Topic #58 Lead Compensators Reference textbook : Control Systems, - - PowerPoint PPT Presentation

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Topic #58 Lead Compensators Reference textbook : Control Systems, - - PowerPoint PPT Presentation

ME 779 Control Systems Topic #58 Lead Compensators Reference textbook : Control Systems, Dhanesh N. Manik, Cengage Publishing, 2012 1 Lead Compensators Magnitude and phase Bode plot of a lead compensator ( ) s z 1 G s ( )


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SLIDE 1

1

ME 779 Control Systems

Lead Compensators

Topic #58

Reference textbook:

Control Systems, Dhanesh N. Manik, Cengage Publishing, 2012

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SLIDE 2

2

Magnitude and phase Bode plot of a lead compensator

1 1

( ) ( ) ( )

c

s z G s s p   

1 1 1 1 1 1

tan tan , p z z p   

 

              

Lead Compensators

1 1

(j ) (j ) (j )

c

z G p      

High pass filter Comparable to a PD controller

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SLIDE 3

3

Electrical lead compensator

1 1 1 1

1 R Z jR C   

1 2 1 1 1 2 1 2 1 1 1

1 1

eq

R Z R jR C jR R C R R jR C          

in eq

E i Z 

Lead Compensators

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SLIDE 4

4

Electrical lead compensator

 

2 1 1 2 1 2 1 1 2

1

in

  • E R

jR C E iR jR R C R R       

1 1 1 2 1 2 1 2

R C R R R      

2 1 1 2

1 1

  • i

E j E j                  

1 1 1 2

tan ( ) tan ( )     

 

 

1 2

  

Lead Compensators

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5

Mechanical lead compensator

1 1 1 1 1 1 1 1 2

( ) ( ) ( ) ( ) c c k k x t x t c c k k k y t y t                               

1 1 1 1 1 1 1 2 1

( ) ( ) k c s k c s X s k c s k k c s Y s                    

Lead Compensators

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SLIDE 6

6

X(s)=Y(s): rigid body motion

1 1 1 2 1

( ) ( ) k c s Y s X s k k c s    

Mechanical lead compensator 1 1 1 1 1 2 1 2

c k k k k      

2 1 1 2 1 2

1 ( ) , ( ) 1 s Y s X s s                   

Lead Compensators

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SLIDE 7

7

2 1 1 2 1 2

1 ( ) , ( ) 1 j Y X j                       

Mechanical lead compensator

Lead Compensators

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SLIDE 8

8

Frequency response

2 1

1

  • in

E E    

Low frequencies

1

  • in

E E 

High frequencies

Between lower and higher frequencies, the following variations take

  • place. Up to a frequency given by

1

1  , the magnitude of the lead

compensator transfer function in decibels is given by

2 1

20log  , which is

  • negative. Then it keeps on increasing till a frequency

2

1 

, and then becomes zero decibels.

Lead Compensators

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9

Assume τ1=10 and τ2=1, for a lead compensator and plot magnitude and phase of the transfer function Determine the frequency at which the phase angle becomes a maximum and the value

  • f maximum phase angle.

Lead Compensators

Example

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SLIDE 10

10

Frequency response

Magnitude of the transfer function of a lead compensator

1 2

10 , 1 s s    

2 1

1 20log 20log 20 10 dB                 

Lead Compensators

Example

 

20log 1 0dB 

2 1

1 10log 10log 10 10 dB                 

maximum Minimum

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11

Phase angle of the transfer function of a lead compensator

Lead Compensators

Example

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12

Compare a lead compensator with a PD

  • controller. Use the following values: τ1=10

and τ2=1 for the lead compensator and Kp=1 and Td=1 for the PD controller.

( ) (1 )

PD p d

G s K T s  

Lead Compensators

Example

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SLIDE 13

13

Lead Compensators

Example

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SLIDE 14

14

Maximum phase angle

   

1 2 2 2 1 2

1 1 d d            

1 1 1 2

tan ( ) tan ( )     

 

 

2 1 2

1

m

   

1 1 1 2 1 2 1 2 1 1 1 2 2 1

1 1 tan tan tan tan

m

          

   

                                   

1 1 1 1 2 1 1 2 2 1

tan tan 1 tan tan        

   

                   

Lead Compensators

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SLIDE 15

15

Maximum phase angle

1 2 m

    

1 2 1 2

sin sin cos cos sin

m

      

1 2 2 2 1 2

1 1 sin 1 1

m

            

1 2

1 sin 1 sin

m m

      

Lead Compensators

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16

Lead compensator design (phase margin)

  • 1. Determine the phase margin φu of the uncompensated feedback transfer

function, whose phase margin has to be increased.

  • 2. Decide on the expected value of the compensated system φe that is

application dependent and give an additional margin of 5o.

  • 3. Based on the first two steps, select a maximum value of phase angle φm

that has to be introduced by the lead compensator:

5

m e u

     

  • 4. Using the φm from step 3, determine the ratio of time constants

Lead Compensators

1 2

1 sin 1 sin

m m

      

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17

5.

The magnitude of the lead compensator varies from

2 1

20log 

to 0 between

1

1  and

2

1  rad/s. Therefore, using the ratio

  • f time constants from step 4, determine the frequency at

which the decibel gain of the uncompensated system is

1 2

10log   and use this as ωm. This will be the frequency

at which the compensated system crosses the unit circle. Since this is also the frequency at which maximum phase angle of the lead compensator is obtained, it will result in maximum increase in phase angle.

Lead Compensators

Lead compensator design (phase margin)

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18

6. Using equation

2 1 2

1

m

   

, determine the actual values

  • f time constants and then design other the elements
  • f the lead compensator

Lead Compensators

Lead compensator design (phase margin)

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The open-loop transfer function of a unity feedback system is given by

100 ( ) ( 2)( 4) G s s s s   

(a) Draw a Bode plot of the above open-loop transfer function and determine the phase margin (b) Use a lead compensator and change the phase margin of the compensated system to 25o (c) Draw root-locus plots of the uncompensated and compensated systems (d) Determine the bandwidth for compensated and uncompensated systems

Lead Compensators

Example

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SLIDE 20

20

 

2 2

100 ( ) ( 2)( 4) 100 ( ) ( 2)( 4) 100 6 8 G s s s s G j j j j j                 

Lead Compensators

6 4 2

100 ( ) 20 60 G j      

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Bode plot for the compensated and uncompensated

  • pen-loop transfer function of equation

The uncompensated system is unstable

Lead Compensators

Example

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Phase margin of the uncompensated system, φu can be obtained as -18o Since the gain margin is negative, the given uncompensated system is unstable 1 2

1 sin 1 sin 48 6.79 1 sin 1 sin 48

m m

          

Lead Compensators

Example

Since the expected value of gain margin for the compensated system is 25o, the maximum phase angle φm of the lead compensator is 25+5-(-18)=480.

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23

1 2

10log 10log6.79 8.3dB    

6 4 2

100 20log 20 64               

6 4 2

100 20log 8.3 20 64

m m m

               

ωm =2.52 rad/s

Lead Compensators

Example

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2 2 2 1 2 1

1 1 0.15 2.52 6.79 0.15 6.79 1.03

m

s s            

Lead Compensators

Example

2 1 2

1

m

   

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25

2 1 1 2

1 100 ( ) ( ) 1 ( 2)( 4) 100 (1 0.15 ) 6.79 ( 2)( 4)(1 1.03 )

c

s G s G s s s s s s s s s s                             

( ) ( 2)( 4) K G s s s s   

1 2

1 ( ) ( ) 1 ( 2)( 4)

c

K s G s G s s s s s                   

Lead Compensators

Example

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Root-locus plot of the uncompensated unity feedback system

Lead Compensators

Example

( ) ( 2)( 4) K G s s s s   

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Root-locus of the system compensated by a lead compensator

Lead Compensators

Example

1 2

1 ( ) ( ) 1 ( 2)( 4)

c

K s G s G s s s s s                   

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( 2)( 4) ( ) ( 2)( 4) 1 ( 2)( 4) K K s s s T s K s s s K s s s          

1 2 1 1 2 1 2

1 1 1 ( 2)( 4) ( ) 1 1 1 ( 2)( 4) 1 1 ( 2)( 4)

c

K s s s s s K s T s K s s s s s K s s s s s                                                                  

uncompensated Compensated

Lead Compensators

Example

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29

Closed-loop frequency response of uncompensated and lead compensated systems

Lead Compensators

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30

The open-loop transfer function of a unity feedback system is given by

( ) ( 2)( 4) K G s s s s   

Design a lead compensator so the dominant closed-loop response has a damping ratio of 0.47 with an undamped natural frequency of 1.7 rad/s. Assume that these values could not have been obtained just by changing the open-loop gain K. That means the closed-loop poles having the above damping ratio and undamped natural frequency are not on the root locus of the above system

(1)

Lead Compensators

Example

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SLIDE 31

31 2 1,2

0.47 1.7 1 0.47 0.8 1.5 s j        

Expected close-loop poles

( 2.5) ( ) ( 2)( )( 4)

c

K s G s s s s p s     

Compensated system

Lead Compensators

Example

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32

Open-loop poles and zeros of the compensated system and the desired closed-loop poles

Lead Compensators

Example

Available space for compensator

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33

41 (118 51 25 ) 180

c

      

27

c

 

1.5 0.8 3.75 tan 27

c

p   

( 2.5) ( ) ( 2)( 3.75)( 4) K s G s s s s s     

0.8 1.5 0.8 1.5 2 0.8 1.5 3.75 0.8 1.5 4 17 0.8 1.5 2.5 j j j j K j                

Lead Compensators

Example

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34

Root locus of the compensated system to obtain the desired closed-loop poles

Lead Compensators

Example

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SLIDE 35

Lead Compensators

Conclusion

35