Lecture note 2

LECTURE NOTES
On
Electrical & Electronics Measurement
(PCEE4204)
3rd
Semester ETC Engineering
Prepared by,
Priyabrata Sethy
Prasanta Kumar Sahu
Ramachandra Dalei
INDIRA GANDHI INSTITUTE OF TECHNOLOGY,
SARANG

Module-1
Accuracy and precision are defined in terms of systematic and random errors.
The more common definition associates accuracy with systematic errors and
precision with random errors. Another definition, advanced by ISO,
associates trueness with systematic errors and precision with random errors,
and defines accuracy as the combination of both trueness and precision.
In the fields of science, engineering, industry, and statistics, the accuracy of
a measurement system is the degree of closeness of measurements of
a quantity to that quantity's actual (true) value.[1]
The precision of a
measurement system, related to reproducibility and repeatability, is the degree
to which repeated measurements under unchanged conditions show the
same results.[1][2]
Although the two words precision and accuracy can
be synonymous in colloquial use, they are deliberately contrasted in the
context of the scientific method.
A measurement system can be accurate but not precise, precise but not
accurate, neither, or both. For example, if anexperiment contains a systematic
error, then increasing the sample size generally increases precision but does
not improve accuracy. The result would be a consistent yet inaccurate string
of results from the flawed experiment. Eliminating the systematic error
improves accuracy but does not change precision.
A measurement system is considered valid if it is both accurate and precise.
Related terms include bias (non-random or directed effects caused by a factor
or factors unrelated to the independent variable) and error (random
variability).
The terminology is also applied to indirect measurements—that is, values
obtained by a computational procedure from observed data.
In addition to accuracy and precision, measurements may also have
a measurement resolution, which is the smallest change in the underlying
physical quantity that produces a response in the measurement.
In numerical analysis, accuracy is also the nearness of a calculation to the true
value; while precision is the resolution of the representation, typically defined
by the number of decimal or binary digits.
Accuracy is also used as a statistical measure of how well a binary
classification test correctly identifies or excludes a condition.
That is, the accuracy is the proportion of true results (both true
positives and true negatives) in the population. To make the context clear by
the semantics, it is often referred to as the "Rand Accuracy". It is a parameter
of the test.

On the other hand, precision or positive predictive value is defined as the
proportion of the true positives against all the positive results (both true
positives and false positives)
An accuracy of 100% means that the measured values are exactly the
same as the given values.
Also see Sensitivity and specificity.
Accuracy may be determined from Sensitivity and Specificity,
provided Prevalence is known, using the equation:
The accuracy paradox for predictive analytics states that
predictive models with a given level of accuracy may have
greater predictive power than models with higher accuracy. It may
be better to avoid the accuracy metric in favor of other metrics
such as precision and recall.[citation needed]
In situations where the
minority class is more important, F-measuremay be more
appropriate, especially in situations with very skewed class
imbalance.
Another useful performance measure is the balanced
accuracy which avoids inflated performance estimates on
imbalanced datasets. It is defined as the arithmetic mean of
sensitivity and specificity, or the average accuracy obtained on
either class:
If the classifier performs equally well on either class, this
term reduces to the conventional accuracy (i.e., the
number of correct predictions divided by the total number
of predictions). In contrast, if the conventional accuracy is
above chance only because the classifier takes advantage
of an imbalanced test set, then the balanced accuracy, as
appropriate, will drop to chance.[5]
A closely related
chance corrected measure is:
[6]
A direct approach to debiasing and renormalizing
Accuracy is Cohen's kappa, whilst Informedness has

been shown to be a Kappa-family debiased
renormalization of Recall.[7]
Informedness and Kappa
have the advantage that chance level is defined to be
0, and they have the form of a probability.
Informedness has the stronger property that it is the
probability that an informed decision is made (rather
than a guess), when positive. When negative this is
still true for the absolutely value of Informedness, but
the information has been used to force an incorrect
response
Error Analysis and Significant Figures
Errors using inadequate data are much less than those using no data at all.
C.
Babbage]
No measurement of a physical quantity can be entirely accurate. It is
important to know, therefore, just how much the measured value is likely to
deviate from the unknown, true, value of the quantity. The art of estimating
these deviations should probably be called uncertainty analysis, but for
historical reasons is referred to as error analysis. This document contains brief
discussions about how errors are reported, the kinds of errors that can occur,
how to estimate random errors, and how to carry error estimates into
calculated results. We are not, and will not be, concerned with the ―percent
error‖ exercises common in high school, where the student is content with
calculating the deviation from some allegedly authoritative number.
You might also be interested in our tutorial on using figures (Graphs).
Significant figures
Whenever you make a measurement, the number of meaningful digits that you
write down implies the error in the measurement. For example if you say that
the length of an object is 0.428 m, you imply an uncertainty of about 0.001 m.
To record this measurement as either 0.4 or 0.42819667 would imply that you
only know it to 0.1 m in the first case or to 0.00000001 m in the second. You
should only report as many significant figures as are consistent with the
estimated error. The quantity 0.428 m is said to have three significant figures,
that is, three digits that make sense in terms of the measurement. Notice that
this has nothing to do with the "number of decimal places". The same
measurement in centimeters would be 42.8 cm and still be a three significant
figure number. The accepted convention is that only one uncertain digit is to
be reported for a measurement. In the example if the estimated error is 0.02 m
you would report a result of 0.43 ± 0.02 m, not 0.428 ± 0.02 m.

Students frequently are confused about when to count a zero as a significant
figure. The rule is: If the zero has a non-zero digit anywhere to its left, then
the zero is significant, otherwise it is not. For example 5.00 has 3 significant
figures; the number 0.0005 has only one significant figure, and 1.0005 has 5
significant figures. A number like 300 is not well defined. Rather one should
write 3 x 102
, one significant figure, or 3.00 x 102
, 3 significant figures.
Absolute and relative errors
The absolute error in a measured quantity is the uncertainty in the quantity
and has the same units as the quantity itself. For example if you know a length
is 0.428 m ± 0.002 m, the 0.002 m is an absolute error. The relative error (also
called the fractional error) is obtained by dividing the absolute error in the
quantity by the quantity itself. The relative error is usually more significant
than the absolute error. For example a 1 mm error in the diameter of a skate
wheel is probably more serious than a 1 mm error in a truck tire. Note that
relative errors are dimensionless. When reporting relative errors it is usual to
multiply the fractional error by 100 and report it as a percentage.
Systematic errors
Systematic errors arise from a flaw in the measurement scheme which is
repeated each time a measurement is made. If you do the same thing wrong
each time you make the measurement, your measurement will differ
systematically (that is, in the same direction each time) from the correct result.
Some sources of systematic error are:
 Errors in the calibration of the measuring instruments.
 Incorrect measuring technique: For example, one might make an
incorrect scale reading because of parallax error.
 Bias of the experimenter. The experimenter might consistently read an
instrument incorrectly, or might let knowledge of the expected value
of a result influence the measurements.
It is clear that systematic errors do not average to zero if you average many
measurements. If a systematic error is discovered, a correction can be made to
the data for this error. If you measure a voltage with a meter that later turns
out to have a 0.2 V offset, you can correct the originally determined voltages
by this amount and eliminate the error. Although random errors can be
handled more or less routinely, there is no prescribed way to find systematic
errors. One must simply sit down and think about all of the possible sources of
error in a given measurement, and then do small experiments to see if these
sources are active. The goal of a good experiment is to reduce the systematic
errors to a value smaller than the random errors. For example a meter stick
should have been manufactured such that the millimeter markings are
positioned much more accurately than one millimeter. mistake or blunder - a

procedural error that should be avoided by careful attention [Taylor, 3]. These
are illegitimate errors and can generally be corrected by carefully repeating
the operations [Bevington, 2].
discrepancy - a significant difference between two measured values of the
same quantity [Taylor, 17; Bevington, 5]. (Neither of these references clearly
defines what is meant by a "significant difference," but the implication is that
the difference between the measured values is clearly greater than the
combined experimental uncertainty.)
relative error [VIM 3.12] - error of measurement divided by a true value of the
measurand [ISO, 34]. (Relative error is often reported as a percentage. The
relative or "percent error" could be 0% if the measured result happens to
coincide with the expected value, but such a statement suggests that somehow
a perfect measurement was made. Therefore, a statement of the uncertainty is
also necessary to properly convey the quality of the measurement.)
significant figures - all digits between and including the first non-zero digit
from the left, through the last digit [Bevington, 4]. (e.g. 0.05070 has 4
significant figures.)
decimal places � the number of digits to the right of the decimal point. (This
term is not explicitly defined in any of the examined references.)
standard error (standard deviation of the mean) � the sample standard
deviation divided by the square root of the number of data points: SE or SDM
= where is the sample variance [Taylor, 102].
(The ISO Guide and most statistics books use the letter s to represent the
sample standard deviation and s (sigma) to represent the standard deviation
of the population; however, s is commonly used in reference to the sample
standard deviation in error analysis discussions, i.e. x ± 2s )
margin of error - range of uncertainty. Public opinion polls generally
use margin of error to indicate a 95% confidence interval, corresponding to an
uncertainty range of x ± 2s [Taylor, 14].
coverage factor, k � numerical factor used as a multiplier of the combined
standard uncertainty in order to obtain an expanded uncertainty. Note: k is
typically in the range 2 to 3 [ISO, 3; Fluke 20-6].
(e.g. If the combined standard uncertainty is uc = 0.3 and a coverage factor
of k = 2 is used, then the expanded uncertainty is Uc = kuc = 0.6)

law of propagation of uncertainty - the uncertainty sz of a quantity z = f(w1, w2,
�, wN) that depends on N input quantities w1, w2, �, wN is found from
where si
2
is the variance of wi and rij is the correlation coefficient of the
covariance of wi and wj. If the input quantities are independent (as is often the
case), then the covariance is zero and the second term of the above equation
vanishes. The above equation is traditionally called the "general law of error
propagation," but this equation actually shows how the uncertainties (not the
errors) of the input quantities combine
Random errors
Random errors arise from the fluctuations that are most easily observed by
making multiple trials of a given measurement. For example, if you were to
measure the period of a pendulum many times with a stop watch, you would
find that your measurements were not always the same. The main source of
these fluctuations would probably be the difficulty of judging exactly when
the pendulum came to a given point in its motion, and in starting and stopping
the stop watch at the time that you judge. Since you would not get the same
value of the period each time that you try to measure it, your result is
obviously uncertain. There are several common sources of such random
uncertainties in the type of experiments that you are likely to perform:
 Uncontrollable fluctuations in initial conditions in the measurements.
Such fluctuations are the main reason why, no matter how skilled the
player, no individual can toss a basketball from the free throw line
through the hoop each and every time, guaranteed. Small variations in
launch conditions or air motion cause the trajectory to vary and the
ball misses the hoop.
 Limitations imposed by the precision of your measuring apparatus, and
the uncertainty in interpolating between the smallest divisions. The
precision simply means the smallest amount that can be measured
directly. A typical meter stick is subdivided into millimeters and its
precision is thus one millimeter.
 Lack of precise definition of the quantity being measured. The length
of a table in the laboratory is not well defined after it has suffered
years of use. You would find different lengths if you measured at
different points on the table. Another possibility is that the quantity
being measured also depends on an uncontrolled variable. (The
temperature of the object for example).

 Sometimes the quantity you measure is well defined but is subject to
inherent random fluctuations. Such fluctuations may be of a quantum
nature or arise from the fact that the values of the quantity being
measured are determined by the statistical behavior of a large number
of particles. Another example is AC noise causing the needle of a
voltmeter to fluctuate.
No matter what the source of the uncertainty, to be labeled "random" an
uncertainty must have the property that the fluctuations from some "true"
value are equally likely to be positive or negative. This fact gives us a key for
understanding what to do about random errors. You could make a large
number of measurements, and average the result. If the uncertainties are really
equally likely to be positive or negative, you would expect that the average of
a large number of measurements would be very near to the correct value of the
quantity measured, since positive and negative fluctuations would tend to
cancel each other
UNIT 1 STANDARD OF MEASUREMENT Measurements
Structure
1.1 Introduction
Objectives
1.2 Standards of Measurements and their Classification
1.2.1 Primary Standard
1.2.2 Secondary Standard
1.3 Standard Unit of Length
1.4 Standard Unit of Weight
1.5 Standard Unit of Time
1.6 Standard Unit of Temperature
1.7 Standard Units of Luminous Intensity of a Source of Light
1.8 Standard Unit of Amount of Substance
1.9 Standard Unit of Electrical Quantities
1.10 Summary

1.11 Key Words
1.12 Answers to SAQs
1.1 INTRODUCTION
In order that the investigators in different parts of the country and different
parts of
world may compare the results of their experiments on a consistent basis, it is
necessary
to establish certain standard units of length, weight, time, temperature and
electrical,
quantities. The National Bureau of Standards has the primary responsibility
for
maintaining these standard in the United States. In India, Indian Standard
Institute (ISI),
New Delhi has taken the responsibility for maintaining all the standard
measurements.
To monitor the standard of measurements, the same Institute issues
instructions to put
ISI mark on measuring instruments and items so that these may be compared
with
non-standard ones.
In the measurement system, the quantity to be measured, in the direct method,
is
compared directly against a standard of same kind of quantity. The magnitude
of
quantity being measured is expressed in terms of a chosen unit for the
standard and a
numerical multiplier. A length can be measured in terms of meter and a
numerical
constant. Thus, a 10 meter length means a length ten times greater than a
meter. Thus, by

the means of standard, it is possible to provide means of establishing and
maintaining the
magnitudes of the various units. The simplest kind of standard is a physical
object
having desired property. This standard can be used as a basis of comparison.
Objectives
After studying this unit, you should be able to
and the general validity of the experimental results.6
Metrology and
Instrumentation 1.2 STANDARDS OF MEASUREMENTS AND THEIR
CLASSIFICATION
The standards of measurements are very useful for calibration of measuring
instruments.
They help in minimizing the error in the measurement systems. On the basis
of the
accuracy of measurement the standards can be classified as primary standards
and
secondary standards.
1.2.1 Primary Standard
A primary standard quantity will have only one value and it is fixed. An
instrument
which is used to measure the value of primary standard quantity is called
primary

standard instrument. It gives the accurate value of the quantity being
measured. No precalibration
is required for this instrument. It is used to calibrate the instruments having
less accuracy. By comparing the readings of the two instruments, the accuracy
of the
second instrument can be determined.
1.2.2 Secondary Standard
The value of the secondary standard quantity is less accurate than primary
standard one.
It is obtained by comparing with primary standard. For measurement of a
quantity using
secondary standard instrument, pre-calibration is required. Without
calibration, the result
given by this instrument is meaningless. Calibration of a secondary standard is
made by
comparing the results with a primary standard instrument or with an
instrument having
high accuracy or with a known input source. In practical fields, secondary
standard
instruments and devices are widely used. Using calibration charts, the error in
the
measurement of these devices can be reduced.
1.3 STANDARD UNIT OF LENGTH
The meter is considered as one of the fundamental unit upon which, through
appropriate
conversion factors, the English system of length is based. The SI unit of
length in metre.
The standard metre is defined as the length of a platinum-iridium bar
maintained at very

accurate conditions at the International Bureau of Weights and Measures at
Sevres, near
Paris, France. All other metres had to be calibrated against the metre. The
conversion
factor for length for English and Metric systems in the United States is fixed
by law as
1 meter = 39.37 inches
Secondary standard of length is maintained at the National Bureau of
Standards for
calibration purposes. In 1960, the general conference on weights and measures
defined
the standard meter in terms of the wavelength of the orange-red light of a
krypton-86
lamp. The standard meter is thus
1 meter = 1,650,763.73 wavelengths of orange-red light of Krypton-86
In 1982, the definition of the meter was changed to the distance light travels in
1/299,792,458ths of a second. For the measurement, light from a helium-neon
laser
illuminates iodine which fluoresences at a highly stable frequency.
In CGS system, the fundamental unit of length is centimeter. Its conversion
factors for
other system are already mentioned above. The derived units for length are as
follows :
1 m = 100 cm
1 km = 105
cm = 1000 m
1 m
cm

1 decameter = 10 m
1 hectometer = 102 m.
We also have some other units, which are frequently used for short and large
lengths.7
Standard of
Measurements
They are :
1 Fermi = 1 f = 10– 15 m
1 Angstrom = 1
o
A
= 10– 10 m
1 light year
(distance that light travels in 1 year)
Note : Velocity of light is
8
1.4 STANDARD UNIT OF WEIGHT
The kilogram is considered as fundamental unit upon which, through
appropriate
conversion factors, the English system of mass is based. The SI unit of mass is
kilogram.

The standard kilogram is defined in terms of platinum-iridium mass
maintained at very
accurate conditions at the International Bureau of Weights and Measures in
Sevres,
France.
The conversion factors for the English and Metric systems in the United States
are fixed
by law is
1 pound-mass = 453.59237 grams
= 0.45359237 kilogram
Secondary standard of mass is maintained at the National Bureau of Standards
for
calibration purpose. In MKS and SI systems, fundamental unit of mass is
kilogram,
whereas in CGS system, the unit for the same is gram. The conversion factors
for the
above units and units derived from them are as follows :
1 kilogram = 1000 grams; 1 gram = 10– 3
kilogram
1 hectogram = 100 grams = 10– 1
kilogram
1 decagram = 10 grams = 10– 2
kilogram
1 milligram = 0.001 gram = 10– 6
kilogram
1.5 STANDARD UNIT OF TIME

The standard units of time are established in terms of known frequencies of
oscillation of
certain devices. One of the simpliest devices is a pendulum. A torsional
vibration system
may also be used as a standard of frequency. The torsional system is widely
used in
clocks and watches. Ordinary 50 HZ line voltage may be used as a frequency
standard
under certain circumstances. An electric clocks uses this frequency as a
standard because
it operates from a synchronous electric motor whose speed depend on line
frequency. A
turning fork is a suitable frequency source, as are piezo-electric crystals.
Electronic
oscillator may also be designed to serve as very precise frequency sources.
The SI unit of
time is second.
The fundamental unit of time, the second, has been defined in the past as
864001of a mean solar day. The solar day is measured as the time interval
between successive transits of the sun across a meridian of the earth. The time
interval varies with location of the earth and time of the year, however, the
mean solar day for one year is constant.The solar year is the time required for
the earth to make one revolution around the sun.The mean solar year is 365
days 5 hr 48 min 48 s.
1.6 STANDARD UNIT OF TEMPERATURE
An absolute temperature scale was proposed by Lord Kelvin in 1854 and
forms the basis for thermodynamic calculations. This absolute scale is so
defined that particular meaning is given to the second law of thermodynamics
when this temperature scale is used.
8 Metrology and Instrumentation
The International Practical Temperature Scale of 1968 furnishes an
experimental basis for a temperature scale which approximates as closely as

possible the absolute thermodynamic temperature scale. In the International
Scale, 11 primary points are
established as given in Table 1.1. Secondary fixed points are also established
as given in
Table 1.2. In addition to the fixed points, precise points are also established
for
interpolating between these points.
Table 1.1 : Primary Points for the International
Practical Temperature Scale of 1968
Point Normal Pressure = 14.6959 psia
Temperature
oC F
428.99
Normal boiling poin
Triple point of water 0.01 32.018
Normal boiling point of water 100 212.00
Normal freezing point of Zinc 419.58 787.24
Normal freezing point of silver 961.93 1763.47
Normal freezing point of gold 1064.43 1947.97

Table 1.2 : Secondary Fixed Points for the International Practical
Standard of Measurements
More recently, the International Temperature Scale of 1990 (ITS-90) has been
adopted. The fixed points for ITS-90 that are differ only slightly from IPTS-
68. For ITS-90, a platinum resistance thermometer is used for interpolation
between the triple point of hydrogen and the solid equilibrium for silver, while
above, the silver point black body radiation is used for interpolation.
Derived Units
The units of all other physical quantities can be expressed in terms of these
base units. For example, we can express the unit of speed in metre per second,
the unit of density in kilogram per cubic metre. Let us consider another
physical quantity like force. From Newton‘s second law of motion, force can
be defined as the product of mass and acceleration. We can therefore take the
unit of force as 1
. We call this by the name, Newton for convenience.The unit of energy is
Newton-metre. We call this by the name Joule. The unit of
power is Joule per second. We call it Watt.
The conversion factor for various units are
1 H.P = 746 watt (J/s)
1 H.P = 550 ft-1b/sec.
1 H.P = 75 kg-m/sec.
1.7 STANDARD UNIT OF LUMINOUS INTENSITY
OF A SOURCE OF LIGHT
Candela is the SI unit of luminous intensity of a source of light in a specified
direction.
The candela is the luminous intensity of a black body of surface area 1/60,000
m2
placed
at the temperature of freezing platinum and at a pressure of 101, 325 N/m2

, in the
direction perpendicular to its surface. Now candela is redefined as the
luminous intensity
in a given direction of a source that emits monochromatic radiation of
frequency
per
steradian. (SI unit of solid angle).
1.8 STANDARD UNIT OF AMOUNT OF SUBSTANCE
The mole (mol) is the SI unit of amount of substance.
One mole is the amount of substance of a system that contains as many
elementary
entities as there are atoms in 0.012 kg of carbon – 12.
1.9 STANDARD UNITS OF ELECTRICAL
QUANTITIES
The International conference on electrical units in London in 1908 confirmed
the
absolute system units adopted by the British Association Committee on
Electrical
Measurement in 1863. This conference decided to specify some material
standard which
can be produced in isolated laboratories and used as International standards.
The desired
properties of International standards are that they should have a definite value,
be
permanent, and be readily set up anywhere in the world, also that their
magnitude should
be within the range at which the most accurate measurements can be done.

The four units – ohm, ampere, volt and watt – established by above
specifications were
known as International units. The ohm and ampere are primary standards.
Definitions of
International unit are given below.10
Metrology and
Instrumentation
International Ohm
The international ohm is the resistance offered to the passage of an unvarying
electric current at the temperature of melting ice by a column of mercury of
uniform cross-section, 106.300 cm long and having mass of 14.4521 gm
(i.e., about 1 sq. mm in cross-section).
International Ampere
The international ampere is the unvarying current which when passed through
a
solution of silver nitrate in water deposits at the rate of 0.0001118 gm per
second.
The International Volt and Watt
The international volt and watt defined in terms of International ohm and
ampere.
As constructing standards, which did not vary appreciably with time, was
difficult
and also as, by 1930, it was clear that the absolute ohm and ampere could be
determined as accurately as the international units. The International
committee on
Weights and Measures decided in October, 1946 to abandon the international
units

and choose January 1, 1948 as the date for putting new units into effect. The
change was made at appropriate time and the absolute system of electrical
units is
now in use as the system on which electrical measurements are based.
SAQ 1
(a) Why are standards necessary?
(b) What is the difference between primary and secondary standards?
(c) The Universal gas constant has a value of 1545 ft-lbf/1bm-mol oR. By
applying appropriate conversion factors, obtain its value in SI unit.
(d) Mention the fundamental SI units which are used in mechanical system.
(e) What are the SI unit of the following :
(i) Temperature,
(ii) Current,
(iii) Luminous intensity of light, and
(iv) Amount of substance.
Kelvin double circuit for measurement of low resistances:
The Kelvin double bridge is the modification of the Wheatstone bridge and
provides greatly increased accuracy in measurement of low value resistance.
An understanding of the Kelvin bridge arrangement may be obtained by the
study of the difficulties that arise in a Wheatstone bridge on account of the
resistance of the leads and the contact resistances while measuring low valued
resistance.
The Kelvin double bridge incorporates the idea of a second set of ratio arms-
hence the name double bridge-and the use of four terminal resistors for the
low resistance arms.
Figure shows the schematic diagram of the Kelvin bridge. The first of ratio
arms is P and Q. the second set of ratio arms, p and q is used to connect the
galvanometer to a point d at the appropriate potential between points m and n
to eliminate effect of connecting lead of resistance r between the unknown
resistance, R, and the standard resistance, S.

The ratio p/q is made equal to P/Q. under balance conditions there is no
current through the galvanometer, which means that the voltage drop between
a and b, Eab is equal to the voltage drop Eamd.
kelvin double bridge
Now the voltage drop between a and b is given by,

Above equation is the usual working equation for the Kelvin Bridge. It
indicates that the resistance of connecting lead, r, has no effect on the
measurement, provided that the two sets of ratio arms have equal ratio. The
former equation is useful, however, as it shows the error that is introduced in
case the ratios are not exactly equal. It indicates that it is desirable to keep r as
small as possible in order to minimize the errors in case there is a difference
between ratios P/Q and p/q.
solution:
Methods of measuring low, medium and high resistances
Classification of resistances:
Low resistance:
Resistance of the order of 1ohm and under.
Medium resistance:
1ohm to 100 Kilo ohm or 0.1Mohm.
High resistance:
100 k ohm and above.
Low resistance
Introduction:
For low resistance, the contact resistance of 0.002 Ω also causes an error.
Therefore, during measurement, the contact resistance should either be
eliminated by some means or taken into account.
Construction:
Consists of four terminals:

(i) One pair of terminals c1c2 called current terminals, is used
to lead current to and from the resistor.
(ii) Other pair p1p2 between which voltage drop is measured is
called potential terminals.
Results:
 Resistors of low values are measured in terms of resistance between
potential terminals.
 It is independent of contact drop.
Methods of measuring low resistance:
(i) ammeter voltmeter method
(ii) Kelvin double bridge method
(iii) Potentiometer method
Ammeter voltmeter method
This is very popular method as instruments required for test are usually
available in the laboratory.
Connection:
Explanation:
 Voltmeter measures true value of voltage
 Ammeter reads sum of currents through resistance and voltmeter
Let Rv =resistance of voltmeter
Iv =current through the voltmeter = V / Rv
Measured value of resistance = Rm =V/I =V / ( Ir+Iv )
=V / (V/R +V/ Rv ) =R / ( 1+ R/Rv )

True value of resoisstance = R= Rm (1+R/Rv)
Or, R=Rm ( Rv + R)/ Rv
Or, R.Rv = RmRv + Rm R
Or, R (Rv-Rm)=RmRv
Or, R= RmRv / (Rv-Rm)
Or, R = Rm[ 1/ (1-Rm/Rv) ]
R=Rm ( 1+ Rm / Rv) (1)
Thus from above eqn. we can say that measured value is much smaller than
the true value.
Again, when Rv » Rm
Then, Rm / Rv is very small, so neglected.
Now from eqn. (i) above, under such condition, R=Rm.
i.e. true value =measured value.
In other words,
The true value of resistance is equal to measured value only if the resistance
of voltmeter Rv is infinite.
From eqn (1)
R=Rm( 1+ Rm/Rv)
Or, Rm- R = - Rm 2
/Rv
Relative error, ε r =(Rm-R)/ R =- Rm 2
/ (Rv R)
Since, Rm ≈ R
Therefore, ε r =- Rm 2
/ (Rv R) =- R/ Rv
i.e. error is very small if value of resistance is very small compared to
resistance of voltmeter.
Advantage: easy and simple method.
Disadvantage: (i) not accurate
(ii) use confined to laboratory work.

Kelvin double bridge method
Purpose: measures low resistance.
Principle:
It is a modification of Wheatstone bridge taking into account the resistance of
leads and contact resistance while measuring low resistance.
Diagram:
Theory:
 When galvanometer is connected to m, the resistance r is connected to
S. indicating low resistance.
 When connected to n, then r is added to R, resulting too high a value
for R.
 Suppose point c is selected ,which will not give any high or plow
value, such that
r1 / r2 =P/Q (1)
Then the presence of r1 causes no error in the result. Then we have,
R+ r1 = P (S+ r2) /Q (2)
From (1), r1 / r2 =P/Q
or, r1 /( r1 + r2) =P/(P+Q)
or, r1= P[ r1 + r2 ] / (P+Q) = P r / (P+Q)
and r2 = Q r /(P+Q)

Now, from (2)
R+ r1 =P(S+ r2 ) /Q
or, R+Pr / (P+Q) =P[ S+Qr / (P+Q)] / Q
or, R+Pr /(P+Q) = PS /Q + Pr / (P+Q)
or, R= PS/Q
i.e. making the galvanometer connection at c, the resistance of leads does
not affect the result.
Practically Kelvin double bridge
It is difficult to find out correct connecting point i.e. c. To overcome this
difficulty, it is compensated by connecting two actual resistance units of
correct ratio between m and n. The galvanometer is connected to junction of
resistors.
This bridge incorporates second set of rated arms. Hence named
double bridge.
Diagram:

Construction:
 First ration arm is P and Q.
 Second ratio arm p and q is used to connect the galvanometer to a
point c at appropriate potential between points m and n to eliminate
the effect of connecting lead of resistance r4 between R and standard
resistance S.
 p/q is made equal to P/Q.
Derivation:
At balance point,
Ead = Eamc (1)
Now,
Ead + P. Eab / [P+Q]
Eab = I [ R+S+ (p+q)r / (p+q+r) ]
Eamc = I [ R+ px (p+q)r / (p+q)(p+q+r) ]
From (1)
Px Eab / (P+Q) = I [ R+ px (p+q)r / (p+q)(p+q+r) ]
Or, Px I [ R+S+ (p+q)r / (p+q+r) ] / (P+Q) = I [ R+ px (p+q)r / (p+q)(p+q+r) ]
Or, R [ 1- P/(P+Q)]= PS/(P+Q) + [ P/(P+Q) – p/(p+q)]x (p+q)r/ (p+q+r)
Or, R. Q / (P+Q) = PS/(P+Q) + [ P/(P+Q) – p/(p+q)]x (p+q)r/ (p+q+r)
Dividing both sides by Q /(P+Q),we get
R= PS/Q + (P+Q)x [ P/(P+Q) – p/(p+q)]x (p+q)r/ (p+q+r)
Q
Let second term on the right side of the above eqn =0
Under such condition, we will get R=PS/Q which is same as Wheatstone
bridge eqn.
However when second term on right side of eqn is made equal to zero, we get
P/(P+Q) =p/(p+q)
Or, (p+q)/p = (P+Q)/P

Or, q/p =Q/P
Or, P/Q=p/q
It means the resistance of connected leads r has no effect on the measurement
provided that the two sets of ration arms have equal ratio.
Shortcomings:
(1) Error is introduced in case ratios are not exactly equal.
Remedy:-keep r as small as possible.
(2) Effect of thermo electric emf.
Remedy: True value R is taken as mean of two readings. Second reading is
taken by reversing battery connection.
Medium resistance
Methods:
(1) Ammeter voltmeter
(2) Substitution
(3) Wheatstone bridge
(4) Ohmmeter
Ammeter voltmeter method
In this method ammeter reads the true value of the current through the
resistance but voltmeter odes not measure the true voltage across the
resistance.
Voltmeter reads sum of voltage across ammeter and resistance
Ra=resistance of ammeter
Rm= measured value
Diagram:
Derivation:
Now, Rm =V/I =(Va+VR) / I = Va / I + VR/ I =Ra +R

True value of resistance, R =Rm -Ra =Rm - Rm. Ra / Rm
=Rm (1-Ra/Rm)
Or, Rm = R +Ra
Thus measured value is higher than true value.
True value is equal to measured value only if the ammeter resistance Ra is
zero.
Relative error, ε r = (Rm-R) / R =Ra/R
If the value of resistance under measurement is large as compared to
internal resistance of ammeter, the error in measurement would be small.
Advantage:
Easy, simple, rough method.
Disadvantage:
 At full scale error may be around 0-1%.
 Errors sometimes considerably high.
Substitution method
Diagram:
A --- Ammeter
r---regulating resistance
S---standard variable resistance
R--- Unknown resistance
S/W ---switch for putting R and S alternatively into circuit.

Procedure:
Case 1: Resistance R in the circuit .
 S/W is set to position 1.
 This brings R into the circuit.
 r is adjusted to give ammeter the chosen scale mark.
Case 2: Resistance S in the circuit.
 Change S/W to position 2.
 This brings S in to the circuit.
 Adjust S to give same chosen scale mark by ammeter.
 The substitution for one resistance by another has left current
unaltered.
 The value of S gives the value of R.
Advantage:
 More accurate than ammeter voltmeter method as no error as the
case of ammeter voltmeter method.
 Many applications in bridge method.
 Used in high frequency ac measurement.
Disadvantage:
 Accuracy depends upon constancy of battery emf and resistance of
circuit( excluding R & S)
 Also depends upon accuracy of measurement of S.
Wheatstone bridge
Purpose: It is an important device tomeasure medium resistance.
Construction:
 Consists of four arms , asource of emf and a null detector( usually a
galvanometer)
 Pand Q fixed resistances.
 S is a variable (standard ) resistance.
 R is an unknown resistance.

Diagram:
Derivation:
When bridge is balanced-
 No current through galvanometer
 Potential at d is equal to potential at c.
i.e. I1P= I2 R (1)
Again I1=I3= E/ (P+Q) (2)
As no current flows through galvanometer
And I2=I4=E/(R+S) (3)
Putting the value of I1 and I2 from eqn (2) & (3) into eqn (1), we get
E x P/ (P+Q) = E x R/(R+S)
Or, (P+Q)/P=(R+S)/S
Or, 1+Q/P =1+S/R
Or, R/S=P/Q
Or, R=PS/Q

Sensitivity:
When the bridge is unbalanced, it is desired to know the galvanometer
response. This is achieved by
1. With a specified bridge arrangement, under given unbalance, the
galvanometer which shows deflection is selected.
2. Determining the minimum unbalance which can be observed with a
given galvanometer.
3. Determining deflection for given unbalance.
Derivation:
Suppose r is changed to R+∆R, creating an unbalance. With galvanometer
branch open-
Ead=I1 P =EP/(P+Q)
Similarly, Eac=I2(R+∆R) =E(R+∆R) / (R+∆R+S)
P.D between points c and d is
e= Eac – Ead
= E [ (R+∆R)/( R+∆R+S) – P/ (P+Q)]
Since P/(P+Q) = R/(R+S)
We have,
e= E[ (R+∆R)/( R+∆R+S) – R/ (R+S)]
= ER. [(1+∆R/R)/( 1+∆R ) – 1]
(R+S) (R+S)
= ER. [(1+∆R/R)( 1- ∆R ) – 1]
(R+S) (R+S)
Neglecting square terms of increment i.e. ∆R2
e= ER. [1- ∆R + ∆R -∆R2
– 1]
(R+S) (R+S) R R(R+S)
=ER. [ ∆R - ∆R2
]
(R+S) R (R+S)
= ER. x ∆R [ ∆R x (R+S) 1]

(R+S) (R+S) R ∆R
= ER. x ∆R [ (R+S) 1]
(R+S) (R+S) R
= ER. x ∆R x S
(R+S) 2
R
= E ∆R S
(R+S) 2
Deflection of galvanometer,
θ= e. Sv
Where Sv is the voltage sensitivity of galvanometer
θ= e. Sv = Sv . E ∆R S / ∆R/R
(R+S) 2
= E Sv S
(R+S) 2
/ R
= E Sv
(R+S) 2
/ R S
= E Sv
(R/S+2+ S/R)
Thus sensitivity is maximum when R/S=1
Sensitivity decreases if ration is greater or smaller than unity.
Limitations:
 Use is limited to the measurement of resistances ranging from a few
ohms to several mega ohms.
 When high resistance is required to measured ,sensitivity decreases
 Upper limit is extended by increasing emf applied.
 Care to be taken to avoid overheating.
 Inaccuracy arises during measurement of high resistance.
Remedy:
 For high resistance, use mega Ohm Bridge.

 For lower resistance measurement, resistance of connecting leads and
contact resistance comes into account
 Lower limit is 1 to 5 ohm.
 For further lower resistance, Kelvin double bridge is suitable.
Ohm meter
Diagram:
Procedure:
 Terminals A and B are shorted together
 Maximum current is adjusted by Rsh to flow through meter which
depends upon Rx.
 This corresponds to zero resistance.
 The terminals are left open. No current flows through the circuit.
Therefore no movement of pointer. This corresponds to maximum
resistance (infinity).
 Based on this, the instrument is calibrated to indicate the resistance.
Types:
Series type ohmmeter
Shunt type ohmmeter
Cross-coil ohmmeter
Advantage: simple, convenient, and fast method.
Disadvantage: accuracy is of low order.

High resistance
Methods:
 Direct deflection method
 Loss of charge method
 Mega ohm bridge
 Megger
Direct deflection method
Purpose: measurement of high resistance such as insulation resistance of
cables.
Diagram:
Explanation:
 Galvanometer G measures current Ir between the conductor and metal
sheath.
 Leakage current Il over the insulating material is carried by guard wire
wound on the insulation
 Cables without metal sheaths can be tested in a similar way by
immersing the cable ends, on which connection are made, in water in a
tank.
 The water and tank then form the return path for the current.
Insulation resistance of cable, R=V/ IR

Requirements:
 A high voltage source500V emf is required.
 A protective series resistance is included
 Galvanometer is short circuited to avoid existence of charging and
absorption current.
 The value of protective resistance is subtracted to get true value.
Loss of charge method
Diagram:
Construction:
 R, an unknown resistance is connected in parallel with a capacitor C
and electrostatic voltmeter.
 A battery with emf V in parallel with R and C.
Operation:
 Capacitor is charged to suitable voltage by battery.
 Then allowed to discharge through resistance.
 Terminal voltage is observed over a considerable period of time during
discharge.
 After application of voltage, Voltage across capacitor at any instant ‗t‘
v =Ve (- t / CR )

or, V/v = e t / CR
or, loge V/v = t / CR
or, R= t / [ C loge V/v ]
= 0.4343 t / [C log10 V/v]
Results:
 If R is very large, time for appreciable fall in voltage is very large.
 Care is to be taken while measuring V and v i.e. voltage at beginning
and end of time ‗t‘
 Error in V/v
 Better results by change in voltage (V-v) directly and calculating R as
R=0.4343 t / [C log10 V/(V-e)]
Where, V-v=e
 This method is applicable to high resistance.
 It requires capacitor of high leakage resistance.
Shortcomings:
 True value of R is not measured as Rv , voltmeter resistance and
leakage resistance of capacitor considered to be infinite.
Correction:
Two resistances are taken into account.
 First if R‘----equivalent resistance of R1 and R
Then discharge eqn gives
R‘=0.4343 t / [ C log10 V/v ] (1)

 Secondly test is repeated with R disconnected, capacitor discharge
through R1,.
 R1 is obtained from here is substituted in eqn (1) which gives
RR1 = 0.4343 t / [ C log10 V/v ]
R+R1
Mega ohm bridge
Introduction:
During measurement of high resistance, the leakage comes into effect over
and around the specimen being measured.
The effect of leakage paths is removed by some form of guard circuit.
Concept of guard circuit:

Diagram of mega ohm bridge:
Sensitive null indicating arrangement
Construction:
 Fixed resistance P
 Guard circuit AGB
 Variable resistance Q
 Standard adjustable resistance S
 Amplifier

 Deflection type voltmeter
Explanation:
The bridge is shown in the fig. The unknown resistance is connected across
terminals AB with proper guard circuit arrangement.
When the unknown resistance is equal to the standard resistance S, the output
given to the amplifier is zero and so the voltmeter which is a null type
voltmeter would not deflect. Thus the standard resistance S value is equal to
the unknown resistance. The adjustment is done with the help of S.

Megger
Purpose: Measures high resistance (insulation resistance)
Construction:
 Hand cranked generator G which generates voltage of 500V,1000V,
2500V.
 A centrifugal clutch is incorporated which slips at predetermined
speed so that a constant voltage is applied to insulation under test.
 Current coli similar to PMMMC
 Voltage coil V1, V2.
 Permanent magnet
Diagram:
Explanation:
 When pointer is at ∞ position, voltage coil can exert very little torque.
 Current coil is parallel to PMMC instrument
 Torque exerted by voltage coil increases as it moves into stronger
field.
 When maximum, pointer is at zero.
 Current in current coil is very large, scale is at zero.
 At ∞, current is very weak.
 Voltage range can be controlled by a voltage selector switch.

AC bridges
The ac bridge is a natural out growth of the Wheatstone bridge. The four arms
is impedance. The battery and galvanometer are replaced by an ac source and
a detector sensitive to small alternating potential difference.
Detectors commonly used are:-
Head phones
Vibration galvanometer
Tunable amplifies detector.
Headphones widely used as detectors at frequency of 250 Hz and above up to
3 or 4kHz.
Vibration galvanometer at frequency 5 Hz to 1000 Hz .commonly used below
200 Hz.
General form of AC bridge:-
R1, R2, R3, R4 are non inductive resistances.
L1, L2 are non resistive inductance.
At balance,
Z1Z4=Z2Z3
Or, (R1+jωL1) R4 = (R2 + jωL2) R3
Or, R1R4+ jωL1R4 = R2R3 + jωL2R3
Equating real and imaginary parts,
We get,
R1R4=R2R3
or, R1=R3R2 /R4
And jωL1R4= jωL2R3

Or, L1= R3L2/R4
Thus if L1, R1 are unknown, the above bridge may be used to measure these
quantities in terns of R2, R3, R4 and L2.
Conclusion:
 For balance in ac bridge, both magnitude and phase relationship must
be satisfied. This requires that real and imaginary terms must be
separated which gives two equations which is to be satisfied for
balance.
 If abridge is balanced for fundamental frequency, it must be balanced
for any harmonics.
Measurement of self inductance
Methods:
 Maxwell‘s inductance bridge
 Maxwell‘s inductance capacitance bridge
 Hay bridge
 Anderson‘s bridge
 Owen bridge
Maxwell‘s inductance bridge
Purpose: It measures unknown inductance by comparing with a variable
standard self inductance.
Connection Diagram:
L1 ---- unknown inductance of resistance R1

L2 ---- variable inductance of fixed resistance r2
R2 ---- variable resistance connected in series with inductor L2.
R3, R4 ----- known non inductive resistances.
Phasor diagram:
Balance equation:
At balance:
(R1+jωL1)R4 = R3 [ (R2+r2) + jωL2]
Or, R1R4 + jωL1R4= R3( R2+r2) + jωL2R3
Or, R1= R3 (R2+r2)/ R4
And L1= R3L2/R4
Note: In some cases an additional known resistance may have to be inserted in
series with unknown coil in order to obtain balance.
]
Maxwell‘s inductance capacitance bridge

Purpose: In this bridge, inductance is measured by comparison with a standard
variable capacitance.
Connection Diagram:
L1=unknown inductance
R1=effective resistance of inductor L1
R2,R3, R4= known non-inductive resistance
C4=variable standard capacitor.
Phasor diagram:

Balance equation: at the point of balance:
(R1+ jωL1) [ R4 / ( 1+ jωC4R4) = R2R3
Or, R1R4 + jωL1R4= R2R3 + jωR2R3R4C4
R1R4=R2R3
Or, R1 = R2R3/ R4
And L1R4= R2R3R4C4
Or, L1 = R2R3C4
And Q factor = ωL1/ R1 = ωR2R3C4/ R1
= ωR2R3C4 = ωR4C4
R2R3
R4
Q factor = ωR4C4
Advantage:
 Balance equations are independent if C4 and R4 are variable.
 Frequency does not effect the calculation of unknown variable.
 Simple expressions for unknown L1 and R1 in terms of known bridge
elements.
 Maxwell‘s inductance-capacitance bridge is very useful for
measurement of wide range of inductance at power and audio
frequency.
Disadvantage:

 Variable capacitor is expensive and less accurate. So fixed capacitor is
sometimes used. In that case balance adjustments are done by-
1. Varying R2 and R4, which is difficult.
2. Putting an additional resistance in series with inductance
under measurement and varying this resistance and R4.
 Limited to measurement of low Q coil (1< Q< 10) also unsuitable for
very low Q (Q<1)
Note: Maxwell‘s bridge is suitable for measurement of only medium Q coils.
Hay Bridge
 It is modification of Maxwell‘s bridge
 Uses resistance in series with standard capacitor.
Connection Diagram:
L1= unknown inductance having a resistance R1
R2, R3, R4 = known non-inductive resistances.
C4=standard capacitor.

Phasor diagram:
Balance equaton:
(R1+ jωL1)(R4- j/ ωC4) = R2R3
Or, R1R4 +L1 + jωL1R4 – jR1/ωC4 = R2R3
Separating real and imaginary parts,
R1R4 +L1/C4 =R2R3 (1)
And L1=R1/ ω2
R4C4 (2)
Solving the equations (1) &(2),
We get,
L1=R2R3C4 / [ 1+ ω2
R4
2
C4
2
]
And R1= ω2
R2R3 R4 C4
2
/ [1+ ω2
R4
2
C4
2
]
Q factor of coil, Q= ωL1/ R!= 1/ ωC4R4
Results:
The expression for inductance and capacitance contains frequency terms. So
frequency should be known accurately.
Now,
L1=R2R3C4 / [1+ ω2
R4
2
C4
2
]
But, Q= 1/ ωC4R4
Therefore,
L1= R2R3C4/ [1+ (1/Q) 2
]
So for Q> 10, the term (1/Q)2
< 100. Which is neglected.
Therefore, this method is suitable for Q > 10 or higher. Under such cases,
L1=R2R3C4.

Advantages:
 Simple expression for inductance of Q>10 and higher.
 Simple expression for Q factor.
 This bridge requires low value resistor for R4 as Q=1/ ωC4R4 for
higher Q., R4 is smaller.
Disadvantage:
Not suitable for measurement of coils having Q < 10.
Anderson‘s bridge
 Modification of Maxwell‘s inductance-capacitance bridge
 Inductance measured in terms of a standard capacitance.
 Applicable for precise measurement of self inductance.
Connection Diagram:
L1=self inductance to be measured
R1=resistance of self inductance
r1= resistance in series with L1
r, R2,R3,R4=known non-inductive resistances

c=fixed –standard capacitor
Phasor diagram:
Balance equation:
At balance, I1=I3 and I2=I4+Ic
Now, I1R3=Icx 1/ jωC
Or, Ic = I1 jωCR3 (1)
Balance equations are,
I1 (R1+r1+ jωL1) =I2R2+Icr (2)
And Ic (r+1/ jωC) = (I2—Ic) R4 (3)
Putting the value of Ic from (1) in (2) and (3), we get,
I1R1+I1r1+ jωI1L1=I2R2 + jωCI1R3r (4)
And jωCI1R3 r + I1R3 = I2R4 – jωC I1R3R4 (5)
From (4),
I1 (R1+r1+ jωL1 – jωC R3 r) = R2I2 ------------------- (6)
And I1 (jωC R3 r +R3 + jωCR3R4) = R4I2 -------------(7)
Dividing (6) by (7), we get
R1+r1+ jωL1 – jωC R3 r = R2
jωC R3 r +R3 + jωCR3R4 R4
Or, R4 ( R1 + r1) + j ω R4(L1 --- CR3 r ) = R2 R3 + jω C R2 ( R3 r +R3R4)
equating real and imaginary parts,

R4 (R1+r1) = R2R3
Or, R1= R2R3 – R4r1 = R2R3 --- r1
R4 R4
Or, R1 = R2R3 --- r1
R4
Also, j ω R4 (L1 --- CR3 r ) = jω C R2 ( R3 r +R3R4)
Or, R4L1 --- CR3R4r = CR2R3r +C R2R3R4
Or, L1 = CR3R4r + CR2R3r + CR2R3
R4 R4
= C R3 [ R4 r + R2 r +R2R4 ]
R4
Therefore, L1 = C R3 [ R4 r + R2 r +R2R4 ]
R4
Conclusion:
From the eqn of 1 and L1, it is clear that adjustment of r1 and r should be
done to obtain easy convergence.
Advantage:
 By manipulation of r1 and r ,they become independent and easier to
obtain balance for low Q coil than Maxwell‘s bridge.
 Fixed capacitor I used.
 Also useful for accurate measurement of capacitance in terms of
inductance.
Disadvantage:
 More complex, manipulation and circuits.
 Additional junction point increases difficulty of shielding the bridge.
Owen‘s bridge
Purpose: measures inductance in terms of capacitance.
Connection Diagram:

L1=unknown self-inductance of resistance R1
R2=variable non inductive resistance
R3=fixed non-inductive resistance
C2=variable standard capacitor
C4=fixed standard capacitor.
Phasor diagram:
Balance equation:
At balance,
(R1 + jωL1) (1/ jωC4) = (R2 + 1 / jωC2 ) R3
Or, -- jR1/ ωC4 + L1/ C4 = R2R3 – j R3 / ωC2
L1/ C4 = R2R3
Or, L1= C4R2R3
And,

R1/ ωC4 = R3 / ωC2
Or, R1 = R3C4/ C2
Advantage:
 Convergence to balance condition is much easier as R2 and C2 the
variable elements are in same form.
 Balance equations are simple and do not contain any frequency
component
 Used over a wide range of measurement of inductance.
Disadvantage:
 Requires a variable capacitor which is expensive
 When Q is high, C2 tends to become rather large.
Measurement of capacitance
Methods:
De Sauty‘s bridge
Schering Bridge
De Sauty ‗s bridge
Principle: Based on comparing two capacitors
Connection Diagram:

C1= capacitor to be measured
C2=A standard capacitor
R3, R4=non-inductive resistors
At balance,
(1/ ωC1) x R4 = (1/ ωC2)x R3
Or, C1=C2 x R4 /R3
The balance is obtained by varying either R3 or R4.
Advantage:
Simple and easy method.
Disadvantage:
 It is impossible to obtain balance if both the capacitors are not free
from dielectric loss.
Use: suitable for air capacitor only.
Remedy: to overcome the problem with dielectric loss , the bridge is
modified.
Modified De Sauty‘s bridge
Connection Diagram:

 R1, R2 are connected in series with C1 and C2 respectively.
 r1, r2 are small resistance representing loss component of the
capacitor.
Phasor diagram:
Balance equation;
(R1+r1+1/ jωC1 ) R4 = (R2 +r2+1/ jωC2) R3
Or, (R1+r1)R4 – j R4/ ωC1 = (R2+r2)R3 – jR3/ ωC2
(R1+r1)R4=(R2+r2)R3-----------(1)
And R4/ ωC1 = R3/ ωC2
Or, C1/C2=R4/R3-----------(2)

Again from (1),
R4/R3 =R2+r2 -------------(3)
R1+r1
From (1) ,(2),(3),
C1/C2 = R4 /R3 = R2+r2 -------------(4)
R1+r1
Balance is obtained by varying R1,R2,R3,R4.
δ1 ----- phase angle of C1
δ2 ------ phase angle of C2
Dissipation factor for C1=D1=tan δ1= ωC1r1 ------------(5)
Dissipation factor for C2 = D2= tan δ1= ωC2r2 ----------(6)
From (4),
C1/C2 = R2+r2
R1+r1
Or, C2R2 +C2r2 =C1R1 +C1r1
Or, C2r2 – C1r1 = C1R1 – C2R2
Or, ωC2r2 – ωC1r1 = ω( C1R1 -- C2R2)
Or, D2 – D1 = ω ( C1R1 -- C2R2 )
Again,
C1/C2 = R4/R3
Therefore, D2 – D1 = ω [ C2 .R4. R1 -- C2R2 ]
R3
= ω C2 [ R4. R1 -- R2 ] ---------- (7)
R3
From, (7)
if dissipation factor of one of the capacitor is known, dissipation factor of
other can be determined.

Results: does not give accurate results i.e. dissipation factor.
Schering bridge
Connection Diagram:
C1=capacitor to be measured.
R1=a series resistance representing loss in C1.
C2= a standard capacitor. It is an air or gas capacitor and hence loss
free.
R3 = a non –inductive resistance.
C4=a variable capacitor.
R4= a variable non non inductive resistance in parallel with C4.
Phasor diagram:
Balance equation:

(R1+1/jωC1 ) [ R4 ] = 1x R3/ j ωC2
(1+ j ωC4R4 )
Or, (r1+ 1/j ωC1 ) . R4 = R3 [ 1+j ωC4R4 ]
j ωC2
or, r1 R4 – j x R4 / ωC1 = -- j x R3 / ωC2 + R3R4C4
C2
r1R4 = R3R4C4
C2
Or, r1 = C4R3/ C2
And R4/C1 = R3 / C2
Or, C1 =C2 R4 / R3
Dissipation factor, D1 = tanδ= ωC1 r1 = ω . R4.C2. C4.R3
R3 C2
Or, D1 = ωC4 R4
Balancing is done by adjustment of R2 and C4 with C2,R4 fixed.
Advantage:
 As C1=R4C2/R3 and C2, R4 fixed. The dial of R3 may be
calibrated to read capacitor directly.
 In case fixed of frequency fixed, dial of capacitor C4 can be
calibrated to read dissipation factor directly as D1= ωC4R4
Disadvantage:
Difficulty in obtaining balance as R3 appears in both equations.

Q meter
 It is an instrument which is designed to measure the value of Q
directly. Therefore it can measure the characteristic of coils and
capacitors.
Principle of working:
It is based on principle of resonant R,L ,C series circuit.
At resonant frequency fo ,
X c = X L , ----------- (1)
X c =1/ 2πfoc=1/ ωo c
X L = 2π fo c = ωo L
From (1),

1/ ωo c = ωo L
Or, ωo
2
= 1/ LC
Or, fo =
1
2 LC
And Io = E/R
Voltage across capacitor, Ec=IoXc=IoXL=Io ωo L
Input voltage, E=IoR
Therefore, Ec/E= Io ωo L/ IoR = ωo L/R =Q.
Ec =Q E
Thus the input voltage E is magnified by Q times and appears across the
capacitor. A voltmeter connected across the capacitor can be calibrated to read
the value of Q directly.
Practical circuit:
Rsh --- low value shunt resistor.
V1--- thermocouple voltmeter
V2--- electronic voltmeter
T1, T2---terminal across which coil is connected.
C---tuning capacitor.
T3, T4--- terminal across which tuning capacitor is connectd.
Cd—distributed capacitor.

Construction:
The practical circuit consists of a self contained variable frequency RF
oscillator. This oscillator injects voltage E into the circuit through small
resistance Rsh. Voltmeter V1 reads injected voltage. The injected voltage is
magnified across capacitor c. this magnified voltage is read by V2.
Therefore, Ec=QE
The voltmeter V2 is calibrated to read Q directly.
Application:
(1) Measurement of Q:
The voltage V2 across capacitor is given by V2=QV1. The voltmeter
across capacitor is calibrated to read Q directly.
This Q represents Q of entire circuit. So error exists.
Cause:
 On account of shunt resistance.
 Due to distributed capacitance of the circuit.

Correction for shunt resistance:
Q measured = ωo L
R+ Rsh
Qtrue = ωo L/R = Qmeasured (R+Rsh)
R
=Qmeasured ( 1+ Rsh/R )
Therefore,
Qmeasured = Qtrue = Q true ( 1—Rsh/R )
1+ Rsh/R
Therefore measured value of Q is smaller than true value.
Results:
For low Q coils (high resistance)--- Rsh/R is negligible
Q measured =Q true.
For high Q coils (low resistance)—
Error caused may be serious.
Correction for distributed capacitance:

It can be shown,
Q true = Q measured (1+Cd / C)
Thus measured value of Q is less than true value.
(2) Measurement of inductance:
We know,
fo = 1/ 2π LC
or,LC= 2 2
1
4 fo
or, L= 2 2
1
4 fo C
fo and C are known, L can be calculated easily.
(3) Measurement of effective resistance:
effective resistance ,R= ωo L /Q true
(4) Measuernent of self capacitance:
Case 1:
1. capacitor is set to high value (C1)
2. circuit is set to resonance by adjustment of oscillator frequency
(f1)
3. resonance indicated by Q meter
4. 1
1
1
2 ( )d
f
L C C
 

------------------(1)
case2:
Frequency is doubled i.e. f2=2f1-----------(2)
Resonance is obtained by adjustment of tuning capacitor (C2)
2
2
1
2 ( )d
f
L C C
 

---------------------(3)
From (1),(2),(3), we get,
f2=2f1
2
1
2 ( )dL C C 
= 2 x
1
1
2 ( )dL C C 

2 1
1 2
1 2
1 4
,
, 4 4
4
,
3
d d
d d
d
or
c c c c
or c c c c
c c
or c

 
  


(5) Measurement of capacitance:
 connect dummy coil across T1 and T2
 resonance is set by varying C (let it is C1)
 Insert capacitor under test (CT) across T3 and T4.
 resonance is set up by varying C (let it is C2)
Therefore capacitor under test, CT =C1-C2
Measurement of Resistance of Insulating
Materials
insulation resistance (IR) test (also commonly known as a Megger) is a spot
insulation test which uses an applied DC voltage (typically either 250Vdc,
500Vdc or 1,000Vdc for low voltage equipment <600V and 2,500Vdc and
5,000Vdc for high voltage equipment) to measure insulation resistance in
either kΩ, MΩ or GΩ. The measured resistance is intended to indicate the
condition of the insulation or dieletric between two conductive parts, where
the higher the resistance, the better the condition of the insulation. Ideally, the
insulation resistance would be infinite, but as no insulators are perfect,
leakage currents through the dielectric will ensure that a finite (though high)
resistance value is measured.
Because IR testers are portable, the IR test is often used in the field as the
final check of equipment insulation and also to confirm the reliability of the
circuit and that there are no leakage currents from unintended faults in the
wiring (e.g. a shorted connection would be obvious from the test results).
One of the advantages of the IR test is its non-destructive nature. DC voltages
do not cause harmful and/or cumulative effects on insulation materials and
provided the voltage is below the breakdown voltage of the insulation, does
not deteriorate the insulation. IR test voltages are all well within the safe test
voltage for most (if not all) insulation materials.

Contents
[hide]
 1 Test Equipment
 2 Test Procedure
 3 Interpretation of Test
Results
 4 Factors Affecting Test
Results
o 4.1 Temperature
o 4.2 Humidity
 5 Related Tests
 6 References
Test Equipment
IR test set (courtesy ofMegger)
The Megger company were the original manufacturers of IR test equipment
over 100 years ago and have become synonymous with insulation resistance
testing. Most modern IR testers are digital, portable / handheld units and some
have multi-functional capabilities (e.g. built-in continuity testing).
Test Procedure
Firstly ensure that the equipment to be tested and the work area is safe, e.g.
equipment is de-energised and disconnected, all the relevant work permits
have been approved and all locks / tags in place.
Next, discharge capacitances on the equipment (especially for HV equipment)
with static discharge sticks or an IR tester with automatic discharging
capabilities.
The leads on the IR tester can then be connected to the conductive parts of the
equipment. For example, for a three-core and earth cable, the IR test would be
applied between cores (Core 1 to Core 2, Core 1 to Core 3 and Core 2 to Core
3) and between each core and earth. Similarly for three-phase motors, circuit
breakrs, switch-disconnectors, etc the IR test can be applied at the equipment
terminals (and earth connection).

Note that when applying an IR test to earth, it is good practice to connect the
positive pole of the IR tester to earth in order to avoid any polarisation effects
on the earth.
Once connected, the IR tester is energised for a typical test duration of 1
minute. The IR test measurements are recorded after 1 minute.
When the IR test is finished, discharge capacitances again for a period of 4-5
times the test duration.
Interpretation of Test Results
The minimum values for IR tests vary depending on the type of equipment
and the nominal voltage. They also vary according to international standards.
Some standards will define the minimum IR test values for the general
electrical installations.
For example, for low voltage installations in the IEC world, IEC 60364-6 [1]
Table 6A gives the minimum IR values and also suggests test voltage, i.e.
Nominal Circuit Voltage
(Vac)
Test Voltage
(Vdc)
Insulation Resistance
(MΩ)
Extra low voltage 250 0.5
Up to 500V 500 1.0
Above 500V 1,000 1.0
In the ANSI/NEC world, the standard ANSI/NETA ATS-2009 [2] provides
test procedures and acceptance levels for most types of electrical equipment.
Table 100.1 provides representative acceptance values for IR test
measurements, which should be used in the absence of any other guidance
(from the manufacturer or other standards):
Nominal Equipment
Voltage (Vac)
Min Test Voltage
(Vdc)
Min Insulation Resistance
(MΩ)
250 500 25
600 1,000 100
1,000 1,000 100
2,500 1,000 500
5,000 2,500 1,000
8,000 2,500 2,000
15,000 2,500 5,000
25,000 5,000 20,000

34,500 and above 15,000 100,000
NFPA 70B [3] also provides some guidance on insulation resistance testing
for different types of equipment.
Factors Affecting Test Results
There are two main factors that will affect IR test results:
Temperature
Electrical resistance has an inverse exponential relationship with temperature,
i.e. as temperature increases, resistance will decrease and vice versa. Since the
minimum acceptable IR test values are based on a fixed reference temperature
(usually 20o
C), the measured IR test values must be corrected to the reference
temperature in order to make sense of them.
As a rule of thumb, the resistance halves for every 10o
C increase in
temperature (and vice versa). So if the measured IR test value was 2MΩ at
20o
C, then it would be 1MΩ at 30o
C or 4MΩ at 10o
C.
ANSI/NETA ATS-2009 Table 100.14 provides correction factors for IR test
measurements taken at temperatures other than 20o
C or 40o
C, which were in
turn based on the correction factors in the freely available Megger book "A
stitch in time..." [4].
Humidity
The presence (or lack) of moisture can also affect the IR test measurements,
the higher the moisture content in the air, the lower the IR test reading. If
possible, IR tests should not be carried out in very humid atmospheres (below
the dew point). While there are no standard correction factors or guidance for
humid conditions, it is good practice to record the relative humidity of each IR
test so that they can be used for baseline comparisons in future tests. For
example, having past data on the IR test values for dry and humid days will
give you a foundation for evaluating future test values

MODULE-II
ELECTRONIC COUNTERS
Frequency Counters
Electronic counters are extensively used for measuring the frequency (number
of occurrence of an
event in a given time), time period of an event and time interval between two
events. Most digital
voltmeters generate a time-interval related to the level of the input voltage
first. Then, they measure
that interval and display it.
Time and Frequency Measurements
Operational Modes of Counters
Electronic counters are extensively used for measuring the frequency (number
of occurrence of an event in a given time), time period of an event and time
interval between two events. They display the results directly in digital forms
that can be easily read by the user. The counters work in three operational
modes as:
-period and
-interval.
The number of occurrences of event over the time of observation (i.e. 6 events
per
second). All
last digit of the
display. If the number displayed is small, this uncertainty causes large reading
errors. Therefore, this mode is useful at high frequencies The inverse of the
time-period (i.e. one explosion every 100 millisecond). This is useful at low
frequencies. Some counters automatically switch to this mode as the low
frequency ranges are selected. The period is measured and inverted usually by
digital techniques and the displayed result is the frequency. New counters
contain microprocessors that perform this operation easily.
Following elements are common in all modes of counters:
The magnitude of the input signal is not important. The periodic input signal
is converted into a pulse sequence by the signal shaper, which is composed of
a comparator and a pulse generator. Here, AC/DC coupling, trigger level and
polarity settings are available as in the case of the oscilloscope. There is no
amplitude range selection except a divide by ten (20 dB) attenuator to reduce
the amplitude of the input signal to a safe level for high-amplitude inputs.

internal time-base. Therefore, a very stable time base is an essential element
of the counter. Calibration of the time-base circuits may be achieved by using
special frequency standards based on tuning forks, crystal oscillators or with
NBS (National Broadcasting Society) standard broadcast frequencies.
frequency of repeating the measurement).
-segment light emitting diode (led) or liquid crystal (lcd)
type displays. Depending upon the frequency range of operation, there may be
six to eight digits displayed. Decimal counters are used to accumulate (count)
incoming pulses from the pulse gate and generate a binary coded decimal
(BCD) code at the output as illustrated in Figure. The code ranges from 0000
to 1001 corresponding to decimal ―0‖ and ―9‖ incrementing with every input
pulse. With the 10th pulse, the code returns to 0000 and the counter provides a
carry pulse to the next stage. At the end of the counting session, the code
accumulated in the
counters is transferred to a digital latch that holds it until the end of the next
counting
session. Counters are cleared automatically after the data is transferred to the
latch. The user can also clear them during initialization. This code stored in
the latch is applied to the display through BCD to 7-segment decoders and
displayed as decimal numbers. The display also incorporates annotations for
and MHz). The
time-base and/or gate control switches set the position of the decimal point.
The Counter in Frequency Mode

Block diagram of the counter in frequency mode
Principle of Operation
Figure shows the block diagram of a counter set to the frequency mode of
operation. The timebase
circuitry provides the start and stop pulses for the pulse gate. The pulses
generated from the input signal via the signal shaper are counted. The duration
of the gate signal (Tg) is equal to the period of the time base signal (Tb).
Number of pulses counted N=Tg* fs
fs being frequency of the input signal. Commonly used values for Tb are 0.1 s,
1 s, and 10 s.
The Time Base
Accuracy of the measurement is directly affected by the uncertainty in gating.
Hence, a time-base with high accuracy, precision and long-term stability is
essential. This is managed via a high stability clock circuit that runs at
frequency fc

Block diagram of the time-base
In some counters, the divider ratio is indicated at the time-base selector
switch. Finally, the frequency of the input (fs) is determined from the number
displayed (Nf) and time-base setting (10m) as:
The decimal point automatically moves in between appropriate digits and
respective frequency unit is also highlighted
to ease the reading as mentioned above.
The Counter in Time-Period Mode
Block diagram of the counter in time-period mode

In the period mode, the input signal provides the gating and the time-base
supplies the pulses for counting as shown in Figure . The number of pulses
counted:N=fb*Tg.
Hence, 10m becomes the multiplier in case of the period measurement. Period
measurement is preferred to frequency measurement in determining lower
frequencies. The read-out logic is designed to automatically positioned the
decimal point and display the proper unit.
The Counter in Time-Interval Mode
The phase-angle (shift) between two signals may be determined by measuring
the time interval between similar points on the two waveforms. Figure 4.40
illustrates the principle diagram of the measuring set-up. Both inputs contain
signal shapers that generate pulses corresponding to the trigger pick-off. One
of the pulse controls the starting of the counting while the other one stops the
counting. Trigger levels and slopes may be different for both channels. A
common-separate switch (Cm / Sep) allows utilization of the same signal for
both channels and with different trigger settings; the time between sections of
the same waveform can be measured. This is especially important in
determining the pulse duration and rise-time of the signal.

Signal Acquisition in a Spectrum Analyzer
Most spectrum analyzers (including the models in lab) are heterodyne
spectrum analyzers (also called scanning spectrum analyzers). A
heterodyne analyzer is essentially a radio receiver (a very sensitive and
selective reciever). Radio receivers, including those based on the
heterodyne , will be covered later in lecture. For now we will provide a
simple description of the basic ideas. Given a voltage signal x(t), we need
to somehow extract the frequency content out of it. As we know, the
digital storage oscilloscope provides one solution as it can calculate the
FFT of the signal from stored samples. Another solution would be to pass
x(t) through a long series of very narrow bandpass filters, having
adjacent passbands, and then plot the amplitudes of the filter outputs.
That is, if filter 1 has passband f1 - BW/2 < f < f1 + BW/2, and filter 2 has
passband f 2 -BW/2 < f < f2 + BW/2, where f1 + BW/2 = f2 - BW/2, and
so on, and if BW (the bandwidth) is small enough, then the filter outputs
give us the frequency components X(f1), X(f 2), . . . and so on . This is, of
course, not a practical solution. A better solution is suggested by a simple
property of Fourier transforms: recall that if we multiply (in the time
domain) a signal by a sinusoid, the spectrum of the signal is shifted in
frequency by an amount equal to the frequency the sinusoid.
Now instead of a bank of narrow filters, we shall have one narrow filter
centered at a fixed frequency, say fI, and we shall scan the signal
spectrum across this filter by multiplying x(t) by a sinusoid of varying
frequency f0 . See Figure 1. The filter is a narrow bandpass filter at a
fixed frequency, fI, (called the intermediate frequency); in a spectrum

analyzer, its bandwidth is selected by the user. The oscillator frequency,
f0, is adjustable, as indicated in Figure 1. In an ordinary AM or FM
radio, when you tune the receiver you are selecting this frequency so that
the signal will pass through the filter; in a spectrum analyzer, this
frequency is automatically scanned (repeatedly) over a range, which must
be selected so that the frequency component X(f) is shifted to fI and
passed by the filter. For example, if we want to view the frequency
content of x(t) from f1 to f2 , then we must select f0 to scan from f1 + fI to
f2 + fI.

MODULE-III
A Basic DC Voltmeter
The moving coil can be used as a voltmeter by adding a series resistance RS as
illustrated in Figure 4.14. The input voltage is divided between the coil
resistance RMC and RS. Current passing through both resistors is IMC which
is limited by the full-scale deflection current IFSD of the coil. The full-scale
input voltage
VM = IFSD(RS+RMC)
The input impedance seen is: RM = RS + RMC
However, with RS>>RMC, RM is approximately equal to RS and VM
IFSDRS.
Basic DC voltmeter
AC VOLTMETERS
The voltmeter based on the permanent magnet moving coil (PMMC or
D‘Arsonval) and digital
voltmeter that will be discussed later cannot be directly used to measure the
alternating voltages.
When measuring the value of an alternating current signal it is often necessary
to convert the signal into a direct current signal of equivalent value (known as
the root mean square, RMS value). This process can be quite complex. Most
low cost instrumentation and signal converters carry out this conversion by
rectifying and filtering the signal into an average value and applying a
correction factor. Hence, we can classify the AC voltmeters in two broad
categories as the averaging and true RMS types.
Average and RMS Values
The moving coil instrument reads the average of an AC waveform. The
average of the current waveform i(t)

where T = 2 /T = radial frequency (rad/sec). However, if
this current is applied to a resistor R, the instantaneous power on the resistor
p(t) = i2(t)R
The average power over the period T becomes
Hence, the average power is equivalent to the power that would be generated
by a DC current callethe effective current that
i
Due to squaring, averaging (mean) and square-rooting operations, this is
called the ―RMS.‖ value of the current and IRMS is the true value of the
current that we want to measure. The averaging time must be sufficiently long
to allow filtering at the lowest frequencies of operation desired. Hence, in
electrical terms, the AC RMS value is equivalent to the DC heating value of a
particular waveform—voltage or current.
The Full-Wave Rectifier
The half-wave rectifier is used in some voltmeters, but the mostly adapted one
uses the full waverectifier shown in Figure 4.23. Here, a bridge-type full-wave
rectifier is shown. For the + half cycle the current follows the root ABDC. For
the – half cycle root CBDA is used. The current through the meter resistor Rm
is the absolute value of the input current as shown in the inset. The voltage
waveform on the meter resistance Rm has the same shape as the current. The
average value of the voltage becomes:

VAV is the DC component of the voltage and it is the value read by the
moving coil instruments.
Hence, the inherently measured value (IM) is the average value, while the
true value is the RMS value.
Form Factor
The ratio of the true value to the measured value is called the form factor or
safe factor (SF). For
sinusoidal signals the form factor is SF = (VRMS/VAV).
In AC voltmeters, the reading is corrected by a scale factor = safe factor (SF)
= 1.11.
True RMS Meters
The rectification, averaging and form factor correction approach produces
adequate results in most cases. However, a correct conversion or the
measurement of non sine wave values, requires a more complex and costly
converter, known as a True RMS converter. The characteristics of these
meters are defined in terms of the input range, bandwidth (frequency range in
which the device operates successfully), accuracy and crest factor. The crest
factor is a measurement of a waveform, calculated from the peak amplitude
of the waveform divided by the RMS value of the waveform
The power dissipated by a resistor R that is exposed to the signal is
The AC signal would be applied to a small heating element which was
twinned with a thermocouple which could be used in a DC measuring circuit.

The technique is not particularly precise but it will measure any waveform at
any frequency. Thermal converters have become quite rare, but as they are
inherently simple and cheap they are still used by radio hams and hobbyists,
who may remove the thermal element of an old unreliable instrument and
incorporate it into a modern design of their own construction.
A true RMS type AC voltmeter that uses the thermal converter principle
an analog multiplier in a specific configuration which multiplies the input
signal by itself (squares it), averages the result with a capacitor, and then
calculates the square root of the value (via a multiplier/squarer circuit in the
feedback loop of an operational amplifier), or
-wave precision rectifier circuit to create the absolute value of the
input signal, which is fed into a operational amplifier arranged to give an
exponential transfer function, then doubled in voltage and fed to a log
amplifier as a means of deriving the square-law transfer function, before time-
averaging and calculating the square root of the voltage, similar to above,
-effect transistor may be used to directly create the square-law
transfer function, before time-averaging. thermal converters they are subject
to bandwidth limitations which makes them unsuitable for most RF work. The
circuitry before time averaging is particularly crucial for high frequency
performance. The slew rate limitation of the operational amplifier used to
create the absolute value (especially at low input signal levels) tends to make
the second method the poorest at high frequencies, while the FET method can
work close to VHF. Specialist techniques are required to produce sufficiently
accurate integrated circuits for complex analog calculations, and very often
meters equipped with such circuits offer True RMS conversion as an optional
extra with a significant price increase.
The third approach is to use Digital RMS converters. Digital and PC-based
oscilloscopes have the waveform being digitized so that the correct RMS
value may be calculated directly. Obviously the precision and the bandwidth
of the conversion is entirely dependent on the analog to digitalconversion. In
most cases, true RMS measurements are made on repetitive waveforms, and
under such conditions digital oscilloscopes (and a few sophisticated sampling
multimeters) are able to achieve very high bandwidths as they sample at a

fraction of the signal frequency to obtain a stroboscopic effect (that will be
explained later in section covering the digital storage oscilloscope).
Analog RMS to DC converter
The third approach is to use Digital RMS converters. Digital and PC-based
oscilloscopes have the waveform being digitized so that the correct RMS
value may be calculated directly. Obviously the precision and the bandwidth
of the conversion is entirely dependent on the analog to digital conversion. In
most cases, true RMS measurements are made on repetitive waveforms, and
under such conditions digital oscilloscopes (and a few sophisticated sampling
multimeters) are able to achieve very high bandwidths as they sample at a
fraction of the signal frequency to obtain a stroboscopic effect (that will be
explained later in section covering the digital storage oscilloscope)
Amplifiers
The amplifier is a device that increases the magnitude of the input voltage
(voltage amplifier as in Figure 4.33), current (current amplifier) and power
(power amplifier). The ratio of the output to the input (if of the same kind, i.e.
both voltage) is called the gain if it is greater than 1 and denoted by G. For a
voltage amplifier; G=Vo/VI
where Vo is the output voltage and VI is the input voltage. The gain is a
unitless quantity.
Sometimes the gain is expressed in decibels (dB) as: GdB = 10log(Po/PI) =
20log(Vo/VI)
where Po is the output power and PI is the input power of the amplifier
measured across the same resistor.

If the output is smaller than the input, this is called the attenuation. GdB is
positive for the
gain and negative for the attenuation. For example, a gain of 60 dB indicates
that the output is the input multiplied by 1000 while a gain of –20 dB shows
that the input is reduced (attenuated) by 10 times by the system.
THE DIGITAL VOLTMETER (DVM)
Use, Advantages and Operation
It is a device used for measuring the magnitude of DC voltages. AC voltages
can be measured after
rectification and conversion to DC forms. DC/AC currents can be measured
by passing them through
a known resistance (internally or externally connected) and determining the
voltage developed
across the resistance (V=IxR).
The result of the measurement is displayed on a digital readout in numeric
form as in the case of the counters. Most DVMs use the principle of time
period measurement. Hence, the voltage is converted into a time interval ―t‖
first. No frequency division is involved. Input range selection automatically
changes the position of the decimal point on the display. The unit of measure
is also highlighted in most devices to simplify the reading and annotation. The
DVM has several advantages over the analog type voltmeters as:
matic range
selection.
Ri Ci
eference voltage
source.
decimal) code and can
be send to computers or printers.
It is composed of an amplifier/attenuator, an analog to digital converter,
storage, display and timing circuits. There is also a power supply to provide
the electrical power to run electronic components. The circuit components
except the analog to digital converter circuits are similar to the ones used in
electronic counters. The input range selection can be manually switched
between ranges to get most accurate reading or it can be auto ranging that
switches between ranges automatically for best reading.

A simplified diagram for a digital voltmeter
The Analog to Digital Converter (ADC) – Sample and Hold
The analog to digital converter contains a sample and hold circuit, and
conversion circuits. The
sample and hold is composed of an electronic switch and a capacitor. The
switch turns on and off at regular intervals. The capacitor charges and
assumes the level of the input voltage as the switch is on. It holds the charge
(hence the level of the input voltage) as the switch is off. The unity-gain
buffer eliminates the loading of the capacitor by proceeding analog to digital
converter circuitry.shows a simplified diagram with the input and output
waveforms of the circuit.
Digitization of Analog Signals
The input of the sample and hold circuit is a continuous time analog signal
that can take any value any time. The output is a discrete time signal that can
take any value but only at certain times. This signal can't be processed by a
digital circuit unless it is converted into a digital code.
The analog input signal is continuous in time and it can take any value at any
time. This is converted to a discrete-time signal that can accept any value but
at certain times. The next stage is to divide the amplitude range into discrete
steps as well by a process called the quantization. The figure exemplifies the
principles for a 4-bit converter in which the dynamic range (the maximum
peak to peak amplitude that the input signal can attain) is divided into 24 – 1 =
15 steps. A binary code (or binary coded decimal – BCD) is assigned for each
level from 0000 to 1111 (1001 for BCD).
Integrating Type Analog to Digital Converters
The Basic Integrator
This type of converters generates a time interval

Functional Block Diagram of Ramp Type (Single Slope) DVM
Functional block diagram of a positive ramp type DVM is shown in Figure
4.46 The timing diagram is given in Fig. It has two major sections as the
voltage to time conversion unit and time
measurement unit. The conversion unit has a ramp generator that operates
under the control of the sample rate oscillator, two comparators and a gate
control circuitry. The internally generated ramp voltage is applied to two
comparators. The first comparator compares the ramp voltage into the input
signal and produces a pulse output as the coincidence is achieved (as the ramp
voltage becomes larger than the input voltage). The second comparator
compares the ramp to the ground voltage (0 volt) and produces an output
pulse at the coincidence.
Th Vm. The ranging
and attenuation section scales the DC input voltage so that it will be within the
dynamic range. The decimal point in the output display automatically
positioned by the ranging circuits.

Simplified block diagram of a single-ramp type digital voltmeter

Timing diagram for a single-ramp digital voltmeter
The outputs of the two comparators derive the gate control circuit that
generates and output
pulse that starts with the first coincidence pulse and ends with the second.
Thus, the duration of the pulse ―t‖ can be computed from the triangles as

For the ramp voltage with fixed slope and time base that runs at fixed rate (fc)
N is directly proportional to Vi. The multiplier T.fc/Vm is set to a constant
factor of 10. The polarity of the voltage is indicated if it is ―-―. With no
indication, it is understood that the polarity is ―+‖. The polarity is detected by
the polarity circuit with the help of comparator pulses. For positive slope ramp
type voltmeter, the first coincidence of the ramp is with the ground voltage if
the input is positive. With a negative input voltage however, the first
coincidence will be with the input voltage. The display stays for sometimes
(around three seconds) and then it is refreshed by the sample rate oscillator. A
trigger pulse is applied to the ramp generator to initiate a new ramp.
Meanwhile a reset (initialize) pulse is applied to the decade counters to clear
the previously stored code.
The display indicates the polarity as well as the numbers in decimal and a
decimal point. The first digit contains the polarity sign and the number
displayed can be only ―1‖ or ―0‖ for most voltmeters. Therefore, this is called
―half‖ digit. Hence, a three and a half digit display can have up to 1999 and a
four and a half digit one can go up to 19999.
Q meter:
A Q meter is a piece of equipment used in the testing of radio
frequency circuits. A Q meter measures Q, the quality factor of a
circuit, which expresses how much energy is dissipated per cycle
in a non-ideal reactive circuit:
This expression applies to an RF and microwave filter, bandpass
LC filter, or any resonator. It also can be applied to an inductor or
capacitor at a chosen frequency. For inductors
Where XLis the reactance of the inductor, L is the inductance,W is the
angular frequency and R is the resistance of the inductor. The
resistance represents the loss in the inductor, mainly due to the

resistance of the wire.Q meter works on the principle of series
resonance. For LC band pass circuits and filters:
Where F is the resonant frequency (center frequency) and BW is the
filter bandwidth. In a band pass filter using an LC resonant circuit,
when the loss (resistance) of the inductor increases, its Q is reduced,
and so the bandwidth of the filter is increased. In a coaxial cavity filter,
there are no inductors and capacitors, but the cavity has an equivalent
LC model with losses (resistance) and the Q factor can be applied as
well.
OPERATION:
Internally, a minimal Q meter consists of a tuneable RF generator with
a very low impedance output and a detector with a very high
impedance input. There is usually provision to add a calibrated amount
of high Q capacitance across the component under test to allow
inductors to be measured in isolation. The generator is effectively
placed in series with the tuned circuit formed by the components under
test, and having negligible output resistance, does not materially affect
the Q factor, while the detector measures the voltage developed
across one element (usually the capacitor) and being high impedance
in shunt does not affect the Q factor significantly either. The ratio of the
developed RF voltage to the applied RF current, coupled with
knowledge of the reactive impedance from the resonant frequency,
and the source impedance, allows the Q factor to be directly read by
scaling the detected voltage.
WORKING PRINCIPLE:

MODULE-IV
OSCILLOSCOPE:
In many applications, observing certain voltage waveforms in a circuit plays a
crucial role in understanding the operation of the circuit. For that purpose
several measurement instruments are used like voltmeter, ammeter, or the
oscilloscope. An oscilloscope (sometimes abbreviated as ―scope‖) is a
voltage sensing electronic instrument that is used to visualize certain voltage
waveforms. An oscilloscope can display the variation of a voltage waveform
in time on the oscilloscope‘s screen.
Oscilloscopes also come in analog and digital types. An analog oscilloscope
works by directly applying a voltage being measured to an electron beam
moving across the oscilloscope screen. The voltage deflects the beam up and
down proportionally, tracing the waveform on the screen. This gives an
immediate picture of the waveform. In contrast, a digital oscilloscope
samples the waveform and uses an analog-to-digital converter (or ADC) to
convert the voltage being measured into digital information. It then uses this
digital information to reconstruct the waveform on the screen.
An oscilloscope measures voltage waves. One cycle of a wave is the portion
of the wave that repeats. A voltage waveform shows time on the horizontal
axis and voltage on the vertical axis. Oscilloscopes are electronic equipment
mainly used in displaying and measuring electrical voltage signals. Other
physical signals can be displayed through proper sensors. The writing pen in
this equipment is the electron beam and writing medium is a special screen
that glows when the electron beam strikes on it. The electron beam can be
deflected from its straight path using electrical or magnetic fields, hence easily
moved across the screen. Eventually a spot of light that can be placed on
different locations on the screen under the control of external electrical signals

becomes available. For y-t recording, the spot travels horizontally across the
screen at a constant speed and moves vertically in response to the magnitude
of the input signal. Intensity or brightness of thedisplay is sometimes called
the z axis.
Oscilloscopes can be classified as analog and digital. To better understand the
oscilloscope controls, we need to know a little more about how oscilloscopes
display a signal. Analog oscilloscopes work somewhat differently than digital
oscilloscopes. However, several of the internal systems are similar. Analog
oscilloscopes are somewhat simpler in concept and are described below. Front
panel of an oscilloscope is shown in Figure 5.3. It has a display screen with a
8 cm by 10 cm grid drawn on it. The display has controls for the intensity
(brightness of the trace), focus and astigmatism (sharpness of the trace). On
the right hand side there are control sections for vertical, horizontal, and
trigger controls and input connectors. The oscilloscope is a versatile
instrument that can be used for measuring signal voltages from a few
millivolts up to hundreds of volts. Depending on how we set the vertical scale
(volts/div control), an attenuator reduces the signal voltage or an amplifier
increases the signal voltage. One cycle of a wave is the portion of the wave
that repeats. In general
use, only a few cycles are displayed.
Simplified block diagram of an analog oscilloscope
Two signals are needed to deflect the beam on the screen horizontally and
vertically. The laboratory oscilloscope is generally used to display signals in
time. The signal to be viewed is applied to a vertical (deflection) amplifier that

increases the potential of the input signal to a level that will provide a useful
deflection of the electron beam.
The time-base circuitry generates a voltage to supply the CRT to deflect the
spot at a constant time-dependant rate. The voltage waveform is named
commonly as the sweep signal and it has the appearance of a repetitive ramp
function. A triggering circuit is used to synchronize the horizontal deflection
with the vertical input, so that the horizontal deflection starts at the same point
of the vertical input signal each time it runs (sweeps). Eventually, the beam
moves at a constant time-dependant rate horizontally and the image generated
on the screen indicates the time variation of the input signal. Each block in a
signal path causes certain time delay. Hence, the beam does not start moving
horizontally immediately following the detection of the trigger point. The
delay line delays the signal applied to the vertical plates by an amount equal to
the time delay for the sweep signal applied to the horizontal deflection plates.
Eventually, the vertical signal is displayed on the screen alwaysstarting at the
trigger point.
DELAY LINE
The purpose of delay lines in oscilloscopes is to allow observation of the
leading edge of the trigger event. In the vertical signal path, before the delay
line, there is typically a trigger pick-off which supplies an undelayed copy of
the vertical signal to the the trigger and sweep circuitry. Trigger and sweep
circuitry need about 60ns to react when presented with the trigger event.
Without a delay line, the trigger event would already have come and gone
before the scope can trigger and sweep. By sending the input signal through a
delay line, the scope will have triggered and begun sweeping by the time the
trigger event emerges from the delay line. Thus, the trigger event is drawn on
the screen where the operator can see it, photograph it, or record it by other
means.
There is an inevitable delay between the application of the input and
appearance of the output in all electronic circuit elements. The amount of
delay depends upon the element itself and specified by its manufacturer. In the
triggered mode of operation, the input signal is applied to the trigger circuit
that derives the sawtooth waveform generator. Then, the resultant sawtooth
waveform is applied to the horizontal deflection plates via the horizontal
amplifier. Hence, there is a time delay (in the order of a few hundred
nanosecond) between the coincidence of the input signal with the trigger level
signal (trigger pick-off) and starting of the sweep on the display. This delay
may not be objectionable at low frequency applications. For example, the
period of a 1 kHz sine wave is 1 millisecond. If the delay is 100 nanosecond
which is one in a ten thousand of the period. Hence, it will not be effective
displaying the signal. However, if we have the frequency as 10 MHz, the
period of the signal is 100 nanosecond, which is the same as the delay. A
delay line is added between the vertical amplifier and the vertical deflection
plates that will delay the application of the input signal to the deflection plates
by the amount of time equal to the delay comes from the time-base circuitry.

The delay in trigger circuit is T1, delay in sawtooth generator is T2 and delay
in the horizontal amplifier is indicated as T3. The input signal is delayed by
the same amount so that the sweeps starts displaying the input signal from the
coincidence point.
PROBES:
A test probe (test lead, test prod, or scope probe) is a physical device used to
connect electronic test equipment to a device under test (DUT).

MULTI-TRACE OSCILLOSCOPES
Most laboratory oscilloscopes display two more traces simultaneously
although they have a single electron gun. Each trace can represent an
independent input signal. There are identical input connector, attenuator and
amplifier for each input. Outputs of vertical amplifiers are selected oneby- one
by an electronic switch and applied to the driver amplifier for the vertical
deflection plate assembly as illustrated in Figure 5.18. There are two modes of
operation of the electronic switch as chopped and alternate. In the chopped
mode, the switch runs at high frequency (around 500 kHz) and calls at each
input for a fraction of the total sweep duration. Hence, traces are drawn as
short spots of light on the screen. For example, if we have two input signals
each at 1 kHz and the sweep rate is 500 kHz, then there are 250 spots across
one period of each trace. The illumination of the spot the gap between the
spots. Also, the chopping is not synchronous with the sweep leading to the
dots appearing at different places along the trajectory for successive sweeps.
Hence, the traces
are seen continuous at low frequency applications. Therefore, the chopped
mode is useful at low frequencies.
In the second operational mode, the switch remains in one of the chan el
throughout the complete sweep duration and it picks the other one in the next
sweep. Since switch displays each channel at alternate cycles of the sweep
signal, the name alternate mode is used. This is useful at high frequency
operations. Some laboratory oscilloscopes incorporate the selection of
chopped or alternate mode in the time-base switch. Only one of the input

channels is used for the trigger control in both modes. In the alternate mode if
channel-1 is selected as the trigger input, it is used even while channel-2 is
displayed.
DIGITAL STORAGE OSCILLOSCOPES (DSO)
Oscilloscopes also come in analog and digital types. An analog oscilloscope
works by directly applying a voltage being measured to an electron beam
moving across the oscilloscope screen. The voltage deflects the beam up and
down proportionally, tracing the waveform on the screen. This gives an
immediate picture of the waveform as described in previous sections. In
contrast, a digital oscilloscope samples the waveform and uses an analog-to-
digital converter (or ADC) to convert the voltage being measured into digital
information. It then uses this digital information to reconstruct the waveform
on the screen. For many applications either an analog or digital oscilloscope
will do. However, each type does possess some unique characteristics making
it more or less suitable for specific tasks. People often prefer analog
oscilloscopes when it is important to display rapidly varying signals in "real
time" (or as they occur). Digital oscilloscopes allow us to capture and view
events that may happen only once. They can process the digital waveform
data or send the data to a computer
for processing. Also, they can store the digital waveform data for later
viewing and printing.
Necessity for DSO and Its Advantages
If an object passes in front of our eyes more than about 24 times a second over
the same trajectory, we cannot follow the trace of the object and we will see
the trajectory as a continuous line of action. Hence, the trajectory is stored in
our physiological system. This principle is used in obtaining a stationary trace
needed to study waveforms in conventional oscilloscopes. This is however, is
not possible for slowly varying signals and transients that occur once and then
disappear. Storage oscilloscopes have been developed for this purpose. Digital

storage oscilloscopes came to existence in 1971 and developed a lot since
then. They provide a superior method of trace storage. The waveform to be
stored is digitized, stored in a digital memory, and retrieved for displayed on
the storage oscilloscope. The stored waveform is continuously displayed by
repeatedly scanning the stored waveform. The digitized waveform can be
further analyzed by either the oscilloscope or by loading the content of the
memory into a computer. They can present waveforms before, during and
after trigger. They provide markers, called the cursors, to help the user in
measurements in annotation (detailing) of the measured values.
Principles of Operation
Principle Diagram Representing Operation of the DSO
A simplified block diagram of a digital storage oscilloscope is shown in fig.
The input circuitry of the DSO and probes used for the measurement are the
same as the conventional oscilloscopes. The input is attenuated and amplified
with the input amplifiers as in any oscilloscope. This is done to the input
signal so that the dynamic range of the A/D converter can be utilized
maximally. Many DSOs can also operate in a conventional mode, bypassing
the digitizing and storing features. The output of the input amplifier drives the
trigger circuit that provides signal to the control logic. It is also sampled under
the control of the control logic. The sample and hold circuit takes the sample
and stores it as a charge on a capacitor. Hence, the value of the signal is kept
constant during the analog to digital conversion. The analog to digital
converter (A/D) generates a binary code related to the magnitude of the
sampled signal. The speed of the A/D converter is important and ―flash‖
converters are mostly used. The binary code from the A/D converter is stored
in the memory. The memory consists of a bank of random access memory
(RAM) integrated circuits (ICs).

Simplified block diagram of a digital storage oscilloscope
(DSO)
Measurement Techniques:
The major concern in observing a signal on the oscilloscope screen is to make
voltage and time measurements. These measurements may be helpful in
understanding the behavior of a circuit component, or the circuit itself,
depending on what you measure. Except for the X-Y mode of operation, the
oscilloscope displays the voltage value of the waveform as a function time.
The oscilloscope screen is partitioned into the grids, which divides both the
horizontal axis(voltage) and the vertical axis(time) into divisions which will
be helpful in making the measurements. Obviously one needs to know the
time or the voltage values corresponding to each division, in order to make
accurate calculations. These values are determined by two variables namely
the time/div and the volt/div both of which can be adjusted from the relevant
buttons available on the front panel of the oscilloscope . Also note that, the
time/div button controls the trace time of the sweep generator, whereas the
volt/div button controls the `gain` in the vertical amplifiers in the vertical
deflection system.
Typical quantities, which are of primer interest when observing a signal with
the scope, are Shown.

For the given figure, suppose that the variables volt/div and time/div are set
to:
volt/div = 2Volts/div.
time/div = 1millisecond/div
Then the corresponding values shown on the figure are calculated to be;
Peak Value = 6volts
Peak to peak value = 12 Volts
DC Value (Average Value) = 2 Volts
Period = 3 milliseconds
Frequency =1/T =333 Hz.
Note that the signal s(t), shown on the oscilloscope screen can be expressed
as,
Phase difference:
In some applications, one may need to monitor or compare two or more
signals simultaneously. A typical example can be the comparison of the input
voltage with the output voltage of a two-port (input and output ports) circuit.
If the signals that are being monitored have the same frequency, a time delay
may occur between the signals (i.e. one signal may lead the other or vice
versa). Two waves that have the same frequency, have a phase difference that
is constant (independent of t). When the phase difference(2*pi) is zero, the
waves are said to be in phase with each other. Otherwise, they are out of phase
with each other. If the phase difference is 180 degrees. , then the two signals

are said to be in anti-phase. If the peak amplitudes of two anti-phase waves
are equal, their sum is zero at all values of time. The phase difference is
expressed in terms of radians or degrees.
In Dual Mode of the oscilloscope the phase difference can be calculated
easily as follows.
Del T = horizontal spacing of the peak values (or the zero crossings) of the
two signals.
T = horizontal spacing for one period.
Then the phase difference=θ= ∆T/T *360 In degree.

Lecture note 2

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Lecture note 2