
                    max
                  
                
                ]
              
              +
              
                
                  
                    υ
                    fmax
                  
                  
                    υ
                    max
                  
                
                ⁡
                
                  [
                  
                    
                      Q
                      f
                    
                    
                      Q
                      max
                    
                  
                  ]
                
              
            
            }
          
        
      
    
    
      
        (
        46
        )
      
    
  




where Qmax=Asvfmax: Maximum plasticizing rate. vfmax(>0) is the screw backward velocity corresponding to the maximum plasticizing rate Qmax. Equation (46) is rewritten as equation (47).





  
    
      
        
          
        
        ⁢
        
          {
          
            Math
            .
            
              
            
            ⁢
            41
          
          }
        
      
    
    
      
        
      
    
  
  
    
      
        
          
            d
            
              d
              t
            
          
          ⁡
          
            [
            
              
                P
                b
              
              
                P
                max
              
            
            ]
          
        
        =
        
          
            β
            
              
                [
                
                  
                    x
                    0
                  
                  
                    x
                    max
                  
                
                ]
              
              -
              
                [
                
                  
                    x
                    s
                  
                  
                    x
                    max
                  
                
                ]
              
            
          
          ⁢
          
            
              υ
              max
            
            
              
                x
                max
              
              ⁢
              
                P
                max
              
            
          
          ⁢
          
            {
            
              
                [
                
                  
                    ω
                    m
                  
                  
                    ω
                    max
                  
                
                ]
              
              +
              
                
                  
                    υ
                    fmax
                  
                  
                    υ
                    max
                  
                
                ⁡
                
                  [
                  
                    
                      Q
                      f
                    
                    
                      Q
                      max
                    
                  
                  ]
                
              
            
            }
          
        
      
    
    
      
        (
        47
        )
      
    
  




In general dimensionless plasticizing rate [Qf/Qmax] is a function of dimensionless screw back pressure [Pb/Pmax] and dimensionless screw revolution speed [Ns/Nmax] given by equation (48). Nmax is the maximum screw revolution speed.




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          42
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          [
          
            
              Q
              f
            
            
              Q
              max
            
          
          ]
        
        =
        
          f
          ⁡
          
            (
            
              
                [
                
                  
                    P
                    b
                  
                  
                    P
                    max
                  
                
                ]
              
              ,
              
                [
                
                  
                    N
                    s
                  
                  
                    N
                    max
                  
                
                ]
              
            
            )
          
        
      
    
    
      
        (
        48
        )
      
    
  




The mathematical model of a plasticizing mechanism necessary for designing the high-gain observer 27 is given by equations (49), (50) and (51) by using equations (42), (45), (47) and (48).




  
    
      
        
          
        
        ⁢
        
          {
          
            Math
            .
            
              
            
            ⁢
            43
          
          }
        
      
    
    
      
        
      
    
  
  
    
      
        
          
            d
            
              d
              t
            
          
          ⁡
          
            [
            
              
                x
                s
              
              
                x
                max
              
            
            ]
          
        
        =
        
          
            
              υ
              max
            
            
              x
              max
            
          
          ⁡
          
            [
            
              
                ω
                m
              
              
                ω
                max
              
            
            ]
          
        
      
    
    
      
        (
        49
        )
      
    
  
  
    
      
        
          
            d
            
              d
              t
            
          
          ⁡
          
            [
            
              
                ω
                m
              
              
                ω
                max
              
            
            ]
          
        
        =
        
          
            
              
                T
                Mmax
              
              
                
                  J
                  eq
                
                ⁢
                
                  ω
                  max
                
              
            
            ⁡
            
              [
              
                
                  i
                  m
                
                
                  i
                  max
                
              
              ]
            
          
          -
          
            
              l
              
                2
                ⁢
                π
              
            
            ⁢
            
              1
              η
            
            ⁢
            
              
                r
                1
              
              
                r
                2
              
            
            ⁢
            
              
                
                  
                    A
                    s
                  
                  ⁢
                  
                    P
                    max
                  
                
                
                  
                    J
                    eq
                  
                  ⁢
                  
                    ω
                    max
                  
                
              
              ⁡
              
                [
                
                  
                    P
                    b
                  
                  
                    P
                    max
                  
                
                ]
              
            
          
          -
          
            
              l
              
                2
                ⁢
                π
              
            
            ⁢
            
              1
              η
            
            ⁢
            
              
                r
                1
              
              
                r
                2
              
            
            ⁢
            
              1
              
                
                  J
                  eq
                
                ⁢
                
                  ω
                  max
                
              
            
            ⁢
            
              
                [
                
                  
                    ω
                    m
                  
                  
                    ω
                    max
                  
                
                ]
              
              
                
                
                  [
                  
                    
                      ω
                      m
                    
                    
                      ω
                      max
                    
                  
                  ]
                
                
              
            
            ⁢
            
              {
              
                
                  
                    C
                    mt
                  
                  ⁢
                  
                    υ
                    max
                    γ
                  
                  ⁢
                  
                    
                      
                      
                        [
                        
                          
                            ω
                            m
                          
                          
                            ω
                            max
                          
                        
                        ]
                      
                      
                    
                    γ
                  
                
                +
                
                  μ
                  ⁢
                  
                    
                  
                  ⁢
                  W
                
              
              }
            
          
        
      
    
    
      
        (
        50
        )
      
    
  
  
    
      
        
          
            d
            
              d
              t
            
          
          ⁡
          
            [
            
              
                P
                b
              
              
                P
                max
              
            
            ]
          
        
        =
        
          
            β
            
              
                [
                
                  
                    x
                    0
                  
                  
                    x
                    max
                  
                
                ]
              
              -
              
                [
                
                  
                    x
                    s
                  
                  
                    x
                    max
                  
                
                ]
              
            
          
          ⁢
          
            
              υ
              max
            
            
              
                x
                max
              
              ⁢
              
                P
                max
              
            
          
          ⁢
          
            {
            
              
                [
                
                  
                    ω
                    m
                  
                  
                    ω
                    max
                  
                
                ]
              
              +
              
                
                  
                    υ
                    fmax
                  
                  
                    υ
                    max
                  
                
                ⁢
                
                  f
                  ⁡
                  
                    (
                    
                      
                        [
                        
                          
                            P
                            b
                          
                          
                            P
                            max
                          
                        
                        ]
                      
                      ,
                      
                        [
                        
                          
                            N
                            s
                          
                          
                            N
                            max
                          
                        
                        ]
                      
                    
                    )
                  
                
              
            
            }
          
        
      
    
    
      
        (
        51
        )
      
    
  




When the dimensionless plasticizing rate [Q f/Qmax] is assumed to be proportional to the screw revolution speed, equation (48) is given by equation (52).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          44
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          f
          ⁡
          
            (
            
              
                [
                
                  
                    P
                    b
                  
                  
                    P
                    max
                  
                
                ]
              
              ,
              
                [
                
                  
                    N
                    s
                  
                  
                    N
                    max
                  
                
                ]
              
            
            )
          
        
        =
        
          
            [
            
              
                N
                s
              
              
                N
                max
              
            
            ]
          
          ⁢
          
            g
            ⁡
            
              (
              
                [
                
                  
                    P
                    b
                  
                  
                    P
                    max
                  
                
                ]
              
              )
            
          
        
      
    
    
      
        (
        52
        )
      
    
  




The following state variables x1, x2 and x3 defined by equation (53) are introduced.




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          45
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            
              
                x
                1
              
              =
              
                
                  x
                  s
                
                
                  x
                  max
                
              
            
          
          
            
              
                x
                2
              
              =
              
                
                  ω
                  m
                
                
                  ω
                  max
                
              
            
          
          
            
              
                x
                3
              
              =
              
                
                  P
                  b
                
                
                  P
                  max
                
              
            
          
        
      
    
    
      
        (
        53
        )
      
    
  




Input variables u1, u2 defined by equation (54) are introduced. u1, u2 are measurable. In the design of high-gain observer 27, the actual motor current im of the servomotor for injection 3 is considered to be equal to motor current demand i*m because the time lag between i*m and im is very small.




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          46
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          u
          1
        
        =
        
          
            
              
                i
                m
              
              
                i
                max
              
            
            ⁢
            
              
            
            ⁢
            
              u
              2
            
          
          =
          
            
              N
              s
            
            
              N
              max
            
          
        
      
    
    
      
        (
        54
        )
      
    
  




The state variable x2 is supposed to be measurable and output variable y is defined by equation (55).
{Math. 47}

y=x2   (55)

The state equations and the output equation representing equations (49), (50), (51), (52) and (55) are given by equations (56) ̃(59).
{Math. 48}

{dot over (x)}1=ax2  (56)

{dot over (x)}2=bx3+χ(x2)+cu1   (57)





  
    
      
        
          
            x
            .
          
          3
        
        =
        
          
            
              d
              
                e
                -
                
                  x
                  1
                
              
            
            ⁢
            
              {
              
                
                  x
                  2
                
                +
                
                  
                    qu
                    2
                  
                  ⁢
                  
                    g
                    ⁡
                    
                      (
                      
                        x
                        3
                      
                      )
                    
                  
                
              
              }
            
          
          =
          
            ψ
            ⁡
            
              (
              
                x
                ,
                
                  u
                  2
                
              
              )
            
          
        
      
    
    
      
        (
        58
        )
      
    
  




y=x2   (59)





  
    
      
        
          
            
              
                x
                =
                
                  [
                  
                    
                      
                        
                          x
                          1
                        
                      
                    
                    
                      
                        
                          x
                          2
                        
                      
                    
                    
                      
                        
                          x
                          3
                        
                      
                    
                  
                  ]
                
              
              ⁢
              
                
              
            
          
          
            
              
                χ
                ⁡
                
                  (
                  
                    x
                    2
                  
                  )
                
              
              =
              
                
                  
                    x
                    2
                  
                  
                    
                    
                      x
                      2
                    
                    
                  
                
                ⁢
                
                  (
                  
                    
                      h
                      ⁢
                      
                        
                          
                          
                            x
                            2
                          
                          
                        
                        γ
                      
                    
                    +
                    p
                  
                  )
                
              
            
          
        
      
    
    
      
        (
        60
        )
      
    
  
  
    
      
        
          
            
              
                a
                =
                
                  
                    υ
                    max
                  
                  
                    x
                    max
                  
                
              
            
            
              
                b
                =
                
                  
                    -
                    
                      l
                      
                        2
                        ⁢
                        π
                      
                    
                  
                  ⁢
                  
                    1
                    η
                  
                  ⁢
                  
                    
                      r
                      1
                    
                    
                      r
                      2
                    
                  
                  ⁢
                  
                    
                      
                        A
                        s
                      
                      ⁢
                      
                        P
                        max
                      
                    
                    
                      
                        J
                        eq
                      
                      ⁢
                      
                        w
                        max
                      
                    
                  
                
              
            
          
          
            
              
                c
                =
                
                  
                    T
                    Mmax
                  
                  
                    
                      J
                      eq
                    
                    ⁢
                    
                      ω
                      max
                    
                  
                
              
            
            
              
                d
                =
                
                  
                    β
                    ⁢
                    
                      
                    
                    ⁢
                    
                      υ
                      max
                    
                  
                  
                    
                      x
                      max
                    
                    ⁢
                    
                      P
                      max
                    
                  
                
              
            
          
          
            
              
                e
                =
                
                  
                    x
                    0
                  
                  
                    x
                    max
                  
                
              
            
            
              
                h
                =
                
                  
                    -
                    
                      l
                      
                        2
                        ⁢
                        π
                      
                    
                  
                  ⁢
                  
                    1
                    η
                  
                  ⁢
                  
                    
                      r
                      1
                    
                    
                      r
                      2
                    
                  
                  ⁢
                  
                    
                      
                        C
                        mt
                      
                      ⁢
                      
                        υ
                        max
                        γ
                      
                    
                    
                      
                        J
                        eq
                      
                      ⁢
                      
                        ω
                        max
                      
                    
                  
                
              
            
          
          
            
              
                p
                =
                
                  
                    -
                    
                      l
                      
                        2
                        ⁢
                        π
                      
                    
                  
                  ⁢
                  
                    1
                    η
                  
                  ⁢
                  
                    
                      r
                      1
                    
                    
                      r
                      2
                    
                  
                  ⁢
                  
                    
                      μ
                      ⁢
                      
                        
                      
                      ⁢
                      W
                    
                    
                      
                        J
                        eq
                      
                      ⁢
                      
                        ω
                        max
                      
                    
                  
                
              
            
            
              
                q
                =
                
                  
                    υ
                    fmax
                  
                  
                    ω
                    max
                  
                
              
            
          
        
        }
      
    
    
      
        (
        61
        )
      
    
  




where χ(x2) and ψ(x, u2) are nonlinear functions.

As the output variable y=x2 represented by equation (59) is measurable, by using the above equation (56) the state variable x1 is calculated by the following equation (62) and is replaced by a variable ys. The variable ys represents a dimensionless screw position and an initial value of ys is assumed to be 0.
{Math. 49}

x1=∫ax2dt=a∫ydt=ys   (62)

Therefore, the state variable x1 is removed from the state variables and a new state equation and a new output equation are represented by the following equations (63) and (64) by using equations (57) ̃(59).




  
    
      
        
          
        
        ⁢
        
          {
          
            Math
            .
            
              
            
            ⁢
            50
          
          }
        
      
    
    
      
        
      
    
  
  
    
      
        
          [
          
            
              
                
                  
                    x
                    .
                  
                  2
                
              
            
            
              
                
                  
                    x
                    .
                  
                  3
                
              
            
          
          ]
        
        =
        
          
            
              
                [
                
                  
                    
                      0
                    
                    
                      b
                    
                  
                  
                    
                      0
                    
                    
                      0
                    
                  
                
                ]
              
              ⁡
              
                [
                
                  
                    
                      
                        x
                        2
                      
                    
                  
                  
                    
                      
                        x
                        3
                      
                    
                  
                
                ]
              
            
            +
            
              [
              
                
                  
                    
                      
                        χ
                        ⁡
                        
                          (
                          
                            x
                            2
                          
                          )
                        
                      
                      +
                      
                        cu
                        1
                      
                    
                  
                
                
                  
                    
                      ψ
                      ⁡
                      
                        (
                        
                          
                            x
                            2
                          
                          ,
                          
                            x
                            3
                          
                          ,
                          
                            u
                            2
                          
                          ,
                          
                            y
                            s
                          
                        
                        )
                      
                    
                  
                
              
              ]
            
          
          =
          
             
            
              
                
                  [
                  
                    
                      
                        
                          A
                          11
                        
                      
                      
                        
                          A
                          12
                        
                      
                    
                    
                      
                        
                          A
                          21
                        
                      
                      
                        
                          A
                          22
                        
                      
                    
                  
                  ]
                
                ⁢
                
                  
                
                [
                
                  
                
                ⁢
                
                  
                    
                      
                        x
                        2
                      
                    
                  
                  
                    
                      
                        x
                        3
                      
                    
                  
                
                ]
              
              +
              
                [
                
                  
                    
                      
                        
                          χ
                          ⁡
                          
                            (
                            
                              x
                              2
                            
                            )
                          
                        
                        +
                        
                          cu
                          1
                        
                      
                    
                  
                  
                    
                      
                        ψ
                        ⁡
                        
                          (
                          
                            
                              x
                              2
                            
                            ,
                            
                              x
                              3
                            
                            ,
                            
                              u
                              2
                            
                            ,
                            
                              y
                              s
                            
                          
                          )
                        
                      
                    
                  
                
                ]
              
            
          
        
      
    
    
      
        (
        63
        )
      
    
  
  
    
      
        y
        =
        
          [
          
            
              
                
                  1
                
                
                  
                    0
                    ]
                  
                
              
            
            ⁡
            
              [
              
                
                  
                    
                      x
                      2
                    
                  
                
                
                  
                    
                      x
                      3
                    
                  
                
              
              ]
            
          
        
      
    
    
      
        (
        64
        )
      
    
  
  
    
      
        
          
            
              
                χ
                ⁡
                
                  (
                  
                    x
                    2
                  
                  )
                
              
              =
              
                
                  
                    x
                    2
                  
                  
                    
                    
                      x
                      2
                    
                    
                  
                
                ⁢
                
                  (
                  
                    
                      h
                      ⁢
                      
                        
                          
                          
                            x
                            2
                          
                          
                        
                        γ
                      
                    
                    +
                    p
                  
                  )
                
              
            
          
          
            
              
                ψ
                ⁡
                
                  (
                  
                    
                      x
                      2
                    
                    ,
                    
                      x
                      3
                    
                    ,
                    
                      u
                      2
                    
                    ,
                    
                      y
                      s
                    
                  
                  )
                
              
              =
              
                
                  d
                  
                    e
                    -
                    
                      y
                      s
                    
                  
                
                ⁢
                
                  {
                  
                    
                      x
                      2
                    
                    +
                    
                      
                        qu
                        2
                      
                      ⁢
                      
                        g
                        ⁡
                        
                          (
                          
                            x
                            3
                          
                          )
                        
                      
                    
                  
                  }
                
              
            
          
        
      
    
    
      
        (
        65
        )
      
    
  




The variable ys in the state equation (63) is considered to be a new input variable in addition to the input variables u1, u2 and the input variable ys is given by the following equation (66) by equation (62).
{Math. 51}

ys=a∫ydt   (66)

As state variable x2 is measurable, it is not necessary to estimate state variable x2. Therefore, the high-gain observer 27 outputs the estimate of state variable x3 by using the measurable screw backward velocity signal y=x2, the actual motor current u1 and the screw revolution speed u2. The estimate {circumflex over (x)}3 is given by the following equation (68) (non patent literature NPL 2). Input variable ys in equation (68) is calculated in the high-gain observer 27 by using a time integration method of equation (66) applied to the measurable screw backward velocity y=x2. K is a gain constant of the high-gain observer 27.
{Math. 52}

{circumflex over ({dot over (x)}3=(A22+KA12){circumflex over (x)}3−K{{dot over (y)}−A11y−χ0(y)−cu1}+A21y+ψ0({circumflex over (x)}3, u2, y, ys)   (67)

{circumflex over ({dot over (x)}3=Kb{circumflex over (x)}3−K{{dot over (y)}−χ0(y)−cu1}+ψ0({circumflex over (x)}3, u2, y, ys)   (68)

where χ0(y), ψ0({circumflex over (x)}3, u2, y, ys): Nominal functions of χ(y), ψ({circumflex over (x)}3, u2, y, ys), respectively, used in the high-gain observer 27. Equation (68) is rewritten by equation (69).

{Math. 53}

{circumflex over ({dot over (x)}3+K{dot over (y)}=Kb{circumflex over (x)}3+K{χ0(y)+cu1}+ψ0({circumflex over (x)}3, u2, y, ys)   (69)

A new variable ŵ is introduced by the following equation (70).
{Math. 54}

ŵ={circumflex over (x)}3+Ky   (70)

The estimate {circumflex over (x)}3 is given by equations (71) and (72) by using equations (69) and (70).
{Math. 55}

{circumflex over ({dot over (w)}=Kb(ŵ−Ky)+K{χ0(y)+cu1}+ψ0(ŵ, u2, y, ys)   (71)

{circumflex over (x)}3=ŵ−Ky   (72)

A positive parameter ε much smaller than 1 is introduced and the gain constant K is given by equation (73) and a new variable {circumflex over (η)} is introduced by equation (74).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          56
        
        }
      
    
    
      
        
      
    
  
  
    
      
        K
        =
        
          
            K
            1
          
          ɛ
        
      
    
    
      
        (
        73
        )
      
    
  
  
    
      
        
          η
          ^
        
        =
        
          ɛ
          ⁢
          
            ω
            ^
          
        
      
    
    
      
        (
        74
        )
      
    
  




Equation (71) is rewritten as the following equation (75) by using equations (73) and (74).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          57
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            η
            ^
          
          .
        
        =
        
          
            
              
                K
                1
              
              ɛ
            
            ⁢
            
              b
              ⁡
              
                (
                
                  
                    η
                    ^
                  
                  -
                  
                    
                      K
                      1
                    
                    ⁢
                    y
                  
                
                )
              
            
          
          +
          
            
              K
              
                1
                ⁢
                χ
                ⁢
                
                  
                
                ⁢
                0
              
            
            ⁡
            
              (
              y
              )
            
          
          +
          
            
              K
              1
            
            ⁢
            
              cu
              1
            
          
          +
          
            ɛ
            ⁢
            
              
            
            ⁢
            
              
                ψ
                0
              
              ⁡
              
                (
                
                  
                    η
                    ^
                  
                  ,
                  
                    u
                    2
                  
                  ,
                  y
                  ,
                  
                    y
                    s
                  
                
                )
              
            
          
        
      
    
    
      
        (
        75
        )
      
    
  




The following equation (76) is given from equation (74).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          58
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          w
          ^
        
        =
        
          
            1
            ɛ
          
          ⁢
          
            η
            ^
          
        
      
    
    
      
        (
        76
        )
      
    
  




By using equation (76), equation (72) is rewritten as the following equation (77).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          59
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            x
            ^
          
          3
        
        =
        
          
            
              1
              ɛ
            
            ⁢
            
              η
              ^
            
          
          -
          Ky
        
      
    
    
      
        (
        77
        )
      
    
  




Thus the estimate of state variable {circumflex over (x)}3 is obtained by the high-gain observer 27. From equations (66), (75) and (77), the calculation procedures are given by equations (78), (79) and (80).
(1) Calculation Procedure 1
{Math. 60}

ys=a∫ydt   (78)

(2) Calculation Procedure 2





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          61
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            η
            ^
          
          .
        
        =
        
          
            
              
                K
                1
              
              ɛ
            
            ⁢
            
              b
              ⁡
              
                (
                
                  
                    η
                    ^
                  
                  -
                  
                    
                      K
                      1
                    
                    ⁢
                    y
                  
                
                )
              
            
          
          +
          
            
              K
              1
            
            ⁢
            
              
                χ
                0
              
              ⁡
              
                (
                y
                )
              
            
          
          +
          
            
              K
              1
            
            ⁢
            
              cu
              1
            
          
          +
          
            
              ɛψ
              0
            
            ⁡
            
              (
              
                
                  η
                  ^
                
                ,
                
                  u
                  2
                
                ,
                y
                ,
                
                  y
                  s
                
              
              )
            
          
        
      
    
    
      
        (
        79
        )
      
    
  




(3) Calculation Procedure 3





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          62
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            x
            ^
          
          3
        
        =
        
          
            1
            ɛ
          
          ⁢
          
            (
            
              
                η
                ^
              
              -
              
                
                  K
                  1
                
                ⁢
                y
              
            
            )
          
        
      
    
    
      
        (
        80
        )
      
    
  




By the calculation procedure 1, ys is calculated, by the calculation procedure 2, the estimate {circumflex over (η)} is obtained and by the calculation procedure 3 the estimate {circumflex over (x)}3 is obtained.
Then it is shown that the high-gain observer 27 as the pressure detecting means satisfies the following two requirements (A) and (B) described in Solution to Problem.
(A) The detection means is high-precision.
(B) The detection means has very small time-lag.
If the nominal functions χ0(y) and ψ0({circumflex over (η)}, u2, y, ys) in equation (79) are replaced with the true but actually unobtainable functions χ(y) and ψ(η, u2, y, ys), the true value η of the estimate {circumflex over (η)} may be obtained by equation (81).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          63
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          η
          .
        
        =
        
          
            
              
                K
                1
              
              ɛ
            
            ⁢
            
              b
              ⁡
              
                (
                
                  η
                  -
                  
                    
                      K
                      1
                    
                    ⁢
                    y
                  
                
                )
              
            
          
          +
          
            
              K
              1
            
            ⁢
            
              χ
              ⁡
              
                (
                y
                )
              
            
          
          +
          
            
              K
              1
            
            ⁢
            
              cu
              1
            
          
          +
          
            ɛψ
            ⁡
            
              (
              
                η
                ,
                
                  u
                  2
                
                ,
                y
                ,
                
                  y
                  s
                
              
              )
            
          
        
      
    
    
      
        (
        81
        )
      
    
  




Then the estimate error {tilde over (η)}=η−{circumflex over (η)} is obtained by equation (82) by using equations (79) and (81).
{Math. 64}

ε{dot over ({tilde over (η)}=K1b{tilde over (η)}+εK1δ1(y)+ε2δ2({tilde over (η)}, u2, y, ys)   (82)





  
    
      
        
          
            
              
                
                ⁢
                
                  
                    
                      δ
                      1
                    
                    ⁡
                    
                      (
                      y
                      )
                    
                  
                  =
                  
                    
                      χ
                      ⁡
                      
                        (
                        y
                        )
                      
                    
                    -
                    
                      
                        χ
                        0
                      
                      ⁡
                      
                        (
                        y
                        )
                      
                    
                  
                
              
            
          
          
            
              
                
                ⁢
                
                  
                    
                      δ
                      2
                    
                    ⁡
                    
                      (
                      
                        
                          η
                          ~
                        
                        ,
                        
                          u
                          2
                        
                        ,
                        y
                        ,
                        
                          y
                          s
                        
                      
                      )
                    
                  
                  =
                  
                    
                      ψ
                      ⁡
                      
                        (
                        
                          η
                          ,
                          
                            u
                            2
                          
                          ,
                          y
                          ,
                          
                            y
                            s
                          
                        
                        )
                      
                    
                    -
                    
                      
                        ψ
                        0
                      
                      ⁡
                      
                        (
                        
                          
                            η
                            ^
                          
                          ,
                          
                            u
                            2
                          
                          ,
                          y
                          ,
                          
                            y
                            s
                          
                        
                        )
                      
                    
                  
                
              
            
          
        
        }
      
    
    
      
        (
        83
        )
      
    
  




As ε is much smaller than 1, the effects of model errors δ1 and δ2 on the estimation error {tilde over (η)} can be made small enough by equation (82). In other words, the high-gain observer 27 satisfies the above requirement (A) “High-precision detection” for screw back pressure estimate {circumflex over (x)}3 obtained by equations (78), (79) and (80).
When the effects of model errors δ1 and δ2 on the estimation error {tilde over (η)} are neglected in equation (82), equation (82) is rewritten as equation (84).
{Math. 65}

ε{dot over ({tilde over (η)}=K1b{tilde over (η)}  (84)

The estimate error {tilde over (η)} is given by the following equation (85) from equation (84).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          66
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            
              
                
                  η
                  ~
                
                ⁡
                
                  (
                  t
                  )
                
              
              =
              
                
                  exp
                  ⁡
                  
                    (
                    
                      
                        
                          
                            K
                            1
                          
                          ⁢
                          b
                        
                        ɛ
                      
                      ⁢
                      t
                    
                    )
                  
                
                ⁢
                
                  
                    η
                    ^
                  
                  0
                
              
            
          
          
            
              (
              
                
                  
                    
                      
                        
                          K
                          1
                        
                        >
                        0
                      
                      ⁢
                      
                        
                      
                    
                  
                  
                    
                      b
                      <
                      0
                    
                  
                
              
              )
            
          
        
      
    
    
      
        (
        85
        )
      
    
  




where t: Time variable, {tilde over (η)}0: Initial value of estimate error {tilde over (η)}. As b<0 in the plasticization process of injection molding machines and ε is much smaller than 1, equation (85) reveals that the time response {tilde over (η)}(t) of the estimate error tends to zero rapidly. In other words, the high-gain observer 27 satisfies the above requirement (B) “Detection with small time-lag” for screw back pressure estimate {circumflex over (x)}3 obtained by equations (78), (79) and (80).

As the back pressure controller 60 executes a control algorithm at a constant time interval Δt, the arithmetic expressions (78), (79) and (80) of the high-gain observer 27 are transformed into the discrete-time arithmetic expressions (non patent literature NPL 3, NPL 4).
A new parameter α is introduced and the time interval Δt is expressed by equation (86).
{Math. 67}

Δt=αε  (86)

A discrete-time expression of a time integration equation (78) can be found by using the standard method of trapezoid rule and is given by the following equation (87).
{Math. 68}

ys(tk+1)=ys(tk)+0.5 aαε{y(tk)+y(tk+1)}  (87)

When function values ys(tk), y(tk) at the discrete time tk(k=0, 1, 2, . . . ) are represented by ys(k), y(k), equation (87) is given by the following equation (88).
{Math. 69}

ys(k+1)=ys(k)+0.5 aαε{y(k)+y(k+1)}  (88)

As the time interval Δt is small, the numerical time integration equation (88) of the output variable y(t) is considered to be high-precision.
Next, a discrete-time equivalent of the continuous-time equation (79) can be found by using the standard method of forward rectangular rule which gives the relation between the Laplace-transform operator s representing time-derivative operation and z-transform operator z as follows.




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          70
        
        }
      
    
    
      
        
      
    
  
  
    
      
        s
        =
        
          
            
              z
              -
              1
            
            
              Δ
              ⁢
              
                
              
              ⁢
              t
            
          
          =
          
            
              z
              -
              1
            
            αɛ
          
        
      
    
    
      
        (
        89
        )
      
    
  




By using equation (89), equation (79) is rewritten as the following equation (90).




  
    
      
        
          
        
        ⁢
        
          {
          
            Math
            .
            
              
            
            ⁢
            71
          
          }
        
      
    
    
      
        
      
    
  
  
    
      
        
          
            
              z
              -
              1
            
            αɛ
          
          ⁢
          
            η
            ^
          
        
        =
        
          
            
              
                K
                1
              
              ɛ
            
            ⁢
            
              b
              ⁡
              
                (
                
                  
                    η
                    ^
                  
                  -
                  
                    
                      K
                      1
                    
                    ⁢
                    y
                  
                
                )
              
            
          
          +
          
            
              K
              1
            
            ⁢
            
              
                χ
                0
              
              ⁡
              
                (
                y
                )
              
            
          
          +
          
            
              K
              1
            
            ⁢
            
              cu
              1
            
          
          +
          
            
              ɛψ
              0
            
            ⁡
            
              (
              
                
                  η
                  ^
                
                ,
                
                  u
                  2
                
                ,
                y
                ,
                
                  y
                  s
                
              
              )
            
          
        
      
    
    
      
        (
        90
        )
      
    
  




The discrete-time expression of equation (90) similar to equation (88) is given by the following equation (91).




  
    
      
        
          
            
              
                
              
              ⁢
              
                {
                
                  Math
                  .
                  
                    
                  
                  ⁢
                  72
                
                }
              
            
          
          
            
              
            
          
        
      
    
    
      
        
      
    
  
  
    
      
        
          
            
              η
              ^
            
            ⁡
            
              (
              
                k
                +
                1
              
              )
            
          
          -
          
            
              η
              ^
            
            ⁡
            
              (
              k
              )
            
          
        
        =
        
          
            α
            ⁢
            
              
            
            ⁢
            
              K
              1
            
            ⁢
            
              b
              ⁡
              
                (
                
                  
                    
                      η
                      ^
                    
                    ⁡
                    
                      (
                      k
                      )
                    
                  
                  -
                  
                    
                      K
                      1
                    
                    ⁢
                    
                      y
                      ⁡
                      
                        (
                        k
                        )
                      
                    
                  
                
                )
              
            
          
          +
          
            αɛ
            ⁢
            
              
            
            ⁢
            
              K
              1
            
            ⁢
            
              
                χ
                0
              
              ⁡
              
                (
                k
                )
              
            
          
          +
          
            αɛ
            ⁢
            
              
            
            ⁢
            
              K
              1
            
            ⁢
            
              
                cu
                1
              
              ⁡
              
                (
                k
                )
              
            
          
          +
          
            
              αɛ
              2
            
            ⁢
            
              
                ψ
                0
              
              ⁡
              
                (
                k
                )
              
            
          
        
      
    
    
      
        (
        91
        )
      
    
  
  
    
      
        
          
        
        ⁢
        
          
            
              χ
              0
            
            ⁡
            
              (
              k
              )
            
          
          =
          
            
              
                y
                ⁡
                
                  (
                  k
                  )
                
              
              
                
                
                  y
                  ⁡
                  
                    (
                    k
                    )
                  
                
                
              
            
            ⁢
            
              (
              
                
                  h
                  ⁢
                  
                    
                      
                      
                        y
                        ⁡
                        
                          (
                          k
                          )
                        
                      
                      
                    
                    γ
                  
                
                +
                p
              
              )
            
          
        
      
    
    
      
        (
        92
        )
      
    
  
  
    
      
        
          
        
        ⁢
        
          
            
              ψ
              0
            
            ⁡
            
              (
              k
              )
            
          
          =
          
            
              d
              
                e
                -
                
                  
                    y
                    s
                  
                  ⁡
                  
                    (
                    k
                    )
                  
                
              
            
            ⁢
            
              {
              
                
                  y
                  ⁡
                  
                    (
                    k
                    )
                  
                
                +
                
                  
                    
                      qu
                      2
                    
                    ⁡
                    
                      (
                      k
                      )
                    
                  
                  ⁢
                  g
                  ⁢
                  
                    (
                    
                      
                        
                          η
                          ^
                        
                        ⁡
                        
                          (
                          k
                          )
                        
                      
                      ,
                      
                        y
                        ⁡
                        
                          (
                          k
                          )
                        
                      
                    
                    )
                  
                
              
              }
            
          
        
      
    
    
      
        
      
    
  




where {circumflex over (η)}(k): Estimate {circumflex over (η)}(tk) at the discrete-time tk, y(k), u1(k), u2(k), ys(k): y(tk), u1(tk), u2(tk), ys(tk) at the discrete-time tk, χ0(k), ψ0(k): χ0(tk), ψ0(tk) at the discrete-time tk. χ0(k) is given by equation (60) and ψ0(k) is given by equation (58). Equation (91) is rewritten as the following equation (93).

{Math. 73}

{circumflex over (η)}(k+1)=(1+αk1b){circumflex over (η)}(k)−αK12by(k)+αεK1χ0(k)+αεK1cu1(k)+αε2ψ0(k)   (93)

The discrete-time equivalent of equation (80) is given by equation (94).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          74
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            
              x
              ^
            
            3
          
          ⁡
          
            (
            k
            )
          
        
        =
        
          
            1
            ɛ
          
          ⁢
          
            {
            
              
                
                  η
                  ^
                
                ⁡
                
                  (
                  k
                  )
                
              
              -
              
                
                  K
                  1
                
                ⁢
                
                  y
                  ⁡
                  
                    (
                    k
                    )
                  
                
              
            
            }
          
        
      
    
    
      
        (
        94
        )
      
    
  




The high-gain observer 27 obtains screw back pressure estimate {circumflex over (x)}3(k) at the discrete-time tk by executing the arithmetic expressions of equations (88), (93) and (94) at a constant time interval Δt. The high-gain observer 27 by equations (88), (93) and (94) does not estimate the measurable state variable x2(k) (screw velocity) and estimates only necessary state variable x3(k) (screw back pressure) and so is called by a reduced-order high-gain observer.
The results of computer simulation are shown in FIG. 6 when the high-gain observer 27 is used in the plasticizing process of an electric-motor driven injection molding machine. The constants of the mathematical model are as follows.
Maximum stroke of screw backward movement xmax=20.0 cm
Maximum screw backward velocity vmax=2.0 cm/sec
Maximum screw back pressure Pmax32 19.6 MPa
Maximum revolution speed of the servomotor for injection wmax=31.67 rad/sec (302.4 rpm)
The constants a, b, c and d in equations (56) ̃(58) are expressed in equation (95).




  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          75
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            
              
                a
                ⁢
                
                =
                
                  0.1000
                  ⁢
                  
                    
                  
                  ⁢
                  
                    sec
                    
                      -
                      1
                    
                  
                
              
            
          
          
            
              
                b
                ⁢
                
                =
                
                  
                    -
                    4.757
                  
                  ⁢
                  
                    
                  
                  ⁢
                  
                    sec
                    
                      -
                      1
                    
                  
                
              
            
          
          
            
              
                c
                ⁢
                
                =
                
                  24.576
                  ⁢
                  
                    
                  
                  ⁢
                  
                    sec
                    
                      -
                      1
                    
                  
                
              
            
          
          
            
              
                d
                ⁢
                
                =
                
                  9.177
                  ⁢
                  
                    
                  
                  ⁢
                  
                    sec
                    
                      -
                      1
                    
                  
                
              
            
          
        
        }
      
    
    
      
        (
        95
        )
      
    
  




A monotone decreasing characteristics is used for the characteristics of function g({circumflex over (P)}b/Pmax), which decides the plasticizing rate according to the value of {circumflex over (P)}b/Pmax at the maximum screw revolution speed Nmax. The gain constant K of equation (73) used by the high-gain observer 27 is given by equation (96). The data K1=0.01, ε=0.01 and Δt=5 msec are used.
{Math. 76}

K=1.0   (96)

FIG. 5 shows simulation conditions for the screw back pressure control. FIG. 5(a) shows a time sequence of screw revolution speed command N*s=Ns from the screw revolution speed setting device 41. FIG. 5(b) shows a time sequence of screw back pressure command P*b from the screw back pressure setting device 21.
FIG. 6 shows time responses of screw back pressure at the control of screw back pressure. FIG. 6(a) shows the time response of screw back pressure when the control of screw back pressure Pb is carried out by the plasticizing controller shown in FIG. 3 using the pressure detector 12. The time response of actual screw back pressure Pb shown in FIG. 6(a) agrees well with that of screw back pressure command P*b shown in FIG. 5(b).
When the high-gain observer 27 is supposed to be used under the control system shown in FIG. 3 and to calculate the estimate of screw back pressure {circumflex over (P)}b by using the screw velocity signal y(t), the actual motor current signal u1(t) of the servomotor for injection and the screw revolution speed signal u2(t), FIG. 6(b) shows the time response of the estimated screw back pressure {circumflex over (P)}b/Pmax. As the time response of screw back pressure in FIG. 6(a) agrees well with that of estimated screw back pressure {circumflex over (P)}b in FIG. 6(b), it is revealed that the high-gain observer 27 can estimate the screw back pressure exactly with small time-lag.
FIG. 6(c) shows the time response of screw back pressure Pb when the control of screw back pressure is carried out by the plasticizing controller shown in FIG. 1 using the high-gain observer 27. As the time response of screw back pressure Pb shown in FIG. 6(a) using the pressure detector 12 agrees well with that of screw back pressure Pb shown in FIG. 6(c), a good control of screw back pressure can be realized by the high-gain observer 27 without using the pressure detector 12.
INDUSTRIAL APPLICABILITY
In the plasticizing control apparatus and the plasticizing control method of electric-motor driven injection molding machines, the following five disadvantages can be avoided by using the estimated screw back pressure obtained by the high-gain observer as a feedback signal of screw back pressure in place of a pressure detector.
(1) A highly reliable pressure detector is very expensive under high pressure circumstances.
(2) Mounting a pressure detector in the cavity or the barrel nozzle part necessitates the troublesome works and the working cost becomes considerable.
(3) Mounting a load cell in an injection shafting alignment from a servomotor for injection to a screw complicates the mechanical structure and degrades the mechanical stiffness of the structure.
(4) A load cell which uses strain gauges as a detection device necessitates an electric protection against noise for weak analog signals. Moreover the works for zero-point and span adjustings of a signal amplifier are necessary (patent literature PTL 13).
(5) For the improvement of the control accuracy of screw back pressure, the usage of two kinds of pressure detectors with different dynamic ranges brings about the cost increase (patent literature PTL 12).
As the high-gain observer can estimate the screw back pressure exactly with small time-lag, the estimate of screw back pressure obtained by the high-gain observer can be used to monitor the screw back pressure and can be used as a feedback signal in the control system. Thus the high-gain observer of the present invention can be applied to the plasticizing control apparatus and the plasticizing control method of electric-motor driven injection molding machines.










{Reference Signs List }
















1
Metal mold


2
Barrel


3
Servomotor for injection


4
Reduction gear


5
Ball screw


6
Bearing


7
Nut


8
Moving part


9
Screw


10
Reduction gear


11
Servomotor for plasticization


12
Pressure detector


13
Linear slider


14
Rotary encoder


15
Rotary encoder


16
Hopper


17
Cavity


20
Back pressure controller


21
Screw back pressure setting device


22
Subtracter


23
Analog/digital (A/D) converter


24
Pressure controller


25
Digital/analog (D/A) converter


26
Analog/digital (A/D) converter


27
High-gain observer


30
Motor controller (servoamplifier) for injection


31
Analog/digital (A/D) converter


32
PWM (Pulse Width Modulation) device


33
Current transducer of the servomotor for injection


34
Differentiator


40
Screw revolution speed controller


41
Screw revolution speed setting device


50
Motor controller (servoamplifier) for plasticization


51
Subtracter


52
Differentiator


53
Speed controller


54
PWM (Pulse Width Modulation) device


60
Back pressure controller


70
Motor controller (servoamplifier) for injection

## Claims

1. An apparatus for controlling a plasticizing capability in an electric-motor driven injection molding machine having a plasticizing mechanism which consists of a screw injection drive system where rotation of a servomotor for injection is transferred to rotation of a ball screw through a reduction gear and rotation of said ball screw is converted to a linear motion of a nut of said ball screw and a screw is moved back and forth through a moving part drived by a movement of said nut and pressure application to the melted polymer stored at the end of a barrel is realized by the movement of said screw and the pressure applied to the melted polymer is referred to as a screw back pressure and a screw revolution drive system where rotation of a servomotor for plasticization is transferred to rotation of said screw through a reduction gear and resin pellets fed through a hopper are melted by the rotation of said screw and a given amount of melted polymer is stored at the end of said barrel, comprising:
a screw back pressure controller operative to provide a motor current demand signal for said servomotor for injection to external, which comprises
a high-gain observer operative to execute at a constant time interval a discrete-time expression of a time integration derived by applying a standard method of trapezoid rule to a continuous-time time integration equation representing a relational expression between a screw position and a screw backward velocity and operative to execute at a constant time interval discrete-time arithmetic expressions derived by applying a standard method of forward rectangular rule to a continuous-time mathematical model representing motion equations of said plasticizing mechanism and consisting of state equations having two state variables of a screw backward velocity variable and a screw back pressure variable and having three input variables of said motor current demand signal applied to said servomotor for injection or an actual motor current signal, a screw revolution speed signal and a screw position signal and an output equation having one output variable of a screw backward velocity signal as a measurable state variable,
a screw back pressure setting device operative to feed a screw back pressure command signal,
a subtracter operative to feed a difference signal between said screw back pressure command signal from said screw back pressure setting device and an estimate of screw back pressure which said high-gain observer outputs by using a screw backward velocity signal detected by a rotary encoder mounted on said servomotor for injection axis and a differentiator, said motor current demand signal applied to said servomotor for injection or said actual motor current signal and a screw revolution speed signal detected in a motor controller for plasticization as inputs and by executing said discrete-time expression of a time integration and said discrete-time arithmetic expressions built in, and
a pressure controller operative to feed said motor current demand signal for said servomotor for injection by using said difference signal from said subtracter so that said estimate of screw back pressure follows said screw back pressure command signal;

a motor controller for injection fed said motor current demand signal from said screw back pressure controller; and
a motor controller for plasticization controlling a revolution speed of said servomotor for plasticization.

2. A method for controlling a plasticizing capability in an electric-motor driven injection molding machine having a plasticizing mechanism which consists of a screw injection drive system where rotation of a servomotor for injection is transferred to rotation of a ball screw through a reduction gear and rotation of said ball screw is converted to a linear motion of a nut of said ball screw and a screw is moved back and forth through a moving part drived by a movement of said nut and pressure application to the melted polymer stored at the end of a barrel is realized by the movement of said screw and the pressure applied to the melted polymer is referred to as a screw back pressure and a screw revolution drive system where rotation of a servomotor for plasticization is transferred to rotation of said screw through a reduction gear and resin pellets fed through a hopper are melted by the rotation of said screw and a given amount of melted polymer is stored at the end of said barrel, comprising:
deriving an estimate of screw back pressure {circumflex over (x)}3 which a high-gain observer outputs by using the input signals of a screw backward velocity signal detected by a rotary encoder mounted on said servomotor for injection and a differentiator in a motor controller for injection, a motor current demand signal applied to said servomotor for injection or actual motor current signal of said servomotor for injection and a screw revolution speed signal detected by a rotary encoder mounted on said servomotor for plasticization and a motor controller for plasticization and by executing at a constant time interval a discrete-time expression of a time integration represented by the following equation (101) in Math. 79 derived by applying a standard method of trapezoid rule to a continuous-time time integration equation representing a relational expression between a screw position ys and a screw backward velocity y represented by the following equation (100) in Math. 78 and by executing at a constant time interval discrete-time arithmetic expressions represented by the following equation (103) in Math. 80 and the following equation (105) in Math. 81 derived by applying a standard method of forward rectangular rule to a continuous-time mathematical model representing motion equations of said plasticizing mechanism and consisting of a state equation represented by the following equation (97) in Math. 77 having two state variables of a screw backward velocity x2 and a screw back pressure x3 and having three input variables of a motor current demand signal applied to said servomotor for injection or an actual motor current signal u1, a screw revolution speed signal u2 and a screw position ys and an output equation represented by the following equation (98) in Math. 77 having one output variable y of a screw backward velocity x2 as a measurable state variable;





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          77
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          [
          
            
              
                
                  
                    x
                    .
                  
                  2
                
              
            
            
              
                
                  
                    x
                    .
                  
                  3
                
              
            
          
          ]
        
        =
        
          
            
              [
              
                
                  
                    0
                  
                  
                    b
                  
                
                
                  
                    0
                  
                  
                    0
                  
                
              
              ]
            
            ⁡
            
              [
              
                
                  
                    
                      x
                      2
                    
                  
                
                
                  
                    
                      x
                      3
                    
                  
                
              
              ]
            
          
          +
          
            [
            
              
                
                  
                    
                      χ
                      ⁡
                      
                        (
                        
                          x
                          2
                        
                        )
                      
                    
                    +
                    
                      cu
                      1
                    
                  
                
              
              
                
                  
                    ψ
                    ⁡
                    
                      (
                      
                        
                          x
                          2
                        
                        ,
                        
                          x
                          3
                        
                        ,
                        
                          u
                          2
                        
                        ,
                        
                          y
                          s
                        
                      
                      )
                    
                  
                
              
            
            ]
          
        
      
    
    
      
        (
        97
        )
      
    
  
  
    
      
        y
        =
        
          [
          
            
              
                1
              
              
                
                  
                    0
                    ]
                  
                  ⁡
                  
                    [
                    
                      
                        
                          
                            x
                            2
                          
                        
                      
                      
                        
                          
                            x
                            3
                          
                        
                      
                    
                    ]
                  
                
              
            
          
        
      
    
    
      
        (
        98
        )
      
    
  
  
    
      
        
          χ
          ⁡
          
            (
            
              x
              2
            
            )
          
        
        =
        
          
            
              x
              2
            
            
              
              
                x
                2
              
              
            
          
          ⁢
          
            (
            
              
                h
                ⁢
                
                  
                    
                    
                      x
                      2
                    
                    
                  
                  γ
                
              
              +
              p
            
            )
          
        
      
    
    
      
        (
        99
        )
      
    
  
  
    
      
        
          ψ
          ⁡
          
            (
            
              
                x
                2
              
              ,
              
                x
                3
              
              ,
              
                u
                2
              
              ,
              
                y
                s
              
            
            )
          
        
        =
        
          
            d
            
              e
              -
              
                y
                s
              
            
          
          ⁢
          
            {
            
              
                x
                2
              
              +
              
                qf
                ⁡
                
                  (
                  
                    
                      x
                      3
                    
                    ,
                    
                      u
                      2
                    
                  
                  )
                
              
            
            }
          
        
      
    
    
      
        
      
    
  



where x2: State variable of screw backward velocity dimensionless made by maximum screw backward velocity, x3: State variable of screw back pressure dimensionless made by maximum screw back pressure, u1: Input variable of motor current demand or actual motor current of a servomotor for injection dimensionless made by the motor current rating, u2: Input variable of screw revolution speed dimensionless made by maximum screw revolution speed, y: Dimensionless output variable expressing measurable state variable x2, ys: Input variable (dimensionless screw position) decided by an output variable y through the following equation (100) in Math. 78, b, c, d, e, h, p, q, γ: Constants of a mathematical model of a plasticizing mechanism, χ(x2), ψ(x2, x3, u2, ys): Nonlinear functions of equation (99), f(x3, u2): Plasticizing rate function of dimensionless state variable x3 (screw back pressure) and dimensionless input variable u2 (screw revolution speed) dimensionless made by maximum plasticizing rate

{Math. 78}


ys=a∫ydt Initial value ys(t=0)=0   (100)

where a: Constant of a mathematical model of a plasticizing mechanism, t: Time variable

{Math. 79}


ys(k+1)=ys(k)+0.5 aαε{y(k)+y(k+1)}  (101)



αε=Δt   (102)

where k: Discrete variable representing a discrete-time tk(k=0, 1, 2, . . . ), ys(k): Value of input variable ys(tk) at a discrete-time tk, y(k): Value of output variable y(tk) at a discrete-time tk, Δt: Sampling period of a discrete-time high-gain observer, ε: Positive parameter much smaller than 1 used in the high-gain observer

{Math. 80}


{circumflex over (η)}(k+1)=(1+αK1b){circumflex over (η)}(k)−αK12by(k)+αεK1χ(k)+αεK1cu1(k)+αε2ψ(k)   (103)






  
    
      
        
          
            
              
                χ
                ⁡
                
                  (
                  k
                  )
                
              
              =
              
                
                  
                    y
                    ⁡
                    
                      (
                      k
                      )
                    
                  
                  
                    
                    
                      y
                      ⁡
                      
                        (
                        k
                        )
                      
                    
                    
                  
                
                ⁢
                
                  (
                  
                    
                      h
                      ⁢
                      
                        
                          
                          
                            y
                            ⁡
                            
                              (
                              k
                              )
                            
                          
                          
                        
                        γ
                      
                    
                    +
                    p
                  
                  )
                
              
            
          
        
        
          
            
              
                ψ
                ⁡
                
                  (
                  k
                  )
                
              
              =
              
                
                  d
                  
                    e
                    -
                    
                      
                        y
                        s
                      
                      ⁡
                      
                        (
                        k
                        )
                      
                    
                  
                
                ⁢
                
                  {
                  
                    
                      y
                      ⁡
                      
                        (
                        k
                        )
                      
                    
                    +
                    
                      qf
                      ⁢
                      
                        (
                        
                          
                            
                              η
                              ^
                            
                            ⁡
                            
                              (
                              k
                              )
                            
                          
                          ,
                          
                            
                              u
                              2
                            
                            ⁡
                            
                              (
                              k
                              )
                            
                          
                          ,
                          
                            y
                            ⁡
                            
                              (
                              k
                              )
                            
                          
                        
                        )
                      
                    
                  
                  }
                
              
            
          
        
      
    
    
      
        (
        104
        )
      
    
  



where {circumflex over (η)}(k): Estimate {circumflex over (η)}(tk) at a discrete-time tk of new state variable η introduced for estimating state variable x3, u1(k): Value of input variable u1(tk) at a discrete-time tk, u2(k): Value of input variable u2(tk) at a discrete-time tk, χ(k), ψ(k): Values of nonlinear functions χ(tk), ψ(tk) at a discrete-time tk, K1: Parameter which decides a gain constant (K1/ε) of the high-gain observer, K1>0





  
    
      
        {
        
          Math
          .
          
            
          
          ⁢
          81
        
        }
      
    
    
      
        
      
    
  
  
    
      
        
          
            
              x
              ^
            
            3
          
          ⁡
          
            (
            k
            )
          
        
        =
        
          
            1
            ɛ
          
          ⁢
          
            {
            
              
                
                  η
                  ^
                
                ⁡
                
                  (
                  k
                  )
                
              
              -
              
                
                  K
                  1
                
                ⁢
                
                  y
                  ⁡
                  
                    (
                    k
                    )
                  
                
              
            
            }
          
        
      
    
    
      
        (
        105
        )
      
    
  



where {circumflex over (x)}3(k) : Estimate {circumflex over (x)}3(tk) of state variable x3 at a discrete-time tk deriving a difference signal between a screw back pressure command signal from a screw back pressure setting device and said estimate of screw back pressure from said high-gain observer by using a subtracter;
deriving said motor current demand signal by using a pressure controller to which said difference signal is fed from said subtracter so that said estimate of screw back pressure follows said screw back pressure command signal;
generating a motor torque of said servomotor for injection corresponding to said motor current demand signal by said motor controller for injection fed said motor current demand signal so that a screw back pressure equal to said screw back pressure command signal is realized.