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8/20/2019 cs_am05 http://slidepdf.com/reader/full/csam05 1/4 s 391 B.E./B.Tech. EGREEEXAMINATION,APRIIIMAY 2005. Fifth Semester Electronics and Communication Engineering EC 334 - CONTROLSYSTEMS Time : Three hours Maximum: 100 marks Ordinary graph sheet,semilogsheet,polar graph sheet will be provided. Answer ALL questions. PARTA-(10 x2=20 marks) 1. What is the mathematical model of a system? 2. What is electrical analogous of a gear? 3. Write the transfer function of the PID controller. 4. What are the standard test signalsemployed or time domain studies? 5. State the rule for finding out the root loci on the real axis. 6. What is the condition for the system G(s) = * t *:,) to has a circie in its root s(s + b) locus? 7. List any two advantagesof frequencyresponseanalysis. 8. Define gain margin of a closed oop system.   w   w   w  .    M   a   a   n   a   v   a    N  .   c   o   m

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s 391

B.E./B.Tech.

EGREE

EXAMINATION,

APRIIIMAY 2005.

Fifth

Semester

Electronics

and Communication

Engineering

EC 334

-

CONTROL

SYSTEMS

Time

: Three

hours

Maximum:

100 marks

Ordinary

graph

sheet,

semilog

sheet,

polar

graph

sheet will be

provided.

Answer ALL

questions.

PARTA- (10

x2=20 marks )

1. What

is the

mathematical

model of a

system?

2. What

is electrical

analogous

of a

gear?

3.

Write

the transfer

function of the

PID controller.

4.

What are

the standard

test signals

employed

or time domain studies?

5. State the rule for finding out the root loci on the real axis.

6. What

is the

condition

for the system

G(s)

=

* t *:,)

to has a circie

in its root

s(s+ b)

locus?

7.

List

any two

advantagesof

frequency

responseanalysis.

8.

Define

gain

margin of a closed

oop system.

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9.

Draw

the

bode

piot

of a

typical

lead compensator.

10.

write

the transfer

function

of

a typical

iag-lead

compensator.

PARTB- (5x16=80marks )

11.

The

loop transfer

function

of a

feedback

control

system

is

given

by

K(s

+ 6)

G(s),F/(s)

 

s (s+4 )

(i)

Sketch

the

root

locus

plot

with

K

as

a

variable

parameter and show

that

loci

of

complex

oots

are

part

of

a

circle'

(ii)

Determine

the break-

awayhreak

in

points' if any'

(iii)

Determine

the

range

of K

for which

the system

s under

damped.

(iv)

Determine

the

value

of K

for critical

damping.

(v)

Determine

the

minimum

value

of

damping

ratio'

lZ.

(a) (i)

Derive

the

mathematical

model

of

an armature

controlled

DC

motor.

(ii)

For the

spring,

damper

and

mass

system

shown

in Fig.

12

(a) (ii),

Obtain

the

differential

equations

governing the system

f

is

the

force

applied.

Fig.

12

(a)

(ii)

Or

2

\rr

v

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(b) (i)

Using block

diagram

from each input to

Fis.

12

(b) (i).

reduction technique

find

the transfer

function

the output

C

for the system

shown

in

Fis. L2 b) i)

(ii)

Draw an equivalent signal

flow

graph

for the system

shown

in

Fig.

12

b) ii).

Fig. 12

(b) (ii)

13.

(a)

(i)

Derive the expression

or

unit impulse

response

of a second

order

under

damped system

G(s)

=

W:

s2+ 2zW,rs

W,?

(ii)

Find

the unit

impulse response

of the second

order

system

rvhose

transfer

function

G(S)

=

-

'

s "

+4s+9

Or

3

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(b)

(i)

Derive the expression

for steady

state error

of the closed loop

system

n terms of

generalizederror coefficients.

1

(ii)

For a closedoop

system with

G(s)

=;*

and .FI(s) 5,

calculate

generalized rrorcoefficientsnd ind the error series.

14.

(a)

Draw the bode

plot

of the system

G(s)

=

*t#Gtu.

Hence

obtain

the exact

plot

by

doingnecessary

orrections t corner

requencies.

(i)

Find the

gain

margin and,

phase margin

(ii)

The value of

K for

phase

margin

=

20".

Or

(b)

Test the stability

of the unity

feedbacksystem

G(s)

=

--.+

when

(s -1 ) ' ( s+5 )

K

=

10 using Nyquist criterion

and

then find the range of K for stability.

15.

(a)

The open

loop transfer

function of a uncompensated system

is

G(s)

=

.j -

. Design a suitable

lay compensator or the system so that

s(s

+ 2)

the static

velocity error constant

K, is

20

sec-l, the

phase

margin is

atieast 55oand the

gain

margin

is atieast 12 dB.

Or

(b)

Considera

type 1 unit f'eedback ystem

with an OLTF GsG)

=

--K-.11

'

s (s+1 )

is specified hat K,

=

12 sec-1 and.

Qry

=

40" Design

lead

compensator

v

to meet

the specifications.

e--

(

/_ , .__

//

,,

\-

,/-,

J \

) l

r/

/

, / - t

:

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