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25 10100
i1 i2
i3 i4
0.2V1V1+
25AA
BC
DE F
01. (a)Sol:
For half wave symmetry periodic signalshould contain odd harmonic components(f0, 3f0, 5f0 ,)(i) For x1(t),0 = G.C.D (2, 6, 10)
= 2Indicating I, III & V harmonicsexhibiting half wave symmetry(ii) For x2(t)0 = G.C.D (2, 4, 6)
= 2Indicating I, II & III harmonicsnot satisfying half wave symmetry.
01. (b).Sol. Given step response of an LTI system is,
tue1ts tSince, x(t) = rect (t 0.5) = u(t) u(t1)
L.T.IOutput is y(t) = s(t) s(t1)
111 1 tuetue ttAlternative:Using laplace transform solve for transferfunction
1s1
sXsY
sH . Then find the output.
01. (c)Sol: Given circuit is
The above diagram can be redrawn as
By applying KCL at Node (1) we geti1 0.2v1 + i2 + 10
v1=0
i1 + i2 = 0.1V1 ----- (1) andV1 = 25i1Substitute in equation (1), we geti1 + i2 = 0.1(25i1)
i2 = 1.5i1 ---- (2)By applying KCL at same node,
25 + 21 i100V = 0
25 + 21 i100V 11 i25V
25 +100
i25 1= 1.5i1
25 = 1i41 1.5i1
i1 = 20Ai2 = 1.5(20) = 30Ai2 = 30Av1 = 500 VBy applying KCL at Node B,i1 + 0.2 v1 + i3 = 0i3 = i1 0.2v1 = (20) 0.2500i3 = 20 100 = 80 Ai3 = 80 A
i3 25+i4+
105000
= 0
i4 = 5A
i1
A
C
E
i2
100
10
0.2v1
v1 +25
B
i3
D
i4
F
v1
(0v) (Node-1)
25A
: 3 : COV 1 Solutions
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01. (d)Sol: Given,
2t1;4t21t0;t2ti
= 0 ; other wise
F21C
We know that
dttiC1V
t
c
dtti2 t
dtti2tV tc
2dtt22t
0
; 0 t 1 dtti2tV tc
2dtti2 21
2422
1
t dtt
2421
2
ttt = 4t8t2 2 ; 1 t 2
The voltage across the capacitor in the interval1 t 2 is,Vc(t) = 2t2 + 8t 4
0 1 2
2i
t
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: 5 : COV 1 Solutions
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01. (e)Sol: From the given circuit
VTH = 0 and RTH:
By applying KCL at node VT is, 101
15V
15V4V TXT
155VV4V TXX
3VX = 4VX +VT VX = VT ---------(2)Sub (2) in (1)
115V
15V3 TT
2VT = 15VT = 7.5
5.71
VR TTH
Thevenins equivalent is
01. (f)Sol: In the given system, applied force f(t) is the
input and displacement x is the output.Let, Laplace transform of f(t) =L{f(t)}= F(s)Laplace transform of x = L {x} = X(s)Laplace transform of x1= L {x1}= X1(s)The system has two nodes and they are massM1, and M2. The differential equationsgoverning the system are given by forcebalanced equations at these nodes.
Let the displacement of mass M1, be x1.
The free body diagram of mass M1 is shown infigure. The opposing forces acting on mass M1are marked as fm1, fb1, fb, fk1 and fk.
fm1= M1 21
2
dtxd
; fb1 = B1 dtdx1 ; fk1 = K1x1;
fb = B dtd (x1 x) ; fk = K(x1 x)
By Newtons second law. fm1 + fb1+ fb + fk1 + fk = 0
M1 2dt1x
2d+B1
dt1dx +B
dtd (x1x)+K1x1+K(x1x) = 0
On taking Laplace transform of aboveequation with zero initial conditions we get,M1s2X1(s)+B1sX1(s)+Bs[X1(s)X(s)]+ K1X1(s)+ K [X1(s) X(s)]= 0X1(s) [M1 s2 + (B1+B)s + (K1 +K)] X(s)[Bs+K] = 0X1(s) [M1 s2 + (B1+B)s + (K1 +K)] = X(s)[Bs+K]X1(s) = )KK(s)BB(sM
KBs)s(X11
21
. (1)The free body diagram of mass M2 is show
in figure.
The opposing forces acting on M2 are markedas fm2, fb2, fb, fk.
2
2
22m dtxdMf ;
dtdxBf 22b
1b xxdtdBf ; 1k xxKf
By Newtons second law,
a
b
7.5
M1
x1
fm1fb1fbfk1fk
M2
x
fm2fb2fbfk
f(t)
+ 4Vx
a
b
155
10
Vx
+
VT
1AVT
+
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Mpc(tp)
12%5%
c(t)
0 td tr tp ts ts
0.5
t
fm2 + fb2 + fb +fk = f(t)
tfxx(K)xxdtdB
dtdxB
dtxdM 1122
2
2
On taking Laplace transform of aboveequation with zero initial conditions we get,M2s2X(s)+B2sX(s) + Bs[X(s) X1(s)]
+K [X(s) X1(s)] = F(s)X(s) [M2s2 + (B2 +B)s + K] X1(s) [Bs + K]
= F(s) (2)Substituting for X1(s) from equation (1) inequation (2) we get,X(s) [M2s2 + (B2 +B)s +K]
X(s) )s(F)KK(s)BB(sM)KBs(
112
1
2
2K)(BsKB)s2
(B2s2
M)K1
K(s)B1
B(2s1
M
)K1K(s)B1B(2
s1M
)s(F)s(X
01.(g)Sol: A control system is a combination of
elements arranged in a planned manner wherein each element causes an effect to produce adesired output. This cause and effectrelationship is governed by a mathematicalrelation. In control system the cause actsthrough a control process which in turn resultsinto an effect.
Control systems are used in manyapplications for example, systems for thecontrol of position, velocity, acceleration,temperature, pressure, voltage and current etc.
Control systems can be broadly divided intwo types.(i) open loop control system
The accuracy of an open loop systemdepends on the calibration of the input. i.e.,output is independent of input.Eg: Traffic control system
Traffic control by means of traffic signalsoperated on a time basis constitutes an openloop control system. The sequence of controlsignals are based on a time slot given for eachsignal. The time slots are decided based on atraffic study. The system will not measure thedensity of the traffic before giving the signals.Since the time slot does not changes according
to traffic density, the system is open loopsystem.(ii) Closed loop control system:
The output of a system depends on input.Eg: Bread Toaster.
Traffic control system can made as aclosed loop system if the time slots of thesignals are decided based on the density oftraffic. In closed loop traffic control system,the density of the traffic is measured on all thesides and the information is fed to a computer.The timings of the control signals are decidedby the computer based on the density oftraffic. Since the closed loop systemdynamically changes the timings, the flow ofvehicles will be better than open loop system.
01.(h)Sol: Time domain specifications (or) transient
response parameters:
Delay time (td): It is the time taken by theresponse to change from 0 to 50% of itsfinal/steady state value.
5.0tt
)t(cd
n
d7.01
t
Rise time (tr): It is the time taken by theresponse to reach from 0 to 100%. Generally10% to 90% for over damped and 5% to 95%for critically damped system is defined.
1)tsin(1
e11tt
)t(c rd2t
r
rn
drt
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Peak time (tp): It is the time taken by theresponse to reach the maximum value.
dp
pt,0
ttdt)t(dc
Time period of damped oscillations isequal to the twice of the peak time = 2tpMaximum (or) Peak overshoot (Mp): It isthe maximum error at the output
21p eM
1)t(cM pp ,
%100)(c)(c)t(c
M% pp
If the input is doubled, then the steadystate and peak values double, thereforemagnitude of Mp doubles but % Mp remainsconstant.
Settling time (ts): It is the time taken by theresponse to reach 2% or 5% toleranceband as shown in the fig above.
i.e.., snte = 5% (or) 2%
n
s
3t for 5% tolerance band.
n
s
4t for 2% tolerance bandIf increases, rise time, peak time increasesand peak overshoot decreases.
02. (a).Sol: Given impulse response is, h(t) = et u(t).
Inverse of the system is hI(t) = k1(t) + k2 tand
1s1
sH By applying Laplace transform,
Hinv(s) = K1+sK2By given H(s) . Hinv(s) = 1
1
1ssKK 21
To make this K1= K2 = 1
02. (b)Sol: Fourier coefficient an:
0n
0n0n )tfn2(sinb)tfn2(cosa)t(f
Multiply both sides by cos (2nf0t) andintegrate from
2T
to2
T 00
2/T
2/T0
0
0
dt)tnf2cos()t(f
2/T
2/T 0n0
2n
0
0
)tnf2(cosa
dt)tnf2sin()tnf2cos(b 00n
dt)nf2sin()tnf2cos(b2
)tnf22(cos1a
00n
0
0nn
20T
20T
2/T
2/T0
n
2/T
2/T
n0
0
0
0
dt)tnf22cos(2
adt2
a
+ dt)tnf2sin()tnf2cos(b 02/T
2/T0n
0
0
00T2a
0n
2/T
2/T0
0n
0
0
dttnf2costfT2
a
02. (c)Sol: Sampling Theorem:
Sample the signal g(t) instantaneously andat a uniform rate, once every Ts seconds.
We refer to Ts as the sampling period, andto its reciprocal 1/Ts as the sampling rate.
This ideal form of sampling is calledinstantaneous sampling.
g(t)
t0
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Sampling theorem for bandlimited signalsof finite energy.
A bandlimited signal of finite energy,which has no frequency components higherthan W hertz, is completely described byspecifying the values of the signal at instantsof time separated by 1/2W seconds.
ORA band-limited signal of finite energy,
which has no frequency components higherthan W hertz, may be completely recoveredfrom a knowledge of its samples taken at therate of 2W per second.
Flat-Top sampling:The analog signal g(t) is sampled
instantaneously at the rate 1/Ts ,and theduration of each sample is lengthened to T .
The flat-top sampled signal s(t) is shown inFig.2
By using flat-top samples, amplitudedistortion as well as a delay of T/2are introduced. This effect is similar to thevariation in transmission with frequency thatis caused by the finite size of the scanningaperture in television and facsimile.Accordingly, the distortion caused bylengthening the samples, is referred to as theaperture effect. This distortion may becorrected by connecting an equalizer in
cascade with the low-pass reconstructionfilter.
02. (d)Sol: Given signal x(t) is shown below
x(t) = 2 [u(t) u(t2)]+(2t2) [u(t2)u(t 3)]+(2t+10) [u(t3)u(t4)]+2[u(t4)u(t6)].
= 2 u(t) + u (t2) [2t22]+u(t3)[2t+102t+2] + u (t4) [210+2t]
2u(t6)
6tu24tr23tr42tr2tu2)t(x
03. (a)Sol:
As we know u(t)*u(t) = r(t) = tu(t) 4tu1tu*2tu21tututh*tx 4tu*2tu21tu*2tu24tu*
1tu1tu*1tu4tu*tu1tu*tu
6tr23tr25tr2tr4tr1tr 6tr25tr4tr3tr22tr1tr
03. (b).Sol: Given
Input of system is, x(t) = et u(t)Output of system is, y(t) = e2t u(t) + e3tu(t) Frequency response of the system is,
j11
j31
j21
XY)(H
g(t)
t0
TsFig. 2
T
s(t)
0 2 4 6 t24
x(t)
t2 3 4 5 6
2
31
1
g(t)
0
Ts
t
Fig.1
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6j5j
j25j12
j32
j212
By applying Inverse Laplace Transform
I.R tue2tuet2th t3t2
03. (c)Sol: The differential equation is given by
)t(x)t(ydt
)t(dy 4Apply Fourier transform to the abovedifferential equation
)(X)(Y)(Yj 4
j)(X
)(Y)(H41
Given x(t) =sin4 t + cos (6 t+ /4) H,)(H 216
1= tan-1( )4/
At 0 = 4 ; 20 4161H
075.018.13
1913.173
1
441tanH o
4034672 01 ..tan
At 0=6 20 6161H
051.025.19
19456.370
1
5.1tan4
6tanH 110
= 78.010= 0.43y(t) = 0.075 sin(4 t 72.340)
+0.05cos(6 t+ /4 78.010)= 0.075sin (4 t 0.4 )
+0.05cos (6 t+ ). 4304
03. (d)Sol: Apply z transform to the given differential
equation
zXz8.0zXzzXz6.0zX4.0zYz4.0zYz6.0zYz8.0zY
321
321
321321
z4.0z6.0z8.01z8.0zz6.04.0
zXzY
zH
No. of delays = No. of state variables = 3q1(n), q2 (n), q3(n) are state variables.
H() ooo Htsin.H Sin 0t
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z
-1
z-1
z-1
y[n]
0.6
1
0.8
0.6
0.8
x[n]
0.4
1 0.4
q3(n)=q2(n+1)
q2(n)=q1(n+1)
q1(n)
q3(n+1)
nxnq8.0nq6.0nq4.01nq 3213 nq1nq 32 nq1nq 21 nq8.0nqnq6.01nq4.0ny 1233 nq8.0nqnq6.0
nxnq8.0nq6.0nq4.04.0ny
123
321
nq8.0nqnq6.0nx4.0
nq32.0nq24.0nqn16.0ny
123
3211
nx4.0nq28.0nq76.0nq64.0ny 321 Q(n+1) = AQ(n) + Bx(n)
y(n) = CQ(n) + Dx(n)
nx100
nqnqnq
8.06.04.0100010
1nq1nq1nq
3
2
1
3
2
1
nx4.0nqnqnq
28.076.064.0ny
3
2
1
8.06.04.0100010
A
100
B ; 28.076.064.0C
4.0D
04.(a)Sol:
V3 = 2VApply KCl at Node V1
02
2V1
VV5.0
2V 1211
02
2VVV4V2 1211 4V1 8 + 2V1 2V2 +V1 2 = 07V1 2V2 = 10 ---- (1)Apply KCl at Node V2.
015.0
V1
2V1
VV 2212
01V22VVV 2212 3V4V 21 ----- (2)
Solve for (1) & (2)V1 = 26
31V,1323
2
i1 = A577.0A2615
1VV 21
04.(b)Sol: Use thevenins Theorem
by using Nodal analysis at Node A
512V
= 12
V 12 = 60 V = 72
I1 = 560
57212 = 12 A
10 I1 = 10 12 = 120 VFinding Vth by applying KVL in Loop
0.5
2 V+
+
2 1
1
1
0.5 1 A
2 V
i1V3V2V1
I1
12V 12A
5
1
20V
+
+
10 I1+
+ VTh
V
: 11 : COV 1 Solutions
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72 ( 120) Vth 20 = 072 + 120 20 = Vth
Vth = 172 VFinding Rth by disabling all sources.No Independent source, so by applying currentof 1 A across 1 & 2
By applying KVL in Loop. 5 I1 10 I1 V I1 = 05 + 10 V + 1 = 0V = 16RTh = 2
V= 16
I = 8.6A04. (c)Sol:
sVsI
3s2ss1s12
sY
V(t) = (t); V(s) = 1 3s2ss
1s12sI
3s
C2s
Bs
AsI
3s2s1s12LtssILtA
0s0s
232112
6232112
sI2sLtB2s
8C
3s8
2s6
s
2sI
i(t) = 2u (t) + 6e2t u(t) 8e3tu(t)if v(t) = u(t)V(s) = 1/s 3s2ss
1s12sI 2
3sD
2sC
s
Bs
A2
232112
sIsLtA 20s
312112
sI3sLtC 20s
38
19212
sI3sLtD3s
3s2s1s12
dsdLtB
0s
23s2s
5s21s3s2s12
31
325612 2
I(s) = 2t u(t) + 1/3 u(t) 3e2tu(t) + 8/3e3t u(t)04. (d)Sol: KCL at node 1 gives
i(t) = iR + iCet U(t) = v(t) 2+j---(1)
The Fourier transform is given by
Let U(t) = j11
Lv(t) = V(j)Taking the Fourier transform on both sides ofequation (1).
j2)j(Vj11
V(j) = j2j11
j21
j11
V(j) =2/j1
5.0j1
1
Talking the inverse Fourier transformV(t) = L-1 -2tt eejV volts.
05. (a)Sol: In many practical situations, a circuit is
designed to provide power to a load. There areapplications in areas such as communicationswhere it is desirable to maximize the powerdelivered to a load. We now address theproblem of delivering the maximum power to
I1 5
1A
+
10 I1+
1
V
16
172V 4+
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a load when given a system with knowninternal losses. It should be noted that this willresult in significant internal losses greater thanor equal to the power delivered to the load.
The Thevenin equivalent is useful in findingthe maximum power a linear circuit can deliver to aload. We assume that we can adjust the loadresistance RL. If the entire circuit is replaced by itsThevenin equivalent except for the load, as shownin fig, the power delivered to the load is
L
2
LTh
ThL
2 RRR
VRiP
--- (1)For a given circuit, VTh and RTh are fixed. By
varying the load resistance RL, the power deliveredto the load varies as sketched in fig (b) . we noticefrom fig (b) that the power is small for small orlarge values of RL but maximum for some value ofRL between 0 and . We now want to show that thismaximum power occurs when RL is equal to RTh.This is known as the maximum power theorem.
Maximum power is transferred to the loadwhen the load resistance equals the Theveninresistance as seen from the load (RL= RTh).To prove the maximum power transfer theorm. Wedifferentiate P with respect to RL and set the resultequal to zero. We obtain.
4
LTh
LThL2
LTh2Th
L RRRRR2RRV
dRdP
0RR)R2RR(V 3
LTh
LLTh2Th
This implies that0 = (RTh + RL 2RL) = (RTh RL)
Which yields
RL = RTh ---(2)Showing that the maximum power transfer takesplace when the load resistance RL equals theThevenin resistance RTh. We can readily confirmthat equation (2) RL = RTh gives the maximumpower by showing that d2P/dR2L 0The maximum power transferred is obtained bysubstituting for
pmax =Th
2Th
R4V
--- (3)
Equation (3) applies only whenRL= RTh, where RL RTh we compute thepower delivered to the load using equation (1).
05. (b)Sol: When switch is in position 1 for long time. It
will go to steady state condition inductor willacts as a short circuit .
Current through inductor A22550
RVIL
A20i0i LL When switch moved to position (2)Inductor acts as a current source of 2A
By converting inductor current and inductorparallel network into series it will look like
+VTh
RTh a
b
RL
i
Fig. (a) The circuit used formaximum power transfer
RL
Pmax
RTh
P
Fig. (b) Powerdelivered to the loadas a function of RL
100/S25
iL(0) 2s
100/S
25
2S
+ 4
50V25
iL(0)
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05.(c)Sol: figures shows the transformed network of
Figure is further simplified to as shown inabove figure
Thevenins impedance ZTH
1s2
1s1s1s1s
1s1sZZ xyTH
=
21s
Open-Circuit VoltageVOC
Voc = 1s21
s
1s2
1s1s2
1
ZZV
ILTH
OC3R
s2
2s2ss1s2
1
2
2s3s1s s2 2s1s1s
s
2sC
1sB
1sA
2
1s2
2s1s1ss1sB
1s2ss
121
1
2s2 2s1ss2sC
2122
2
1s
22
2s1ss1s
dsdA
1s2s
s
dsd
1s22s
1s12s
= 1s22ss2s
1s22s2
2212
2 Therefore,
2s2
1s1
1s2
sI 23R
or
tue2tee2ti t2tt3R 05. (d)Sol:
6sK
2sK
s
K6s2s3s1s2
s
sF 210
2
16s2s3s1s2K
0s0
41
6ss3s1s2K
2s1
45
2ss3s1s2K
6s2
6s
45
2s41
s21
s
sF
6s
s45
2s
s41
21
sF
+
1S
1
S+1
S
1S X
Y
S+1
+
1S
1
S R3
1
1/S
S
1
1
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+++
+
+ G3
G4
G11H2G1
2G
1/G3H1
C(s)R(s)
H2
++
+ ++
H1
H2
G1 G3
G4
R(s) C(s)
1H2G12G
if F(s) is an impedance function, i.e.,
,6s
s45
2s
s41
21
sZ
:H81
241
KL;K41R;
21KR
1
111100
H245
645
KL;45KR
2
2222
The foster form I synthesized network isshown in Fig. (a).
if F(s) is an admittance function, i.e.
6s
s45
2s
s41
21)s(Y
;F81
241
KC;4K1R;2
K1R
1
11
11
00
F245
645
KC;54
K1R
2
22
22
06.(a)Sol:
Step1: Splitting the summing point andrearranging the branch points
Step 2: Eliminating the feedback path
Step 3: Shifting the branch point after theblock
Step 4: Combining the blocks in cascadeand eliminating feedback path
Step5: Combining the blocks in cascade andeliminating feedback path
++
++
+G1 G2 G3
H1
C(s)R(s)
H2
G4
++
+ +
++
C(s)R(s)
H2
G1 G2 G3
G4
H1H1
++++
G4
G1
H1/G3
C(s)R(s)23212
32HGGHG1
GG
1/8H 5/24H
5/41/41/2
ZRL (s)
YRC (s)2 4
1/8F 5/24F4/5
: 15 : COV 1 Solutions
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Step 6: Eliminating forward path
412123212
321 GHGGHGGHG1
GGG)s(R)s(C
06.(b)Sol: The characteristic equation of the system is
s5+4s4+8s3+8s2+7s+4=0.The given characteristic polynomial is 5thorder equation and so it has 5 roots.s5: 1 8 7s4: 1 2 1s3: 1 1s2: 1 1s1 : s0: 1
When 0, there is no sign change in thefirst column of routh array. But we have arows of all zeros (s1 row or row-5) and so thereis a possibility of roots on imaginary axis. Thiscan be found from the roots of auxiliarypolynomial. Here the auxiliary polynomial isgiven by s2 row.
The auxiliary polynomial is, s2 + 1 = 0; s2 = 1 or s = 1 = j1The roots of auxiliary polynomial are +j1, andj1, lying on imaginary axis. The roots ofauxiliary polynomial are also roots ofcharacteristic equation. Hence two roots ofcharacteristic equation are lying on imaginaryaxis and so the system is limitedly ormarginally stable. The remaining three roots ofcharacteristic equation are lying on the lefthalf of s-plane.
06.(c)Sol: (i) )3s()1s(s
)2s(20)s(G
Let us assume unity feedback system, H(s) = 1
The open loop system has a pole atorigin. Hence it is a type-1 system. Insystems with type number 1, thevelocity (ramp) input will give a constantsteady state error.
The steady state error with unit
velocity input, ess =vK
1
Velocity error constant, Kv=0s
Lt
sG(s) H(s) Kv =
0sLt
sG(s)
= )3s()1s(s)2s(20
sLt0s
=
31220
=
340
Steady state error, ess =vK
1=
403
= 0.075
(ii) )3s()2s(10)s(G
Let us assume unity feedback system, H(s) = 1
The open loop system has no pole atorigin. Hence it is a type-0 system. Insystems with type number 0, the stepinput will give a constant steady stateerror.
The steady state error with unit step input,
ess =pK1
1
Position error constant,Kp =
0sLt
G(s) H(s)
sGLt0s
= )3s()2s(10Lt
0s = 3210 = 3
5
Steady state error, ess =pK1
1 =
351
1
=
533 = 8
3 = 0.375
1H2G1G2H3G2G1H2G13G2G1G ++
G4
C(s)R(s)
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(iii) )2s()1s(s10)s(G 2
Let us assume unity feedback system, H(s) = 1.The open loop system has two poles atorigin. Hence it is a type-2 system. Insystems with type number-2, theacceleration (parabolic) input will give aconstant steady state error.The steady state error with unityacceleration input,
ass K
1e .
Acceleration error constant,Ka =
0sLt
s2 G(s) H(s) =
0sLt
s2 G(s)
= )2s()1s(s10
sLt 22
0s = 2110 = 5
Steady state error, ess =aK
1=
51
= 0.2
06.(d)Sol: Given that, c(t) = 1+0.2e60t 1.2 e10t
On taking Laplace transform of c(t) we get,C(s) = )10s(
12.1)60s(12.0
s
1
= )10s()60s(s)60s(s2.1)10s(s2.0)10s()60s(
=
)10s()60s(ss722s2.1s22s2.0600s702s
= )10s()60s(s600
= )10s()60s(
600s
1
Since input is unit step, R(s) = 1/s C(s) = R(s) )10s()60s(
60
= R(s)600s70s
6002
The closed loop transfer function of thesystem,
600s70s600
)s(R)s(C
2
The damping ratio and natural frequency ofoscillation can be estimated by comparing thesystem transfer function with standard form ofsecond order transfer function.
2nn
2
2n
s2s)s(R)s(C
=
600s70s600
2 On comparing we get, 2n = 70 and
2n = 600 43.149.242
70270
n
n = 600 = 24.49 rad/sec.07. (a)Sol: (i) The sensitivity of overall transfer function
(M) w.r.t. forward path transfer function (G) isgiven by
)s(H)s(G11SMG
25.6s2ss2s
25.0)2s(s251
12
2
Put js
25.62j2jS 2
2MG
Put 1 .
25.612j112j1S 2
2MG
398.02j25.5
2j1
(ii) The sensitivity of overall transfer function(M) w.r.t. feedback path transfer function(H) is given by
)s(H)s(G1)s(H)s(GSMH
25.6s2s25.6
25.0)2s(s251
25.0)2s(s25
2
Put s = j
25.62j25.6S 2
MH
put 1 11.1
2j25.525.6
25.612j125.6S 2
MH
: 17 : COV 1 Solutions
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1 1
3 4 521
G1 G2 C(s)R(s)6
1
1 2 3 4 5 6
G3
C(s)R(s) 1 1 1
1 2 3 4 5 6R(s) C(s)1 1
1 G1 G2
G3
H
07.(b)Sol: The nodes are assigned at input, output, at
every summing point and branch point asshown in figure.
The signal flow graph of the above system isshown in figure.
Forward Paths:There are two forward paths K = 2Let the forward path gains be P1 and P2
Gain of forward path-1, P1 = G1G2Gain of forward path-2, P2= G3
Individual Loop GainThere is only one individual loop. Let the
individual loop gain be P11Loop gain of individual loop-1,P11 = G1H
Gain Products of Two Non-touching LoopsThere are no combinations of non-touching
loops.Calculations of and K : = 1 [P11] = 1 + G1H
Since there are no part of the graph which isnon-touching with forward path-1 and 2,1 = 2 = 1Transfer Function, T
By Masons gain formula the transferfunction, T is given by,
T = 1 PK K =
1 [P11 + P22]
=HG1GGG
1
321
07.(c)Sol: The overall transfer function for the system is
)2s3s(
2)s(R)s(C
or
1.)3s(s21
)3s(s2
)s(R)s(C
2
It is noted that the denominator of the aboveexpression can be factored as [(s+1)(s+2)]
)2s)(1s(2)s(R)s(C
As the input is a unit steps/1)s(R
)2s)(1s(2
.
s
1)s(C The R.H.S. of the above expression can beexpanded into partial fraction as follows:
)2s(3K
)1s(K
s
K)2s)(1s(
2.
s
1 21
The coefficients 321 KandK,K can bedetermined as
1Kand2K,1K 321
2s1
)1s(2
s
1)s(C Taking inverse Laplace transform on bothsides, .tuee21)t(c t2t
07.(d)Sol: The overall Transfer function is given by
TK
sT1
s
T/K
1.)1sT(sK1
)1sT(sK
)s(R)s(C
2
+G1 G2
G3
H
C(s)R(s)+
1
23 4 5 6
4321 G1
H
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The characteristic equation is
0TK
sT1
s2
T/12andT/K nn
KT21
T/K21
.
T1
21
.
T1
n
Let 1K be the forward path gain when
%60M 1p and the corresponding dampingratio be .1Since
100e60%100eM21
121
1
111p
or )e(log1
)6.0(loge2
1
1e
1.1
51.0or21
1
)1(51.0 2122
21
or
025.0or)1(026.0 212121 158.01
Let 2K be the forward path gain when%20M 2p and the corresponding damping
ratio be .2Since
100e20%100eM22
222
2
112p
From the above relation the value of 2 can becalculated as
447.02 Assuming time constant T to be constant
TK1
.
21
andTK
1.
21
22
11
1TK2
TK1
.
21 2
12
1
Hence, .81
447.0158.0
KK 2
2
2
1
1
2