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                     Time Response
•   How to find the time response from the transfer function

•   How to use poles and zeros to determine the response of a control
    system

•   How to describe quantitatively the transient response of first- and
    second order systems

•   How to approximate higher-order systems as first or second order

•   How to find the time response from the state-space representation




                                                        Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                          Copyright © 2004 by John Wiley & Sons. All rights reserved.
2

          Poles, Zeros, and System Response

•   The output response of a system is the sum of two responses:
    the forced response and the natural response.


•   The poles of a transfer function are the values of the Laplace
    transform variable, s, that cause the transfer function to become
    infinite.

•   The zeros of a transfer function are the values of the Laplace
    transform variable, s, that cause the transfer function to become
    zero.




                                                       Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                         Copyright © 2004 by John Wiley & Sons. All rights reserved.
3


Poles and Zeros of a First-Order System (1)

                        Unit step response is given by:




                                       Control Systems Engineering, Fourth Edition by Norman S. Nise
                                         Copyright © 2004 by John Wiley & Sons. All rights reserved.
4


Poles and Zeros of a First-Order System (2)




                                 Control Systems Engineering, Fourth Edition by Norman S. Nise
                                   Copyright © 2004 by John Wiley & Sons. All rights reserved.
5


Example: Given the system below, specify the natural and forced
parts of the output c(t)




                                                    Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                      Copyright © 2004 by John Wiley & Sons. All rights reserved.
6
                 First-Order Systems




Step response:




                                       Control Systems Engineering, Fourth Edition by Norman S. Nise
                                         Copyright © 2004 by John Wiley & Sons. All rights reserved.
7

                       First-Order Systems

Time constant of the system: 1/a, it is
time it takes for the step response to rise
to 63% of its final value

Rise time, Tr : time for the waveform
to go from 0.1 to 0.9 of its final value




 Settling time, Ts : time for the response
 to reach, and stay within, 2% of its
 final value



                                              Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                Copyright © 2004 by John Wiley & Sons. All rights reserved.
8

First-Order Transfer Functions via Testing

With a step input, we can measure the time constant and the steady-state value,
from which the transfer function can be calculated.

 Let first order system is

 and the step response is



                                       1.   Final value = 0.72
                                       2.   63 % of final value = 0.63*0.72=0.45
                                       3.   Curve reaches 0.45 at 0.13 s, hence
                                            a = 1/0.13 = 7.7
                                       4.   Steady state value K/a = 0.72, hence
                                            K = 5.54

                                                       5.54
                                             G(s) =
                                                      s + 7.7

                                                                Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                                  Copyright © 2004 by John Wiley & Sons. All rights reserved.
9
    Second-Order Systems: Introduction
•   a second-order system exhibits a wide range of responses




                                                       Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                         Copyright © 2004 by John Wiley & Sons. All rights reserved.
10


Second-Order Systems: Introduction




                            Control Systems Engineering, Fourth Edition by Norman S. Nise
                              Copyright © 2004 by John Wiley & Sons. All rights reserved.
11

        Summary of Second-Order Systems (1)
There are four possible responses:
                  1. Overdamped responses
                  2. Underdamped responses
                  3. Undamped response
                  4. Critically damped responses




                                                   Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                     Copyright © 2004 by John Wiley & Sons. All rights reserved.
12

Summary of Second-Order Systems (2)




                           Control Systems Engineering, Fourth Edition by Norman S. Nise
                             Copyright © 2004 by John Wiley & Sons. All rights reserved.
13

Summary of Second-Order Systems (3)




                   ωd … damped frequency of oscillation




                                   Control Systems Engineering, Fourth Edition by Norman S. Nise
                                     Copyright © 2004 by John Wiley & Sons. All rights reserved.
14

Summary of Second-Order Systems (4)




                           Control Systems Engineering, Fourth Edition by Norman S. Nise
                             Copyright © 2004 by John Wiley & Sons. All rights reserved.
15

Summary of Second-Order Systems (5)




                           Control Systems Engineering, Fourth Edition by Norman S. Nise
                             Copyright © 2004 by John Wiley & Sons. All rights reserved.
16

            The General Second-Order System (1)
Natural Frequency, ωn
- the frequency of oscillation of the system without damping.


Damping Ratio, ζ




Derivation of the second order system in terms of ωn and ζ

 Consider

  Let us determine what is the term a and the term b in terms of ωn and ζ .




                                                            Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                              Copyright © 2004 by John Wiley & Sons. All rights reserved.
17




Without damping (a=0) the poles are on the imaginary axis and



                                                    Then




                                                         Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                           Copyright © 2004 by John Wiley & Sons. All rights reserved.
18


Now, let us assume an underdamped system. The real part of the complex
pole is σ = - a/2 and it determines the exponential decay frequency.


  Hence



  Then, the general second-order transfer function is




 and the poles of this transfer function are:



                            s1, 2 = −ζω n ± jωn 1 − ζ 2

                                                          Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                            Copyright © 2004 by John Wiley & Sons. All rights reserved.
19




Control Systems Engineering, Fourth Edition by Norman S. Nise
  Copyright © 2004 by John Wiley & Sons. All rights reserved.
20

      Underdamped Second-Order Systems (1)
- represent a common model for physical problems


 Step response:


 Expanding by partial fraction we obtain:




 Then in time domain:




                                                   Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                     Copyright © 2004 by John Wiley & Sons. All rights reserved.
21

Underdamped Second-Order Systems (2)




                           Control Systems Engineering, Fourth Edition by Norman S. Nise
                             Copyright © 2004 by John Wiley & Sons. All rights reserved.
22
        Underdamped Second-Order Systems (3)
Specifications:




                                   Control Systems Engineering, Fourth Edition by Norman S. Nise
                                     Copyright © 2004 by John Wiley & Sons. All rights reserved.
23

          Underdamped Second-Order Systems (4)
Evaluation of Tp,
Tp is found by differentiating c(t) and
finding the first zero crossing after t = 0.
                      π
       Tp =
              ωn 1 − ζ 2


 Evaluation of % OS



           − (ζπ / 1−ζ 2 )
 %OS = e                     × 100

        − ln(%OS / 100)
 ζ =
       π 2 + ln 2 (%OS / 100)




                                               Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                 Copyright © 2004 by John Wiley & Sons. All rights reserved.
24

              Underdamped Second-Order Systems (5)

Evaluation of Ts




               4
       Ts =
              ζω n

Evaluation of Tr
- cannot be found
analytically




                                         Control Systems Engineering, Fourth Edition by Norman S. Nise
                                           Copyright © 2004 by John Wiley & Sons. All rights reserved.
25

         Underdamped Second-Order Systems (6)

 - now we will evaluate peak time, settling
 time and overshoot in terms of the pole
 location


From the Pythagorean theorem:




     ωd … damped frequency of oscillation
     σd … exponential damping frequency


                                              Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                Copyright © 2004 by John Wiley & Sons. All rights reserved.
26

       Underdamped Second-Order Systems (7)




%OS = e −(ζπ /   1−ζ 2 )
                           × 100




                                   Control Systems Engineering, Fourth Edition by Norman S. Nise
                                     Copyright © 2004 by John Wiley & Sons. All rights reserved.
27

Underdamped Second-Order Systems (8)




                          Control Systems Engineering, Fourth Edition by Norman S. Nise
                            Copyright © 2004 by John Wiley & Sons. All rights reserved.
28

Problem: Given the plot, find ζ, ωn, Tp, %OS and Ts



                                        Solution:




                                            ωn = 7 2 + 32 = 7.62




                                                            Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                              Copyright © 2004 by John Wiley & Sons. All rights reserved.
29


    System Response with Additional Poles (1)


•    If a system such has more than two poles or has zeros, we
     cannot use the previously derived formulae to calculate the
     performance specifications


•    However, under certain conditions, a system with more than
     two poles or with zeros can be approximated as a second-
     order system that has just two complex dominant poles




                                                     Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                       Copyright © 2004 by John Wiley & Sons. All rights reserved.
30


     System Response with Additional Poles (2)
- Let us consider a system with complex poles and a real pole



                s3 = −α r


- Then the step response can be found using partial fraction expansion




                                                            Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                              Copyright © 2004 by John Wiley & Sons. All rights reserved.
31
        System Response with Additional Poles (3)




•   We can assume that the exponential decay is negligible after five time constants.

                                                              Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                                Copyright © 2004 by John Wiley & Sons. All rights reserved.
32

           System Response with Zeros (1)




    If a >> b, c :

•   zero looks like a simple gain factor and does not change the relative amplitudes of
    the components of the response.




                                                               Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                                 Copyright © 2004 by John Wiley & Sons. All rights reserved.
33

             System Response with Zeros (2)
Different approach to investigate the effect of a zero:

•   Let C(s) be the response of a system, T(s), with unity in the numerator

•   If we add a zero to the transfer function, yielding (s + a)T(s), the Laplace
    transform of the response will be


               If a is very large and positive, then the response is approximately a
               scaled version of the original response

               If a is small and positive, then the derivative term has a greater
               effect on the response – more overshoot




                                                                Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                                  Copyright © 2004 by John Wiley & Sons. All rights reserved.
34

     System Response with Zeros (3)


        If a is negative (in the right haf-plane), then the derivative term will
        be of opposite sign from the scaled response term




If the response begins to turn towards the negative direction even though the
final value is positive then the system is known as nonminimum-phase
system - (zero is in the right half-plan).


                                                         Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                           Copyright © 2004 by John Wiley & Sons. All rights reserved.
35


                Pole-zero cancellation


    Consider:



•     If the zero at –z is very close to the pole at –p3 then it can be shown
      using partial fraction expansion of T(s) that the residue of the pole at –
      p3 is much smaller than any of the other residues




                                                                Control Systems Engineering, Fourth Edition by Norman S. Nise
                                                                  Copyright © 2004 by John Wiley & Sons. All rights reserved.
36

Laplace Transform Solution of State Equations



Taking the Laplace transform of




  After taking the Laplace transform of



                            y(t)=L-1{Y(s)}

                                             Control Systems Engineering, Fourth Edition by Norman S. Nise
                                               Copyright © 2004 by John Wiley & Sons. All rights reserved.
37

Laplace Transform Solution of State Equations

Eigenvalues and Transfer Function Poles




If x(0) = 0 :




 Hence, we can find poles from



                                          Control Systems Engineering, Fourth Edition by Norman S. Nise
                                            Copyright © 2004 by John Wiley & Sons. All rights reserved.

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  • 1. 1 Time Response • How to find the time response from the transfer function • How to use poles and zeros to determine the response of a control system • How to describe quantitatively the transient response of first- and second order systems • How to approximate higher-order systems as first or second order • How to find the time response from the state-space representation Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 2. 2 Poles, Zeros, and System Response • The output response of a system is the sum of two responses: the forced response and the natural response. • The poles of a transfer function are the values of the Laplace transform variable, s, that cause the transfer function to become infinite. • The zeros of a transfer function are the values of the Laplace transform variable, s, that cause the transfer function to become zero. Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 3. 3 Poles and Zeros of a First-Order System (1) Unit step response is given by: Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 4. 4 Poles and Zeros of a First-Order System (2) Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 5. 5 Example: Given the system below, specify the natural and forced parts of the output c(t) Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 6. 6 First-Order Systems Step response: Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 7. 7 First-Order Systems Time constant of the system: 1/a, it is time it takes for the step response to rise to 63% of its final value Rise time, Tr : time for the waveform to go from 0.1 to 0.9 of its final value Settling time, Ts : time for the response to reach, and stay within, 2% of its final value Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 8. 8 First-Order Transfer Functions via Testing With a step input, we can measure the time constant and the steady-state value, from which the transfer function can be calculated. Let first order system is and the step response is 1. Final value = 0.72 2. 63 % of final value = 0.63*0.72=0.45 3. Curve reaches 0.45 at 0.13 s, hence a = 1/0.13 = 7.7 4. Steady state value K/a = 0.72, hence K = 5.54 5.54 G(s) = s + 7.7 Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 9. 9 Second-Order Systems: Introduction • a second-order system exhibits a wide range of responses Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 10. 10 Second-Order Systems: Introduction Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 11. 11 Summary of Second-Order Systems (1) There are four possible responses: 1. Overdamped responses 2. Underdamped responses 3. Undamped response 4. Critically damped responses Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 12. 12 Summary of Second-Order Systems (2) Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 13. 13 Summary of Second-Order Systems (3) ωd … damped frequency of oscillation Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 14. 14 Summary of Second-Order Systems (4) Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 15. 15 Summary of Second-Order Systems (5) Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 16. 16 The General Second-Order System (1) Natural Frequency, ωn - the frequency of oscillation of the system without damping. Damping Ratio, ζ Derivation of the second order system in terms of ωn and ζ Consider Let us determine what is the term a and the term b in terms of ωn and ζ . Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 17. 17 Without damping (a=0) the poles are on the imaginary axis and Then Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 18. 18 Now, let us assume an underdamped system. The real part of the complex pole is σ = - a/2 and it determines the exponential decay frequency. Hence Then, the general second-order transfer function is and the poles of this transfer function are: s1, 2 = −ζω n ± jωn 1 − ζ 2 Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 19. 19 Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 20. 20 Underdamped Second-Order Systems (1) - represent a common model for physical problems Step response: Expanding by partial fraction we obtain: Then in time domain: Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 21. 21 Underdamped Second-Order Systems (2) Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 22. 22 Underdamped Second-Order Systems (3) Specifications: Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 23. 23 Underdamped Second-Order Systems (4) Evaluation of Tp, Tp is found by differentiating c(t) and finding the first zero crossing after t = 0. π Tp = ωn 1 − ζ 2 Evaluation of % OS − (ζπ / 1−ζ 2 ) %OS = e × 100 − ln(%OS / 100) ζ = π 2 + ln 2 (%OS / 100) Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 24. 24 Underdamped Second-Order Systems (5) Evaluation of Ts 4 Ts = ζω n Evaluation of Tr - cannot be found analytically Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 25. 25 Underdamped Second-Order Systems (6) - now we will evaluate peak time, settling time and overshoot in terms of the pole location From the Pythagorean theorem: ωd … damped frequency of oscillation σd … exponential damping frequency Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 26. 26 Underdamped Second-Order Systems (7) %OS = e −(ζπ / 1−ζ 2 ) × 100 Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 27. 27 Underdamped Second-Order Systems (8) Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 28. 28 Problem: Given the plot, find ζ, ωn, Tp, %OS and Ts Solution: ωn = 7 2 + 32 = 7.62 Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 29. 29 System Response with Additional Poles (1) • If a system such has more than two poles or has zeros, we cannot use the previously derived formulae to calculate the performance specifications • However, under certain conditions, a system with more than two poles or with zeros can be approximated as a second- order system that has just two complex dominant poles Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 30. 30 System Response with Additional Poles (2) - Let us consider a system with complex poles and a real pole s3 = −α r - Then the step response can be found using partial fraction expansion Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 31. 31 System Response with Additional Poles (3) • We can assume that the exponential decay is negligible after five time constants. Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 32. 32 System Response with Zeros (1) If a >> b, c : • zero looks like a simple gain factor and does not change the relative amplitudes of the components of the response. Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 33. 33 System Response with Zeros (2) Different approach to investigate the effect of a zero: • Let C(s) be the response of a system, T(s), with unity in the numerator • If we add a zero to the transfer function, yielding (s + a)T(s), the Laplace transform of the response will be If a is very large and positive, then the response is approximately a scaled version of the original response If a is small and positive, then the derivative term has a greater effect on the response – more overshoot Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 34. 34 System Response with Zeros (3) If a is negative (in the right haf-plane), then the derivative term will be of opposite sign from the scaled response term If the response begins to turn towards the negative direction even though the final value is positive then the system is known as nonminimum-phase system - (zero is in the right half-plan). Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 35. 35 Pole-zero cancellation Consider: • If the zero at –z is very close to the pole at –p3 then it can be shown using partial fraction expansion of T(s) that the residue of the pole at – p3 is much smaller than any of the other residues Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 36. 36 Laplace Transform Solution of State Equations Taking the Laplace transform of After taking the Laplace transform of y(t)=L-1{Y(s)} Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.
  • 37. 37 Laplace Transform Solution of State Equations Eigenvalues and Transfer Function Poles If x(0) = 0 : Hence, we can find poles from Control Systems Engineering, Fourth Edition by Norman S. Nise Copyright © 2004 by John Wiley & Sons. All rights reserved.