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    Cont ro l Syst emContents

    Chapter Topic PageNo

    Chapter-1 IntroductionTheory at a glance

    Previous Years GATE Questions

    Previous Years IES Questions

    Previous Years GATE Answer

    Previous Years IES Answer

    22

    8

    8

    10

    10

    Chapter-2 Transfer Function, Block Diagramsand Signal Flow GraphsTheory at a glance

    Previous Years GATE Questions

    Previous Years IES Questions

    Previous Years GATE Answer

    Previous Years IES Answer

    1212

    19

    21

    24

    25

    Chapter-3 Mathematical Modeling ControlSystemTheory at a glance

    Previous Years IES Questions

    35Previous Years IES Answer

    28

    28

    33

    35

    Chapter-4 Time Response Analysis ofControl SystemTheory at a glance

    Previous Years GATE Questions

    Previous Years IES Questions

    Previous Years GATE Answer

    Previous Years IES Answer

    37

    37

    49

    52

    59

    62

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    IES Academy Contents

    www.iesacademy.com Email: [email protected] Page-1________________________________________________________________________25, 1st Floor, Jia Sarai, Near IIT. New Delhi-16 Ph: 011-26537570, 9810958290

    Chapter-5 Frequency AnalysisTheory at a glance

    Previous Years IES Questions

    Previous Years IES Answer

    6969

    74

    76Chapter-6 Stability Analysis of Control

    SystemTheory at a glance

    Previous Years GATE Questions

    Previous Years IES Questions

    Previous Years GATE Answer

    Previous Years IES Answer

    77

    77

    92

    98

    110

    118

    Chapter-7 Root Locus TechniqueTheory at a glance

    Previous Years GATE Questions

    Previous Years IES QuestionsPrevious Years GATE Answer

    Previous Years IES Answer

    132132

    136

    138143

    146

    Chapter-8 CompensatorsTheory at a glance

    Previous Years GATE Questions

    Previous Years IES Questions

    Previous Years GATE Answer

    Previous Years IES Answer

    150150

    155

    156

    160

    161

    Chapter-9 Industrial ControllersTheory at a glance

    Previous Years GATE QuestionsPrevious Years IES Questions

    Previous Years GATE Answer

    Previous Years IES Answer

    165165

    171172

    176

    177

    Chapter-10 Introduction to State SpaceVariableTheory at a glance

    Previous Years GATE Questions

    Previous Years IES Questions

    Previous Years GATE Answer

    Previous Years IES Answer

    180

    180

    188

    190

    192

    195

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    I n t roduc t i onContents for this chapter

    1. Introduction2. OpenLoop System

    3. Mathematical Model for Open-loop Control System

    4. Closed-Loop Control System

    5. Mathematical Model for Closed-Loop System

    6. Comparison of Open Loop and Closed Loop

    7. Laplace Transform

    8. Basic Laplace Transform Theorem

    9. Summary

    Theory a t a Glanc e(For IES, GATE, PSU & JTO)

    1. IntroductionControl system is a combination of elements arranged in a planned manner. Where each

    element causes an effect to produce a desire output.

    Example of control systems

    1. System for the control of position.

    2. System for the control of velocity.

    2. OpenLoop System1. No feedback in open loop system is used.

    2. Control system (open-loop) depends only on the accuracy of input calibration.

    Example of open-loop control system

    1. Traffic signal light

    2. Electric lift

    3. Automatic washing machine

    3. Mathematical Model for Open-loop Control System

    C= G

    R

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    Where, G = gain of system

    C = o/p of system

    R = input

    Points:

    1. Feedback system is not used for improving stability.2. An open-loop system may become unstable when we used negative feedback.

    4. Closed-Loop Control SystemIn a closed loop control system the output has an effect on control action through a feedback.

    Example of closed-loop system:1. D.C. Motor speed control

    2. Radar tracking system

    3. Auto pilot system

    5. Mathematical Model for Closed-Loop System

    C G=

    R 1+GH

    1* Here feedback is negative

    2. This form is also called control canonical form

    From figure

    C(S)= G(S) =

    E(S)As a Forward path transfer function

    B(S)=H(S)=

    C(S)As a feedback transfer function

    The o/p of summing point

    [ ]E(S) R(S) B(S)= ;

    C(S)= R(S) B(S)G(S) ;

    C(S)= R(S) C(S) H(S)

    G(S);

    C(S) = R(S) G(S) G(S) C(S) H(S) ;

    [ ]C(S) 1+G(S) H(S) = R(S) G(S)

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    C(S) G(S)=

    R(S) 1+G(S) H(S)

    6. Comparison of Open Loop and Closed LoopOpen Loop System Closed Loop System

    1. The accuracy of an open loop system

    depends on the calibration of the i/p.

    1. As the error between the reference input

    and the output is continuously measured-

    through feedback.

    2. The open loop system is more stable. 2. The closed loop system is less stable.

    3. It is less accurate. 3. It is more accurate.

    4. It is cheap and less complex. 4. It is expensive and more complex circuit.

    5. Effect of Noise and disturbance is morein open loop control system. 5. Effect of Noise and disturbance is less inclosed loop control system.

    7. Laplace TransformLaplace transformation is very great tool in control system.

    The mathematical expression for laplace transforms

    st

    0

    F(t) F(S)

    F(S) F(t) e dt

    =

    =

    L

    The term laplace transform of F(t) is used for the letter LF(t).

    8. Basic Laplace Transform TheoremBasic theorems of laplace transform are given below

    Theorem 1: Multiplication by a constantLet k be a constant and F(S) be the laplace transform of F(t), then

    [ ]Kf(t) KF(S)= Theorem 2: Sum and difference

    Let F1(S) and F2(S) be the laplace transform of ( ) ( )1 2f t f t , then

    ( ) ( )1 2 1 2f t f t = F (S) F (S)

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    Theorem 3: Differentiation

    [ ]

    22 1

    2

    dF(t)i. = SF(S) -F(0)

    dt

    d F(t)ii. = S F(S) - F(0) -f (0)

    dt

    L

    L

    1 dF(0)where, F (0) =dt

    In general, for higher order derivatives or F(t)

    1 2 (1) ( 1)( ) ( ) ( ) (0) (0)

    =

    nn n n n

    n

    d F ts F S s f O s f f

    dtL

    Where, F1(0) denotes the ith order derivative of f(t) with respect to t1,

    Theorem 4: Integration

    1

    1 2

    2 2

    F(S) F (0)i. F(t) = +

    S S

    F(S) F (0) F (0)ii. F(t) = + +

    S S S

    L

    L

    Theorem 5: Shift in time

    The laplace transform of F(t) delayed by time T is equal to the laplace transform F(t)multiplied by eST that is

    [ ] -STsF(t T) u (t T) = e F(S)L Where US(tT) denotes the unit step function that is shifted in time to the right by T.

    Theorem 6: Complex shifting

    The laplace transform of F(t) multiplied byte , where is a constant is equal to the laplace

    transform F(S), with S replaced by ( )S that is

    t

    e F(t) = F(S

    )

    L

    Theorem 7: Initial-value theoremIf the laplace transform of F(t) is F(S), then

    0lim ( ) lim ( )

    =

    t SF t SF S

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    Theorem 8: Final value theorem

    0

    0

    lim ( ) lim ( )

    lim ( ) lim ( )

    t S

    t S

    F t S F t

    F t SF S

    =

    =

    L

    Point to be RememberIf the denominator of SF(S) has any root having real part as zero or positive, then final value

    theorem is not valid. [GATE 2007]

    USEFUL TRANSFORM (LAPLACE) PAIR

    1 F(t) F(S) = LF(t)2 (t) unit impulse 1

    3 U(t)1

    S

    4 U(tT)1 st

    eS

    5 t2

    1

    S

    6

    2

    2

    t 3

    1

    S

    7n

    t 1nn

    s +

    8 ate

    1

    s a+

    9 ate 1

    s a

    10 atte ( )

    2

    1

    s a+

    11 atte ( )2

    1

    s a

    12

    13 h tt e ( )1

    /+

    +n

    n s a

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    14 sin t2 2

    +s

    15 cos t

    e t

    ( )2 2

    +

    + +

    s

    s

    16 sin t

    e t( )

    2 2

    + +s

    17 sin h t2 2

    s

    18 cos h t2 2

    s

    s

    9. Summary1. Open loop control system no feedback used.

    2. In closed loop control system we used feedback.

    3. Open loop system is more stable.

    4. Closed loop system is more accurate.

    5. Final value theorem can not used if denominators of SF(S) have real part as a zero or

    positive.

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    ASKED OBJECTIVE QUESTIONS (GATE, IES)

    Previous Years GATE Quest ions

    Basic Laplace Transform Theorem

    GATE-1. If the Laplace Transform of a signal y(t) is1

    ( ) ,( 1)

    =

    Y ss s

    then its final

    value is: [GATE-2007]

    (a) -1 (b) 0 (c) 0 (d) Unbounded

    GATE-2. The unit impulse response of a system is ( ) , 0= t f t e t [GATE-2006]

    For this system, the steady-state value of the output for unit step inputis equal to

    (a) -1 (b) 0 (c) 1 (d)

    Previous Years IES Quest ions

    Closed-Loop Control SystemIES-1. When a human being tries to approach an object, his brain acts as

    (a) An error measuring device (b) A controller [IES-1999]

    (c) An actuator (d) An amplifier

    IES-2. Assertion (A): Feedback control systems offer more accurate control

    over open-loop systems. [IES-2000]

    Reason (R): The feedback path establishes a link for input and output

    comparison and subsequent error correction.

    (a) Both A and R are true and R is the correct explanation of A

    (b) Both A and R are true but R is NOT the correct explanation of A

    (c) A is true but R is false

    (d) A is false but R is true

    IES-3. Consider the following statements: [IES-2000]

    1. The effect of feedback is to reduce the system error

    2. Feedback increases the gain of the system in one frequency rangebut decreases in another

    3. Feedback can cause a system that is originally stable to become

    unstable

    Which of these statements are correct?

    (a) 1, 2 and 3 (b) 1 and 2 (c) 2 and 3 (d) 1 and 3

    IES-4. Consider the following statements which respect to feedback control

    systems: [IES-2006]

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    1. Accuracy cannot be obtained by adjusting loop gain.

    2. Feedback decreases overall gain.

    3. Introduction of noise due to sensor reduces overall accuracy.

    4. Introduction of feedback may lead to the possibility of instability of

    closed loop system.

    Which of the statements given above are correct?(a) 1, 2, 3 and 4 (b) Only 1, 2 and 4

    (c) Only 1 and 3 (d) Only 2, 3 and 4

    IES-5. A negative-feedback closed-loop system is supplied to an input of 5V.

    The system has a forward gain of 1 and a feedback gain of a 1. What is

    the output voltage? [IES-2009]

    (a) 1.0 V (b) 1.5 V (c) 2.0 V (d) 2.5 V

    Basic Laplace Transform Theorem

    IES-6. Consider the function F(s) =2 2s

    +where F(s) is the Laplace transform

    of f(t). What is the steady-state value of f(t) ? [IES-2009](a) Zero (b) One (c) Two (d) A value between -1 and +1

    IES-7. The transfer function of a linear-time-invariant system is given as

    ( )1

    s 1+. What is the steady-state value of the unit-impulse response?

    [IES-2009]

    (a) Zero (b) One (c) Two (d) Infinite

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    Answ ers w i th Ex p lanat ion

    (Object ive)

    Previous Years GATE Answ er

    GATE-1. Ans. (d)1

    ( )( 1)

    Final value of Y(s)

    1 1 1-1 -1 -1LT ( ( )) LT = LT( 1) 1

    ( ) ( )

    value =

    t

    =+

    = + +

    =

    Y sS S

    Y sS S S S

    tY t e u t

    final

    GATE-2. Ans. (c) Unit impulse response of a system is

    ( ) t 0= t f t e

    1( )

    1=

    +f s

    S

    O/P for unit step I/P1 1

    1=

    +S S

    1

    ( 1)=

    +S S

    1( ( )) lim = 1

    ( 1)0t

    C s SS Ss

    = =

    +

    Previous Years IES Answ er

    IES-1.Ans. (b)

    IES-2. Ans. (a)

    IES-3. Ans. (d) Feedback is applied to reduce

    the system error. Consider the

    example.

    ( )( )

    ( )( ) ( )

    C s G s

    R s 1 G s H s

    1 1s 11 s 1

    1s 1

    =

    += =

    +

    Thus, we see that the closed loop system is unstable while the open loop system is

    stable.

    IES-4. Ans. (d)

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    IES-5. Ans. (d) Output voltage = inA

    V1 AB+

    ( )1

    5x 2.5V1 1x1x

    = =+

    IES-6. Ans. (d) This is the Laplace transform of sin t.

    So, f(t) = sin t

    Steady-state value of f(t) is undetermined because poles of F(s) are not in LHS ofs-plane. Therefore, steady-state value will vary between - 1 and + 1.

    IES-7. Ans. (a) Steady state value =( )s 0

    1lims 1

    s 1 += 0