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EXPERIMENT – 1
TIME RESPONSE OF A SECOND ORDER SYSTEM
AIM: To study the time response of second order system.
APPARATUS:
1. Second order system kit2. Function Generator3. CRO4. Connecting wires
CIRCUIT DIAGRAM:
Fig: 1.1. Second Order System using RLC
THEORY:
PROCEDURE:
1. Apply square wave input of magnitude 5V peak to peak
2. Connect the output to CRO and measure the output voltage for various points.
3. Repeat for various values of ξ = 0.3, 0.7, 1, 2.
1
0 – 10 K
FORMULAE:
1. ωn = 1/√LC
2. ξ = (R/2) √(C/L)
3. tr = [(П – tan-1(√1-ξ2)/ ξ]/( ωn((√1-ξ2))
4. tp = П/ (ωn((√1-ξ2))
5. Mp = e((-Пξ)/( √1-ξ2))
6. td = (1+ 0.7 ξ)/ ωn
7. ts = 4/ ξωn for 2% tolerance band
GRAPHS:
Fig:1.2. Step Response of an under damped system
RESULT:
COMCLUSION:
2
Vol
tage
Time (msec)
0.5
ess
ts
1
EXPERIMENT - 2
CHARACTERISTICS OF SYNCHROS
AIM:
1. To study synchro transmitter.
2. To Study synchro transmitter and receiver pair.
APPARATUS:
1. Synchro transmitter Receiver pair trainer kit.
2. Patch chords.
PROCEDURE:
SYNCHRO TRANSMITTER
1. Connect the main supply to the system with the help of cable provided. Do not
interconnect S1, S2 and S3 to S11, S2
1, S31.
2. Switch ON main supply for the unit and transmitter rotor supply.
3. Starting from zero position, note down the voltage between stator winding
terminals ie., Vs1s2, Vs1s3, Vs2s3, in a sequential manner. Enter the readings in a
tabular form and plot the graph of angular position Vs rotor voltages for all the 3-
phases.
4. Note that zero position of the stator coincide with Vs3s1, voltage equal to zero
voltage. Do not disturb this condition.
SYNCHRO TRANSMITTER RECEIVER PAIR
1. Connect the main supply cable
2. Connect S1, S2 , S3 terminals transmitter to S1, S2, S3 of synchro receiver by patch
chords provided respectively.
3. Switch ON rotor supply of both transmitter and receiver and also switch ON the
main supply.
4. Move the pointer i.e. rotor position of synchro transmitter in steps of 300 and
observe the rotor position. Observe that whenever transmitter rotor is rotated, the
receiver rotor follows it for both the directions of rotations and their positions are
in good agreement.
5. Enter the input angular position and output angular position in the tabular form
and plot a graph.
3
CIRCUIT DIAGRAM:
Fig: 2.1. Synchro transmitter and receiver pair
4
THEORY:
TABULAR COLUMN:
Synchro Transmitter:
S.NO Rotor Position
in degrees
Vs3s1 Vs1s2 Vs2s3
0
30
60
.
.
.
.
.
.
330
Synchro transmitter & Receiver Pair:
S.NO Rotor position of
transmitter in degrees
Rotor position of receiver in
degrees
0
30
60
.
.
.
.
330
5
GRAPHS:
SYNCHRO TRANSMITTER
Fig: 2. 2.
SYNCHRO TRANSMITTER RECEIVER PAIR
Fig: 2.3
RESULT:
COLCLUSION:
6
Rec
eive
r an
gula
r po
siti
on
Transmitter angular position
Sta
tor
indu
ced
line
vo
ltag
e
V
θ
Vs1s3 Vs3s2 Vs2s1 Vs1s3
EXPERIMENT - 3
EFFECT OF FEEDBACK ON DC SERVO MOTOR
AIM :
To study DC position control with and without feedback.
APPARATUS:
DC Position control trainer kit.
CIRCUIT DIAGRAM:
Fig: 3.1. DC Position Control System
THEORY:
PROCEDURE:
1. The switches SW3 , SW4 are initially OFF and are ON as soon as the power
supply is ON.
e a
J2M
7
Am
pli
fier
5 V
2. Keeping the SW1 switch open adjust the input to different values and note down
the corresponding output and the deviation.
3. Now keeping the SW1 ON note down the output for different values of input in
both degenerative and regenerative modes and also the deviation.
TABULAR COLUMN:
1. TACHO OUT:
S.NO INPUT OUTPUT DEVIATION
2. TACHO DEGENERATIVE:
S.NO INPUT OUTPUT DEVIATION
8
3. TACHO IN (REGENERATIVE):
S.NO INPUT OUTPUT DEVIATION
GRAPHS:
Fig: 3.2. Tacho Out Fig: 3.3 Tacho IN (Regenerative)
Fig: 3.4 Tacho IN ( Degenerative)
RESULT:
CONCLUSION:
9
PositionPosition
Position
Dev
iati
on
Out
put
Dev
iati
on
EXPERIMENT - 4
EFFECT OF P, PD, PI, PID CONTROLLER ON A SECOND ORDER SYSTEM
AIM:
To study the effect of proportional, integral, differential, controllers on a second
order system.
APPARATUS:
1. Microprocessor based PID controller trainer kit.
2. Patch chords
CIRCUIT DIAGRAM:
Fig: 4.1. Effect of PID on second order system
THEORY:
PROCEDURE:
PROPORTIONAL CONTROLLER
1. Select DC source set the amplitude of a dc source to some predefined value.
2. Connect the PID output to time constant – 1 input, connect time constant -1
output to feed back input –VF. Set the PID parameter P-20.00, I and D = 0. Now
start the PID controller. It shows run. Note down Vs, VF , Error and PID output.
3. Repeat this for different values of proportional gain and tabulate the result.
10
PID Controller Second OrderSystem
Verr VPID
OutputVs
PROPORTIONAL INTEGRAL CONTROLLER
1. Select DC source set the amplitude of DC source to some value.
2. Connect DC source to set input Vs connect PID output to time constant – 1 input,
time constant – 1 output to feed back input – VF
3. Set P – to some value, ‘I’ to some value and‘d’ to zero now start the controller.
Note down Vs, VF, Verr and PID output voltages. Repeat this for different values of
P and I, gain and tabulate then readings.
PROPORTIONAL DERIVATIVE CONTROLLER
1. Repeat the above with P and D gain settings keeping I gain at 0.
2. Tabulate the readings of Vs, VF and Verr and PID output.
PROPORTIONAL INTEGRAL DERIVATIVE CONTROLLER
1. Repeat the above process for different P, D and I gains.
TABULAR COLUMN:
P – CONTROLLER
S.NO P - Gain Set voltage
Vs
Feed back
voltage VF
Error
Voltage
PID o/p Vo
I - CONTROLLER
11
S.NO P - Gain Set voltage
Vs
Feed back
voltage VF
Error
Voltage
PID o/p Vo
D - CONTROLLER
S.NO P - Gain Set voltage
Vs
Feed back
voltage VF
Error
Voltage
PID o/p Vo
PI - CONTROLLER
S.NO P - Gain Set voltage
Vs
Feed back
voltage VF
Error
Voltage
PID o/p Vo
PD - CONTROLLER
12
S.NO P - Gain Set voltage
Vs
Feed back
voltage VF
Error
Voltage
PID o/p Vo
PID - CONTROLLER
S.NO P - Gain Set voltage
Vs
Feed back
voltage VF
Error
Voltage
PID o/p Vo
RESULT:
COLCLUSION:
EXPERIMENT - 5
13
STATE SPACE MODEL FOR CLASSICAL TRANSFER FUNCTION USING
MATLAB
AIM: To write a program using MATLAB to transform a transfer function into state
space and vice versa
PROGRAM:
a= input (‘enter “1” for tf to to ss conversion and “2” for ss to tf conversion’);
If a= =1
num=input(‘enter the numerator of tf’);
den= input(‘enter the denominator of tf’);
[A,B,C,D] = tf 2 ss (num,den);
A,B,C,D
End
If a= =2
A=input(‘enter the system matrix’);
B=input(‘enter the input matrix’);
C=input(‘enter the output matrix’);
D=input(‘enter the transmission matrix’);
[num,den]=ss2tf(A,B,C,D);
Num,den
end
y=tf(num,den)
RESULT:
CONCLUSION:
EXPERIMENT - 6
14
LAG AND LEAD COMPENSATION – MAGNITUDE AND PHASE PLOT
AIM:
1. To Study lead compensation.
2. To study lag compensation.
3. To study lead lag compensation.
APPARATUS:
1. Trainer kit.
2. Function generator.
3. Connecting wires.
CIRCUIT DIAGRAM:
1. LAG NETWORK:
Fig: 5.1.
2. LEAD NETWORK:
15
Fig : 5.2.
3. LIMITED LAG NETWORK
Fig: 5.3.
4. LIMITED LEAD NETWORK:
16
Fig: 5.4.
5. LAG LEAD COMPENSATION NETWORK
Fig: 5.5.
17
THEORY:
PROCEDURE:
1. Circuit is to be connected as per the circuit diagram.
2. Give a sinusoidal function as input using a function generator with an amplitude
of 3V.
3. Select various frequencies and give as input to the lag, lead and lag lead
compensating networks.
4. Note the phase angle from the phase angle meter and tabulate the input and output
voltages for different frequencies.
5. Calculate the phase angle theoretically and verify with the indicated value.
6. Draw the frequency and phase plots.
TABULAR COLUMN:
1. LEAD NETWORK
S.NO Freq(Hz) ω=2Пf V0(V) Vi(V) Gain
A(dB)
Indicated
T(j ω)θ
Calculated
T(j ω)θ
18
2. LAG NETWORK
S.NO Freq(Hz) ω=2Пf V0(V) Vi(V) Gain
A(dB)
Indicated
T(j ω)θ
Calculated
T(j ω)θ
3. LIMITED LAG NETWORK
S.NO Freq(Hz) ω=2Пf V0(V) Vi(V) Gain
A(dB)
Indicated
T(j ω)θ
Calculated
T(j ω)θ
19
4. LIMITED LEAD NETWORK
S.NO Freq(Hz) ω=2Пf V0(V) Vi(V) Gain
A(dB)
Indicated
T(j ω)θ
Calculated
T(j ω)θ
5. LAG LEAD NETWORK
S.NO Freq(Hz) ω=2Пf V0(V) Vi(V) Gain
A(dB)
Indicated
T(j ω)θ
Calculated
T(j ω)θ
20
GRAPHS:
1. Lag network
2. Lead network
3. Limited lag network
4. Limited lead network
5. Lag lead network
RESULT:
CONCLUSION:
21
EXPERIMENT - 7
TRANSFER FUNCTION OF A DC GENERATOR
AIM: To determine the transfer function of a DC generator after determining the various
constants
APPARATUS:
1. D.C. Motor-Generator set.
2. Motor stator.
3. Field rheostat for Motor.
4. Rheostat as potential divider for excitation of generator.
5. Ammeter M.C,M.I
6. Voltmeter M.C,M.I
7. Tachometer.
8. Variac and connecting wires.
THEORY
PROCEDURE:
1. Make the connections as per the circuit diagram, keep the motor field rheostat
in minimum position and potential divider also kept in minimum potential
position.
2. Start the motor with the help of motor starter and adjust the speed to rated
value.
3. To determine Kg ,magnetization characteristics If vs Vg of separately excited
DC generator has to be found use the straight line portion to determine
Kg =Vg / If
22
4. The field resistance of generator Rf is determined by drop test method as
shown in fig 6.2
5. To find Lf of generator, first the impedance Zf is determined by voltmeter and
ammeter method as shown in fig 6.3 using A.C. supply and determines X f and
Lf.
6. Plot the magnetization characteristics between Generated voltage vs Field
current
CIRCUIT DIAGRAM:
Fig: 6.1. O.C.C of a DC Generator
z
zz
z
zz
M G
23
Fig: 6.2. Field resistance Drop Test
Fig: 6.3. Field Impedance Drop Test
24
TABULAR COLUMN:
1) Magnetization Characteristic :
S.No. Field current If(Amps) Generated voltage (Volts)
2)Field Resistance Rf:
S.No. V(volts) I(amps) Rf=V/I
25
3)Field Impedance:
S.No. V I Z=V/I
CALCULATIONS:
Field Resistance Rf = 1.2*Rfavg
Xf = (Zf2 - Rf
2 )0.5
Field Inductance Lf = Xf / (2*П*f)
To calculate the Kg ,The linear portion of the magnetizing characteristics is
required Kg=Vg/If
Therefore, The Transfer Function of a DC Generator is given by
Vg(s) /Vf(s) = Kg / ( Lf S+Rf)
26
MODEL GRAPH:
Field Current If
RESULT:
CONCLUSION:
27
Gen
erat
ed V
olta
ge E
g
EXPERIMENT - 8
TEMPERATURE CONTROLLER USING PID
AIM:
To study the phenomenon of steady state error of a temperature control system
using proportional controller, proportional integral controller and proportional differential
controller.
APPARATUS:
1. Trainer kit
2. Connecting wires
CIRCUIT DIAGRAM
Fig: 7.1 . Proportional Controller
θ
28
Fig: 7.2. Proportional Integral Controller
Fig:7.3. Proportional Derivative Controller
θ
θ
29
THEORY:
PROCEDURE:
1. Establish the connection between the conditions unit and the model process with
the help of cable provided.
2. Connect Red 3, Black 1 for P – controller, Red 3, Black 2, and Red 1, Black 1 for
PI controller, RED 3, Black 3 and Red 2 , Black 1 for PD controller with the help
of patch chords.
3. Set the ‘SET’ potentiometer at position of 16Ω corresponding to 400 of
temperature.
4. Set proportional band control to 10% i.e. K1 = 10
5. Now turn ON the power supply.
TABULAR COLUMN:
P CONTROLLER
S.NO LOW SPEED DEVIATION HIGH SPEED
DEVIATION
30
PI CONTROLLER
S.NO LOW SPEED DEVIATION HIGH SPEED
DEVIATION
PD CONTROLLER
S.NO LOW SPEED DEVIATION HIGH SPEED
DEVIATION
31
GRAPHS:
Fig:7.4. P – Controller Fig: 7.5. PI - Controller
Fig: 7.6. PD - Controller
RESULT:
CONCLUSION:
32
Low Speed
High SpeedTime(sec)
Dev
iati
on
Low Speed
High Speed
Time (Sec)
Dev
iati
onHigh Speed
Low Speed
Time (Sec)
Dev
iati
on
EXPERIMENT - 9
CHARACTERISTICS OF MAGNETIC AMPLIFIERS
AIM:
1. To study series connected magnetic amplifier.
2. To study parallel connected magnetic amplifier.
3. to study saturated magnetic amplifier.
APPARATUS:
1. Magnetic amplifier trainer kit.
2. Latches.
CIRCUIT DIAGRAM:
1. SERIES CONNECTED
Fig 8.1. Series connected magnetic amplifier
A1
B1
33
2. PARALLEL CONNECTED
Fig 8.2. Parallel connected magnetic amplifier
34
3. SATURATED MAGNETIC AMPLIFIER
Fig 8.3.Self saturated magnetic amplifier
THEORY:
PROCEDURE:
SERIES CONNECTED MAGNETIC AMPLIFIER
The complete circuit diagram for conducting this experiment is built in the unit itself.
1. Keep slide switch in position ‘0’ which will be indicated by an indicator, after the
unit is switched ON.
2. Keep control current setting knob at its extreme left position which ensures zero
control current at starting.
35
3. With the help of plug in links, connect following terminals on the front panel of
the unit.
a) Connect Ac to A1
b) Connect B1 to A2
c) Connect B2 to L
4. Connect 100W fluorescent lamp in the holder provided for this purpose and
switch ON the unit.
5. Now gradually increase control current by rotating control current setting knob
clockwise in steps and note down control current and corresponding load current.
6. Plot the graph of load current Vs control current.
PARALLEL CONNECTED MAGNETIC AMPLIFIER
The procedure is same as for series connected magnetic amplifier but connections of
the terminals on the front panel of the unit are made as follows:
a) Connect Ac to A1
b) Connect A1 to A2
c) Connect B2 to L
d) Connect B1 to B2
SELF SATURATED AMPLIFIER
The procedure is same as explained above but switch is kept in position ‘E’ and the
terminals on the front panel of the unit are made as follows:
a) Connect Ac to C1
b) Connect A3 to B3
c) Connect B3 to L
36
TABULAR COLUMN
SERIES CONNECTED
S.NO Control Current IC(mA) Load Current IL(mA)
PARALLEL CONNECTED
S.NO Control Current IC(mA) Load Current IL(mA)
SATURATED MAGNETIC AMPLIFIER
S.NO Control Current IC(mA) Load Current IL(mA)
37
GRAPHS:
Fig: 8.4. Series Connected magnetic amplifier Fig: 8.5. Parallel Connected
Magnetic amplifier
Fig: 8.6.Saturated Magnetic amplifier
RESULT:
CONCLUSION:
Control Current Control Current
Control Current
38
Loa
d C
urre
nt
Loa
d C
urre
nt
Loa
d C
urre
nt
EXPERIMENT - 10
CHARACTERISTICS OF AC SERVOMOTOR
AIM:
To study the speed torque characteristics of AC servomotor.
APPARATUS:
1. Trainer kit
2. Multimeter
3. Connecting wires.
CIRCUIT DIAGRAM:
Fig: 9.1.AC Servomotor
Servo Amplifier
V
39
THEORY:
PROCEDURE:
1. Study all the controls carefully on the front panel.
2. Initially keep the load switch at OFF position, indicating that the armature circuit
of DC machine is not connected to auxiliary DC supply 12V dc. Keep servomotor
supply switch also at OFF position.
3. Ensure load potentiometer and control voltage autotransformer at minimum
position.
4. Now switch on main supply to the unit and also AC servomotor supply switch.
Vary the control voltage transformer. You can observe that the AC servomotor
will be indicated by the tachometer in the panel.
5. With load switch in OFF position, vary the speed of AC servomotor by moving
the control voltage and note down back emf generated by the DC machine(Now
working as a generator or tacho), Enter the results in the table.
6. Now with load switch at OFF position, switch ON AC servomotor and keep the
speed in the minimum position. You can observe that the AC servomotor starts
moving with speed being indicated by the tachometer. Now vary the control
winding voltage by varying the autotransformer and set the speed for maximum
speed. Now switch on the load switch and start loading AC servomotor by
varying the load potentiometer slowly. Note down the corresponding values of Ia
and speed-readings are entered. The control voltage is also noted.
40
TABULAR COLUMN:
No load Torque T=0, Ia = 0
S.NO VC(Volts) Eb (Volts) Speed ‘N’ rpm
VC = 150V
S.NO Eb(Volts) N(rpm) Ia(Amps) P = EbIa(Watts) Torque(Nm)
41
VC=220V
S.NO Eb(Volts) N(rpm) Ia(Amps) P = EbIa(Watts) Torque(Nm)
VC = 225V
S.NO Eb(Volts) N(rpm) Ia(Amps) P = EbIa(Watts) Torque(Nm)
42
GRAPHS:
Fig:9.2 Fig: 9.3.
Fig:9.4.
RESULT:
43
Tor
qu
e
Speed
X1/R1>X2/R2>X3/R3
x
y y
x
1
23
Sp
eed
Torque
Vc=225V
Vc=200V
Vc=175V
Vc=150V
Eb
Speed
CONCLUSION:
EXPERIMENT - 11
ROOT LOCUS, BODE PLOT FROM MATLAB
AIM: To analyze the stability of a system using a) Bode plot b)Root locus c)Nyquist plot
PROGRAM:
Using Bode plot:
num = input(‘enter the numerator of tf’);
den = input(‘enter the denominator of tf’);
sys= tf(num,den);
bode(sys);
[gm, pm, weg , wep]=margin(sys)
gmbd = 20 * log 10(gm)
if((pm>0)&(gmbd>0))
disp(‘the given system is stable’);
else
if((pm= =0)&(gmbd= =0))
disp(‘given system is marginally stable’);
else
disp(‘given system is unstable’);
end
end
Using Root locus:
num=input(‘enter the numerator of tf’);
den= input(‘enter the denominator of tf’);
sys= tf(num,den);
[r,k] = rlocus(sys);
44
rlocus(sys)
count=0
for i=1;length(k);
if real (r(i)>0)
count =count+1;
end
end
if count= =0
disp(‘system is stable’);
else
disp(‘system is unstable’);
end
Using Nyquist plot:
num=input(‘enter the numerator of tf’);
den= input(‘enter the denominator of tf’);
s= tf(num,den);
nyquist(num,den);
[gm,pm,def,pef]=margin(s)
if((gm>0)&(pm>0))
disp(‘system is stable’);
else
disp(‘system is unstable’);
end
OUTPUT:
CONCLUSION:
45
EXPERIMENT – 12
ON – OFF TEMPERATURE CONTROLLER
AIM: To study ON – OFF temperature Controller.
APPARATUS:
1. ON – OFF Temperature Controller Equipment
CIRCUIT DIAGRAM:
Fig: 12.1 Block Diagram of ON – OFF Temperature Controller
Heater
+ 12 V230 V
46
THEORY:
PROCEDURE:
1. Connect the RTO sensor PT – 100 to the binding post provided on the front panel.
2. Connect the heater cable on the rear side socket.
3. Keep rotary switch on the front panel in 00 degree position. And on the supply.
4. The D.P.M should indicate 0-0 degree centigrade.
5. When select switch is taken to 100 degree position DPM should indicate 100
degree centigrade. This completes calibration check and ensures that MIN and
MAX controls on the PCB are properly adjusted.
6. Keep the select switch in SET position and adjust SET TEMP.(p1)
pot to 560 c. Keep dead band pot to most counter clock wise position(MIN).
7. Take select switch to RTD position. Now you can observe that RTD temperature
goes on increasing and the controller keeps the temperature of the process around
the set point depending on dead band adjustment.
8. Take readings of the temperature at regular intervals of 10sec or 15sec and plot a
graph for temperature vs time readings.
9. You may adjust dead band to most clock wise position(MAX) and repeat the
process again.
10. If you keep a fan near process model, you may again take another set of readings
and observe oscillations in temperature.
47
TABULAR COLUMN:
Set temperature = 500
Minimum dead band:
S.NO. Time(Sec) Temperature(degrees)
Maximum dead band:
S.NO. Time(Sec) Temperature(degrees)
48
GRAPHS:
Fig: 12.2. Temperature Verses Time
RESULT:
CONCLUSION:
49
Time (sec) x
Tem
pera
ture
y