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EC2353 -Antenna and wave propagation
Introduction
An antenna is an electrical conductor or system of conductors Transmission - radiates electromagnetic energy into space Reception - collects electromagnetic energy from space
In two-way communication, the same antenna can be used for transmission andreception
An antenna is a circuit element that provides a transition form a guided wave on atransmission line to a free space wave and it provides for the collection of
electromagnetic energy.
In transmit systems the RF signal is generated, amplified, modulated and appliedto the antenna
In receive systems the antenna collects electromagnetic waves that are cuttingthrough the antenna and induce alternating currents that are used by the receiver
CONCEPT OF VECTOR POTENTIAL
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Hertzian dipole
A simple practical antenna is a doublet or Hertzian dipole (see a figure below). It
is very short length of wire over which the current distribution can be assumed uniform.Maxwells equations show that such an antenna when energized by a high frequencycurrent is associated with an induction field which decreases inversely as square of the
distance and a radiation field which decreases inversely as distance only. The later is still
measurable at large distances from the doublet and is well-known radiation field used inradio communications
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DEFINITIONS
Radiation Intensity. In a given direction, the power radiated form an antenna perunit solid angle.
Directive Gain. In a given direction, 4 times the ratio of theradiation intensity inthat direction to the total power radiated by the antenna.
Directivity. The value of the directive gain in the direction of its maximum value. Power Gain. In a given direction, 4 times the ratio of the radiationintensity in
that direction to the net power accepted by the antenna from the connected
transmitter. NOTES: (1) When thedirection is not stated, the power gain is usually
taken to be thepower gain in the direction of its maximum value. (2) Power gaindoes not include reflection losses arising from mismatchof impedance.
Beamwidthis the angular separation of the half-power points of the radiatedpattern
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Bandwidthis the difference between the upper and lowercutoff frequenciesof,for example, afilter,acommunication channel,or asignal spectrum,and is
typically measured inhertz.In case of abasebandchannel or signal, the andwidthis equal to its upper cutoff frequency. Bandwidth in hertz is a centralconcept in
many fields, includingelectronics,information theory,radiocommunications,
signal processing,andspectroscopy GAINGain is an antenna property dealing with an antenna's ability to
direct its radiated power in a desired direction, or to receive
energy preferentially from a desired direction. However, gain isnot a quantity which can be defined in terms of physical quantities
such as the Watt, ohm or joule, but is a dimensionless ratio.
As a consequence, antenna gain results from the interaction of
all other antenna characteristics.Antenna characteristics of gain,beamwidth, and efficiency areindependent of the antenna's use for
either transmitting or receiving. Generally these characteristics are
more easilydescribed for the transmitting case, however, theproperties apply as well to receiving applications.
Radiation resistanceAn important property of a transmitting antenna is its radiation resistance which is
associated with power radiated by the antenna. If I is the r.m.s (root mean square)antenna current and Rr is its radiation resistance, then the power radiated is I2Rr
watts where Rr is afictitiousresistance which accounts for the radiated power
somewhat like a circuit resistance which dissipates heat. The larger the radiationresistance the larger the power radiated by the antenna. In contrast, for receiving
antenna its input impedance is important. The input impedance is defined as the ratio
of voltage to current at its input and it must be generally matched to the connecting
line or cable. The input impedance may or may not be equal to radiation resistance,though very often it does. In most case Rr may be calculated or it can be determined
experimentally.
Half-wavelength dipoleThis type of antenna is a special case where each wire is exactly one-quarter of
the wavelength, for a total of a half wavelength. The radiation resistance is about 73
ohms if wire diameter is ignored, making it easily matched to a coaxial transmissionline. The directivity is a constant 1.64, or 2.15 dB. Actual gain will be a little less due
to ohmic losses.
Folded dipoleA folded dipole is a dipole where an additional wire (/2) links the two ends of the
(/2) half wave dipole. The folded dipole works in the same way as a normal dipole,
but the radiation resistance is about 300ohmsrather than the 75 ohms which is
expected for a normal dipole. The increase in radiation resistance allows the antenna
to be driven from a 300 ohm balanced line.
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RECIPROCITY: An antenna ability to transfer energy form the atmosphere to its receiver with the
same efficiency with which it transfers energy from the transmitter into the
atmosphere Antenna characteristics are essentially the same regardless of whether an antenna
is sending or receiving electromagnetic energy
An antenna with a non-uniform distribution of current over its length L can be considered
as having a shorter effective length Le over which the current is assumed to be uniformand equal to its peak. The relationship between Le and L is given by:
Effective apertureThe power received by an antenna can be associated with collecting area. Every
antenna may be considered to have such a collecting area which is called its effectiveaperture A. If Pd is a power density at the antenna and Pr is received power, then:
Polarization is the direction of the electric field and is the same as the physicalattitude of the antenna
A vertical antenna will transmit a vertically polarized waveThe receive and transmit antennas need to possess the same polarization
Antenna Gain Relationship between antenna gain and effective area
G = antenna gain
Ae = effective areaf = carrier frequency
c = speed of light ( 3 108 m/s)
= carrier wavelength
Radiation Pattern Radiation pattern is an indication of radiated field strength around the antenna.
Power radiated from a /2 dipole occurs at right angles to the antenna with nopower emitting from the ends of the antenna. Optimum signal strength occurs at
right angles or 180 from opposite the antenna
Radiation pattern Graphical representation of radiation properties of an antenna Depicted as two-dimensional cross section
Beam width (or half-power beam width) Measure of directivity of antenna
Reception pattern Receiving antennas equivalent to radiation pattern
Antenna Temperature
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( ) is a parameter that describes how much noise an antenna produces in a given
environment. This temperature is not the physical temperature of the antenna. Moreover,an antenna does not have an intrinsic "antenna temperature" associated with it; rather the
temperature depends on its gain pattern and the thermal environment that it is placed in.
To define the environment, we'll introduce a temperature distribution - this is thetemperature in every direction away from the antenna in spherical coordinates. Forinstance, the night sky is roughly 4 Kelvin; the value of the temperature pattern in thedirection of the Earth's ground is the physical temperature of the Earth's ground. This
temperature distribution will be written as . Hence, an antenna's temperature willvary depending on whether it is directional and pointed into space or staring into the sun.
For an antenna with aradiation patterngiven by , the noise temperature is
mathematically defined as:
This states that the temperature surrounding the antenna is integrated over the entire
sphere, and weighted by the antenna's radiation pattern. Hence, an isotropic antenna
would have a noise temperature that is the average of all temperatures around the
antenna; for a perfectly directional antenna (with a pencil beam), the antenna temperaturewill only depend on the temperature in which the antenna is "looking".
The noise power received from an antenna at temperature can be expressed in terms ofthebandwidth(B) the antenna (and its receiver) are operating over:
In the above,Kis Boltzmann's constant (1.38 * 10^-23 [Joules/Kelvin = J/K]). The
receiver also has a temperature associated with it ( ), and the total system temperature
(antenna plus receiver) has a combined temperature given by . This
temperature can be used in the above equation to find the total noise power of the system.
These concepts begin to illustrate how antenna engineers must understand receivers and
the associated electronics, because the resulting systems very much depend on each other.
A parameter often encountered in specification sheets for antennas that operate in certainenvironments is the ratio ofgainof the antenna divided by the antenna temperature (or
system temperature if a receiver is specified). This parameter is written as G/T, and has
units of dB/Kelvin [dB/K].
UNIT _2 WIRE ANTENNAS AND ANTENNA ARRAYS
Half wave antenna
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Quarter wave or unipole antenna
The quarter wave or unipole antenna is a single element antenna feed at one end,that behaves as a dipole antenna. It is formed by a conductor in length. It is fed in
the lower end, which is near a conductive surface which works as a reflector (see
Effect of ground). The current in the reflected image has the same direction andphase that the current in the real antenna. The set quarter-wave plus image forms
a half-wave dipole that radiates only in the upper half of space.
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Antenna arrayis a group of antennas or antenna elements arranged to provide the
desired directional characteristics. Generally any combination of elements can form anarray. However, equal elements in a regular geometry are usually used.
PATTERN MULTIPLICATIONThe pattern multiplication principle states that the radiation patterns of an array ofN
identical antennas is equal to the product of the element patternFe( )(pattern of one ofthe antennas) and the array patternFa( ), whereFa( )is the pattern obtained upon
replacing all of the actual antennas with isotropic sources.
LOOP ANTENNAThe small loop antenna is a closed loop as shown in Figure 1. These antennas
have low radiation resistance and high reactance, so that theirimpedanceis
difficult to match to a transmitter. As a result, these antennas are most often
used as receive antennas, where impedance mismatch loss can be tolerated.
The radius is a, and is assumed to be much smaller than a wavelength (a
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Figure 1. Small loop antenna.
Since the loop is electrically small, the current within the loop can be
approximated as being constant along the loop, so thatI= .
The fields from a small circular loop are given by:
The variation of the pattern with direction is given by , so that the
radiation pattern of a small loop antenna has the same power pattern as that of a
short dipole.However, the fields of a small dipole have the E- and H- fields
switched relative to that of a short dipole; the E-field is horizontally polarized
in the x-y plane.
The small loop is often referred to as the dual of the dipole antenna, because if
a small dipole had magnetic current flowing (as opposed to electric current as
in a regular dipole), the fields would resemble that of a small loop.
While the short dipole has a capacitive impedance (imaginary part of
impedance is negative), the impedance of a small loop is inductive (positive
imaginary part). The radiation resistance (and ohmic loss resistance) can be
increased by adding more turns to the loop. If there areNturns of a small loop
antenna, each with a surface area S(we don't require the loop to be circular at
this point), the radiation resistance for small loops can be approximated (in
Ohms) by:
For a small loop, the reactive component of the impedance can be determined
by finding the inductance of the loop, which depends on its shape (then
X=2*pi*f*L). For a circular loop with radius aand wire radiusp, the reactive
component of the impedance is given by:
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Small loops often have a low radiation resistance and a highly inductivecomponent to their reactance. Hence, they are most often used as receive
antennas. Exaples of their use include in pagers, and as field strength probes
used in wireless measurements.
Loop antennaA loopantennahas a continuous conducting path leading from
one conductor of a two-wire transmission line to the other conductor. All planar loops aredirectional antennas with a sharp null, and have a radiation pattern similar to thedipoleantenna.However, the large and small loops have different orientations with respect to
their radiation pattern.
Small loopsA loop is considered asmall loopif it is less than 1/4 of a
wavelength in circumference. Most directional receiving loops are about 1/10 of a
wavelength. The small loop is also called themagnetic loopbecause it is more sensitivie
to themagnetic componentof the electromagnetic wave. As such, it is less sensitive tonear field electric noise when properly shielded. The received voltage of a small loop can
be greatly increased by bringing the loop into resonance with a tuning capacitor.
Since the small loop is small with respect to a wavelength, thecurrent around the antenna is nearly completely in phase. Therefore, waves approaching
in the plane of the loop will cancel, and waves in the axis perpendicular to the plane of
the loop will be strongest. This is the opposite mechanism as the large loop.
Large loopsThe (large) loop antenna is similar to a dipole, except that the
ends of the dipole are connected to form a circle, triangle () or square. Typically a loop is
a multiple of a half or full wavelength incircumference.A circular loop gets higher gain(about 10%) than the other forms of large loop antenna, as gain of this antenna is directly
proportional to the area enclosed by the loop, but circles can be hard to support in a
flexible wire, making squares and triangles much more popular. Large loop antennas are
more immune to localized noise partly due to lack of a need for a groundplane. The largeloop has its strongest signal in the plane of the loop, and nulls in the axis perpendicular tothe plane of the loop. This is the opposite orientation to the small loop.
AM loopsAM loops are loops tuned for theAM broadcastingband.
Because of the extremely long wavelength, an AM loop may have multiple turns of wire
and still be less than 1/10 of a wavelength. Typically these loops are tuned with a
capacitor, and may also be wound around aferriterod to increaseaperture.
Direction finding with loops
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Loops are somewhat directional along the axis of highest gain,
but have a sharp null in the axis perpendicular to their highest gain. Therefore, when
using a loop for direction finding, the plane of the antenna is rotated until the signaldisappears. As planar loops have a 180 degree symmetry, other methods must be used to
determine if the signal is in front or behind the loop.
Frequently, a dipole and a loop are used together, to obtain acombinedcardioidradiation pattern with a sharp null on only one side.
Uniform linear array
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Slot antennasare used typically at frequencies between 300 MHz and
24 GHz. These antennas are popular because they can be cut out of whateversurface they are to be mounted on, and haveradiation patternsthat are roughly
omnidirectional (similar to a linear wire antenna, as we'll see). The polarization
is linear. The slot size, shape and what is behind it (the cavity) offer design
variables that can be used to tune performance.
Consider an infinite conducting sheet, with a rectangular slot cut out of
dimensions aand b, as shown in Figure 1. If we can excite some reasonable
fields in the slot (often called the aperture), we have an antenna.
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Figure 1. Rectangular Slot antenna with dimensions aand b.
To gain an intuition about slot antennas, first we'll learn Babinet's principle (put
into antenna terms by H. G. Booker in 1946). This principle relates the radiated
fields and impedance of an aperture or slot antenna to that of the field of its
dual antenna. The dual of a slot antenna would be if the conductive materialand air were interchanged - that is, the slot antenna became a metal slab in
space. An example of dual antennas is shown in Figure 2:
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Hence, if we know the fields from one antenna we know the fields of the other
antenna. Hence, since it is easy to visualize the fields from adipole antenna,the
fields and impedance from a slot antenna can become intuitive if Babinet's
principle is understood.
Note that thepolarizationof the two antennas are reversed. That is, since the
dipole antenna on the right in Figure 2 is vertically polarized, the slot antenna
on the left will be horizontally polarized.
Duality Example
As an example, consider a dipole similar to the one shown on the right in
Figure 2. Suppose the length of the dipole is 14.4 centimeters and the width is 2
centimeters, and that the impedance at 1 GHz is 65+j15 Ohms. The fields fromthe dipole antenna are given by:
What are the fields from a slot at 1 GHz, with the same dimensions as the
dipole?
Using Babinet's principle, the impedance can be easily found:
The impedance of the slot for this case is much larger, and while the dipole's
impedance is inductive (positive imaginary part), the slot's impedance is
capacitive (negative imaginary part). The E-fields for the slot can be easily
found:
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We see that the E-fields only contain a phi (azimuth) component; the antenna istherefore horizontally polarized.
Horn antennas are very popular at UHF (300 MHz-3 GHz) and higher
frequencies (I've heard of horns operating as high as 140 GHz). They often
have a directionalradiation patternwith a highgain, which can range up to 25
dB in some cases, with 10-20 dB being typical. Horns have a wide impedance
bandwidth,implying that theinput impedanceis slowly varying over a wide
frequency range (which also implies low values forS11orVSWR). The
bandwidth for practical horn antennas can be on the order of 20:1 (for instance,
operating from 1 GHz-20 GHz), with a 10:1 bandwidth not being uncommon.
The gain often increases (and thebeamwidthdecreases) as the frequency of
operation is increased. Horns have very little loss, so thedirectivityof a horn is
roughly equal to its gain.
Horn antennas are somewhat intuitive and not relatively simple to manufacture.
In addition, acoustic horns also used in transmitting sound waves (for example,
with a megaphone). Horn antennas are also often used to feed a dish antenna, or
as a "standard gain" antenna in measurements.
Popular versions of the horn antenna include the E-plane horn, shown in Figure
1. This horn is flared in the E-plane, giving the name. The horizontal dimension
is constant at w.
Figure 1. E-plane horn.
Another example of a horn is the H-plane horn, shown in Figure 2. This horn is
flared in the H-plane, with a constant height for the waveguide and horn of h.
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Figure 2. H-Plane horn.
The most popular horn is flared in both planes as shown in Figure 3. This is a
pyramidal horn, and has widthBand heightAat the end of the horn.
Figure 3. Pyramidal horn.
Horns are typically fed by a section of a waveguide, as shown in Figure 4. The
waveguide itself is often fed with ashort dipole,which is shown in red in
Figure 4. A waveguide is simply a hollow, metal cavity. Waveguides are used
to guide electromagnetic energy from one place to another. The waveguide in
Figure 4 is a rectangular waveguide of width band height a, with b>a. The E-
field distribution for the dominant mode is shown in the lower part of Figure 1.
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Figure 4. Waveguide used as a feed to horn antennas.
Reflector AntennaTo increase thedirectivityof an antenna, a fairly intuitive solution is to use a
reflector. For example, if we start with a wire antenna (lets say ahalf-wave
dipoleantenna), we could place a conductive sheet behind it to direct radiation
in the forward direction. To further increase the directivity, a corner reflector
may be used, as shown in Figure 1. The angle between the plates will be 90
degrees.
Figure 1. Geometry of Corner Reflector.
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The radiation pattern of this antenna can be understood by using image theory,
and then calculating the result via array theory. For ease of analysis, we'll
assume the reflecting plates are infinite in extent. Figure 2 below shows the
equivalent source distribution, valid for the region in front of the plates.
Figure 2. Equivalent sources in free space.
The dotted circles indicate antennas that are in-phase with the actual antenna;
the x'd out antennas are 180 degrees out of phase to the actual antenna.
Assume that the original antenna has an omnidirectional pattern given by .Then the radiation pattern (R) of the "equivalent set of radiators" of Figure 2
can be written as:
The above directly follows from Figure 2 and array theory (kis thewave
number.The resulting pattern will have the same polarization as the original
vertically polarized antenna. The directivity will be increased by 9-12 dB. The
above equation gives the radiated fields in the region in front of the plates.
Since we assumed the plates were infinite, the fields behind the plates are zero.
The directivity will be the highest when dis a half-wavelength. Assuming the
radiating element of Figure 1 is ashort dipolewith a pattern given by ,
the fields for this case are shown in Figure 3.
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Figure 3. Polar and azimuth patterns of normalized radiation pattern.
The radiation pattern, impedance and gain of the antenna will be influenced by
the distance dof Figure 1. The input impedance is increased by the reflector
when the spacing is one half wavelength; it can be reduced by moving the
antenna closer to the reflector. The lengthLof the reflectors in Figure 1 are
typically 2*d. However, if tracing a ray travelling along the y-axis from the
antenna, this will be reflected if the length is at least . The height of the
plates should be taller than the radiating element; however since linear antennasdo not radiate well along the z-axis, this parameter is not critically important.
The Parabolic Reflector
Antenna (Satellite Dish)
The most well-known reflector antenna is the parabolic reflector antenna, commonly
known as a satellite dish antenna. Examples of this dish antenna are shown in the
following Figures.
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Figure 1. The "big dish" of Stanford University.
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Figure 2. A random "direcTV dish" on a roof.
Parabolic reflectors typically have a very highgain(30-40 dB is common) and lowcross
polarization.They also have a reasonable bandwidth, with thefractional bandwidth
being at least 5% on commercially available models, and can be very wideband in the
case of huge dishes (like the Stanford "big dish" above, which can operate from 150
MHz to 1.5 GHz).
The smaller dish antennas typically operate somewhere between 2 and 28 GHz. The
large dishes can operate in the VHF region (30-300 MHz), but typically need to be
extremely large at this operating band.
The basic structure of a parabolic dish antenna is shown in Figure 3. It consists of a feed
antenna pointed towards a parabolic reflector. The feed antenna is often ahorn antenna
with a circular aperture.
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Figure 3. Components of a dish antenna.
Unlike resonant antennas like thedipole antennawhich are typically approximately a
half-wavelength long at the frequency of operation, the reflecting dish must be much
larger than a wavelength in size. The dish is at least several wavelengths in diameter, but
the diameter can be on the order of 100 wavelengths for very high gain dishes (>50 dB
gain). The distance between the feed antenna and the reflector is typically several
wavelenghts as well. This is in contrast to thecorner reflector,where the antenna is
roughly a half-wavelength from the reflector.
In the next section, we'll look at the parabolic dish geometry in detail and why a parabola
is a desired shape.To start, let the equation of a parabola with focal lengthFcan be written in the
(x,z) plane as:
This is plotted in Figure 1.
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Figure 1. Illustration of parabola with defining parameters.
The parabola is completely described by two parameters, the diameterDand
the focal lengthF. We also define two auxilliary parameters, the vertical height
of the reflector (H) and the max angle between the focal point and the edge of
the dish ( ). These parameters are related to each other by the following
equations:
To analyze the reflector, we will use approximations from geometric optics.
Since the reflector is large relative to a wavelength, this assumption is
reasonable though not precisely accurate. We will analyze the structure viastraight line rays from the focal point, with each ray acting as a plane wave.
Consider two transmitted rays from the focal point, arriving from two distinct
angles as shown in Figure 2. The reflector is assumed to be perfectly
conducting, so that the rays are completely reflected.
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Figure 2. Two rays leaving the focal point and reflected from the parabolicreflector.
There are two observations that can be made from Figure 2. The first is that
both rays end up travelling in the downward direction (which can be
determined because the incident and reflected angles relative to the normal of
the surface must be equal). . The rays are said to be collimated. The second
important observation is that the path lengths ADE and ABC are equal. This
can be proved with a little bit of geometry, which I won't reproduce here. These
facts can be proved for any set of angles chosen. Hence, it follows that:
All rays emanating from the focal point (the source or feed antenna) will be
reflected towards the same direction.
The distance each ray travels from the focal point to the reflector and then to
the focal plane is constant.
As a result of these observations, it follows the distribution of the field on the
focal plane will be in phase and travelling in the same direction. This gives rise
to the parabolic dish antennas highly directionalradiation pattern.This is why
the shape of the dish is parabolic.
Finally, by revolving the parabola about the z-axis, a paraboloid is obtained, as
shown below.
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For design, the value of the diameterDshould be increased to increase the gain
of the antenna. The focal lengthFis then the only free parameter; typical
values are commonly given as the ratioF/D, which usually range between 0.3and 1.0. Factors affecting the choice of this ratio will be given in the following
sections.
In the next section, we'll look at gain calculations for a parabolic reflector
antenna.
The fields across the aperture of the parabolic reflector is responsible for this
antenna's radiation. The maximum possible gain of the antenna can be
expressed in terms of the physical area of the aperture:
The actual gain is in terms of theeffective aperture,which is related to the
physical area by the efficiency term ( ). This efficiency term will often be on
the order of 0.6-0.7 for a well designed dish antenna:
Understanding this efficiency will also aid in understanding the trade-offs
involved in the design of a parabolic reflector. The efficiency can be written as
the product of a series of terms:
We'll walk through each of these terms.
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Radiation Efficiency
The radiation efficiency is the usual efficiency that deals with ohmic losses,
as discussed on theefficiencypage. Sincehorn antennasare often used as
feeds, and these have very little loss, and because the parabolic reflector istypically metallic with a very high conductivity, this efficiency is typically
close to 1 and can be neglected.
Aperture Taper Efficiency
The aperture radiation efficiency is a measure of how uniform the E-field is
across the antenna's aperture. In general, an antenna will have the maximum
gain if the E-field is uniform in amplitude and phase across the aperture (the
far-field is roughly the Fourier Transform of the aperture fields). However, the
aperture fields will tend to diminish away from the main axis of the reflector,
which leads to lower gain, and this loss is captured within this parameter.
This efficiency can be improved by increasing theF/Dratio, which also lowers
the cross-polarization of the radiated fields. However, as with all things in
engineering, there is a tradeoff: increasing theF/Dratio reduces the spillover
efficiency, discussed next.
Spillover Efficiency
The spillover efficiency is simple to understand. This measures the amount
of radiation from the feed antenna that is reflected by the reflector. Due to the
finite size of the reflector, some of the radiation from the feed antenna will
travel away from the main axis at an angle greater than , thus not being
reflected. This efficiency can be improved by moving the feed closer to the
reflector, or by increasing the size of the reflector.
Other Efficiencies
There are many other efficiencies that I've lumped into the parameter . This
is a major of all other "real-world effects" that degrades the antenna's gain and
consists of effects such as:
Surface Error- small deviations in the shape of the reflector degrades
performance, especially for high frequencies that have a small wavelength and
become scattered by small surface anomalies
Cross Polarization- The loss of gain due tocross-polarized(non-desirable)
radiation
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Aperture Blockage- The feed antenna (and the physical structure that holds
it up) blocks some of the radiation that would be transmitted by the reflector.
Non-Ideal Feed Phase Center- The parabolic dish has desirable properties
relative to a single focal point. Since the feed antenna will not be a point
source, there will be some loss due to a non-perfect phase center for a horn
antenna.
Calculating Efficiency
The efficiency is a function of where the feed antenna is placed (in terms ofF
andD) and the feed antenna's radiation pattern. Instead of introducing complex
formulas for some of these terms, we'll make use of some results by S. Silver
back in 1949. He calculated the aperture efficiency for a class of radiation
patterns given as:
TYpically, the feed antenna (horn) will not have a pattern exactly like the
above, but can be approximated well using the function above for some value
of n. Using the above pattern, the aperture efficiency of a parabolic reflector
can be calculated. This is displayed in Figure 1 for varying values of and the
F/Dratio.
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Figure 1. Aperture Efficiency of a Parabolic Reflector as a function ofF/Dorthe angle , for varying feed antenna radiation patterns.
Figure 1 gives a good idea on design of optimal parabolic reflectors. First,Dis
made as large as possible so that the physical aperture is maximized. Then the
F/Dratio that maximizes the aperture efficiency can be found from the above
graph. Note that the equation that relates the ratio ofF/Dto the angle can be
foundhere.
In the next section, we'll look at the radiation pattern of a parabolic antenna.
In this section, the 3d radiation patterns are presented to give an idea of what
they look like. This example will be for a parabolic dish reflector with the
diameter of the dishDequal to 11 wavelengths. TheF/Dratio will be 0.5. A
circular horn antenna will be used as the feed.
The maximum gain from the physical aperture is ; the
actual gain is 29.3 dB = 851, so we can conclude that the overall efficiency is
77%. The 3D patterns are shown in the following figures.
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As can be seen, the pattern is highly directional. TheHPBWis approximately 5
degrees, and thefront-to-back ratiois approximately 33 dB.
LENS ANTENNA.Another antenna that can change spherical waves into flat plane waves is thelens antenna. This antenna uses a microwave lens, which is similar to an optical lens to straighten the
spherical wavefronts. Since this type of antenna uses a lens to straighten the wavefronts, its design is
based on the laws of refraction, rather than reflection. Two types of lenses have been developedto provide a plane-wavefront narrow beam for tracking radars, while avoiding the problems
associated with the feedhorn shadow. These are the conducting(acceleration) type and
the dielectric (delay) type. The lens of an antenna is substantially transparent to microwave energy thatpasses through it. It will, however, cause the waves of energy to be either converged or
diverged as they exit the lens. Consider the action of the two types of lenses. The conducting type of lens
is illustrated in figure 1-10, view A. This type of lens consists of flat metal strips placed parallel to the
electric field of the wave and spaced slightly in excess of one-half of a wavelength. To the wave
these strips look like parallel waveguides. The velocity of phase propagation of a wave is greater in a
waveguide than in air. Thus, since the lens is concave, the outer portions of the transmitted
spherical waves are accelerated for a longer interval of time than the inner portion.
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Helical AntennaAntennas List Antenna Theory Home
Helix antennas have a very distinctive shape, as can be seen in the following
picture.
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Photo courtesy of Dr. Lee Boyce.
The most popular helical antenna (often called a 'helix') is a travelling wave
antenna in the shape of a corkscrew that produces radiation along the axis of thehelix. These helixes are referred to as axial-mode helical antennas. The benefits of
this antenna is it has a wide bandwidth, is easily constructed, has a real input
impedance, and can producecircularly polarizedfields. The basic geometry is
shown in Figure 1.
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Figure 1. Geometry of Helical Antenna.
The parameters are defined below.
D- Diameter of a turn on the helix.
C- Circumference of a turn on the helix (C=pi*D).
S- Vertical separation between turns.
- pitch angle, which controls how far the antenna grows in the z-direction per
turn, and is given by
N- Number of turns on the helix.
H- Total height of helix,H=NS.
The antenna in Figure 1 is a left handed helix, because if you curl your fingers on
your left hand around the helix your thumb would point up (also, the waves
emitted from the antenna are Left Hand Circularly Polarized). If the helix was
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wound the other way, it would be a right handed helical antenna.
The pattern will be maximum in the +z direction (along the helical axis in Figure
1). The design of helical antennas is primarily based on empirical results, and the
fundamental equations will be presented here.
Helices of at least 3 turns will have close to circular polarization in the +z
direction when the circumference Cis close to a wavelength:
Once the circumference Cis chosen, the inequalites above roughly determine the
operating bandwidth of the helix. For instance, if C=19.68 inches (0.5 meters),
then the highest frequency of operation will be given by the smallest wavelengththat fits into the above equation, or =0.75C=0.375 meters, which corresponds
to a frequency of 800 MHz. The lowest frequency of operation will be given by
the largest wavelength that fits into the above equation, or =1.333C=0.667
meters, which corresponds to a frequency of 450 MHz. Hence, thefractional BW
is 56%, which is true of axial helices in general.
The helix is a travelling waveantenna, which means the current travels along the
antenna and the phase varies continuously. In addition, the input impedance is
primarly real and can be approximated in Ohms by:
The helix functions well for pitch angles ( ) between 12 and 14 degrees.
Typically, the pitch angle is taken as 13 degrees.
The normalized radiation pattern for the E-field components are given by:
For circular polarization, the orthogonal components of the E-field must be 90
degrees out of phase. This occurs in directions near the axis (z-axis in Figure 1) of
the helix. Theaxial ratiofor helix antennas decreases as the number of loopsNis
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added, and can be approximated by:
The gain of the helix can be approximated by:
In the above, cis the speed of light. Note that for a given helix geometry
(specified in terms of C, S, N), the gain increases with frequency. For anN=10
turn helix, that has a 0.5 meter circumference as above, and an pitch angle of 13
degrees (giving S=0.13 meters), the gain is 8.3 (9.2 dB).
For the same example helix, the pattern is shown in Figure 2.
Figure 2. Normalized radiation pattern for helical antenna (dB).
The Half-Power Beamwidth for helical antennas can be approximated (in degrees)
by:
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Yagi-Uda AntennaAntennas List Antenna Theory .com
The Yagi-Udaantenna or Yagi is one of the most brilliant antenna designs. It is
simple to construct and has a highgain,typically greater than 10 dB. These
antennas typically operate in the HF to UHF bands (about 3 MHz to 3 GHz),
although theirbandwidthis typically small, on the order of a few percent of the
center frequency. You are probably familiar with this antenna, as they sit on top
of roofs everywhere. An example of a Yagi-Uda antenna is shown below.
The Yagi antenna was invented in Japan, with results first published in 1926. The
work was originally done by Shintaro Uda, but published in Japanese. The work
was presented for the first time in English by Yagi (who was either Uda's
professor or colleague, my sources are conflicting), who went to America and
gave the first English talks on the antenna, which led to its widespread use.
Hence, even though the antenna is often called a Yagi antenna, Uda probably
invented it. A picture of Professor Yagi with a Yagi-Uda antenna is shown below.
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In the next section, we'll explain the principles of the Yagi-Uda antenna.
The basic geometry of a Yagi-Uda antenna is shown in Figure 1.
Figure 1. Geometry of Yagi-Uda antenna.
The antenna consists of a single 'feed' or 'driven' element, typically adipoleor a
folded dipoleantenna. This is the only member of the above structure that is
actually excited (a source voltage or current applied). The rest of the elements
are parasitic - they reflect or help to transmit the energy in a particular
direction. The length of the feed element is given in Figure 1 asF. The feed
antenna is almost always the second from the end, as shown in Figure 1. This
feed antenna is often altered in size to make itresonantin the presence of the
parasitic elements (typically, 0.45-0.48 wavelengths long for a dipole antenna).
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The element to the left of the feed element in Figure 1 is the reflector. The
length of this element is given asRand the distance between the feed and the
reflector is SR. The reflector element is typically slightly longer than the feed
element. There is typically only one reflector; adding more reflectors improves
performance very slightly. This element is important in determining thefront-
to-back ratioof the antenna.
Having the reflector slightly longer than resonant serves two purposes. The first
is that the larger the element is, the better of a physical reflector it becomes.
Secondly, if the reflector is longer than its resonant length, the impedance of
the reflector will be inductive. Hence, the current on the reflector lags the
voltage induced on the reflector. The director elements (those to the right of the
feed in Figure 1) will be shorter than resonant, making them capacitive, so that
the current leads the voltage. This will cause a phase distribution to occur
across the elements, simulating the phase progression of a plane wave across
the array of elements. This leads to the array being designated as a travelling
wave antenna. By choosing the lengths in this manner, the Yagi-Uda antenna
becomes an end-fire array - the radiation is along the +y-axis as shown in
Figure 1.
The rest of the elements (those to the right of the feed antenna as shown in
Figure 1) are known as director elements. There can be any number of directors
N, which is typically anywhere fromN=1 toN=20 directors. Each element is of
lengthDi, and separated from the adjacent director by a length SDi. As alluded
to in the previous paragraph, the lengths of the directors are typically less than
the resonant length, which encourages wave propagation in the direction of the
directors.
The above description is the basic idea of what is going on. Yagi antenna
design is done most often via measurements, and sometimes computer
simulations. For instance, lets look at a two-element Yagi antenna (1 reflector,
1 feed element, 0 directors). The feed element is a half-wavelength dipole,
shortened to be resonant (gain = 2.15 dB). The gain as a function of the
separation is shown in Figure 2.
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Figure 2. Gain versus separation for 2-element Yagi antenna.
The above graph shows that the gain is increases by about 2.5 dB if the
separation SDis between 0.15 and 0.3 wavelengths. Similarly, the gain can be
plotted as a function of director spacings, or as a function of the number ofdirectors used. Typically, the first director will add approximately 3 dB of
overall gain (if designed well), the second will add about 2 dB, the third about
1.5 dB. Adding an additional director always increases the gain; however, the
gain in directivity decreases as the number of elements gets larger. For
instance, if there are 8 directors, and another director is added, the increases in
gain will be less than 0.5 dB.
In the next section, I'll go further into the design of Yagi-Uda antennas.
The design of a Yagi-Uda antenna is actually quite simple. Because Yagi antennas havebeen extensively analyzed and experimentally tested, the process basically follows this
outline:
Look up a table of design parameters for Yagi antennas
Build it (or model it numerically), and tweak it till the performance is acceptable
As an example, consider the table published in "Yagi Antenna Design" by P Viezbicke
from the National Bureau of Standards, 1968, given in Table I. Note that the "boom" is
the long element that the directors, reflectors and feed elements are physically attached to,
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and dictates the lenght of the antenna.
Table I. Optimal Lengths for Yagi-Uda Elements, for Distinct Boom Lengths
d=0.0085
SR=0.2
Boom Length of Yagi-Uda Array (in )
0.4 0.8 1.2 2.2 3.2 4.2
R 0.482 0.482 0.482 0.482 0.482 0.475
D1 0.442 0.428 0.428 0.432 0.428 0.424
D2 0.424 0.420 0.415 0.420 0.424
D3 0.428 0.420 0.407 0.407 0.420
D4 0.428 0.398 0.398 0.407D5 0.390 0.394 0.403
D6 0.390 0.390 0.398
D7 0.390 0.386 0.394
D8 0.390 0.386 0.390
D9 0.398 0.386 0.390
D10 0.407 0.386 0.390
D11 0.386 0.390
D12 0.386 0.390
D13 0.386 0.390
D14 0.386
D15 0.386
Spacing
between
directors,
(SD/ )
0.20 0.20 0.25 0.20 0.20 0.308
Gain (dB) 9.25 11.35 12.35 14.40 15.55 16.35
There's no real rocket science going on in the above table. I believe the authors of
the above document did experimental measurements until they found an
optimized set of spacings and published it. The spacing between the directors is
uniform and given in the second-to-last row of the table. The diameter of the
elements is given by d=0.0085 . The above table gives a good starting point to
estimate the required length of the antenna (the boom length), and a set of lengths
and spacings that achieves the specified gain. In general, all the spacings, lengths,
diamters (including the boom diameter) are design variables and can be
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continuously optimized to alter performance. There are thousands of tables that
further give results, such as how the diamter of the boom affects the results, and
the optimal diamters of the elements.
As an example of Yagi-antenna radiation patterns, a 6-element Yagi antenna (with
axis along the +x-axis) is simulated in FEKO (1 reflector, 1 driven half-
wavelength dipole, 4 directors). The resulting antenna has a 12.1 dBi gain, and the
plots are given in Figures 1-3.
Figure 1. E-plane gain of Yagi antenna.
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Figure 2. H-Plane gain of Yagi antenna.
Figure 3. 3-D Radiation Pattern of Yagi antenna.
The above plots are just an example to give an idea of what the radiation pattern
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of the Yagi-Uda antenna resembles. The gain can be increased (and the pattern
made more directional) by adding more directors or optimizing spacing (or rarely,
adding another refelctor). Thefront-to-back ratiois approximately 19 dB for this
antenna, and this can also be optimized if desired.
A LONG-WIRE ANTENNAis an antenna that is a wavelength or more long at the operating frequency.These antennas have directive patterns that are sharp in both the horizontal and vertical planes.
BEVERAGE ANTENNASconsist of a single wire that is two or more wavelengths long.
A V ANTENNAis a bi-directional antenna consisting of two horizontal, long wires arranged to form a V.
The RHOMBIC ANTENNAuses four conductors joined to form a rhombus shape. This antenna has a
wide frequency range, is easy to construct and maintain, and is noncritical as far as operation and
adjustment are concerned.
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The TURNSTILE ANTENNAconsists of two horizontal, half-wire antennas mounted at right angles to
each other.
LOG-PERIODIC ANTENNALOG-PERIODIC ANTENNA
Intelecommunication,a log-periodic antenna(LP,
also known as a log-periodicarray) is abroadband,multielement,
unidirectional,narrow-beamantennathat hasimpedanceand
radiationcharacteristics that are regularly repetitive as a
logarithmic function of the excitationfrequency.The individual
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components are oftendipoles,as in a log-periodic dipole array
(LPDA).
Log periodic antennas are arrays that are designed to be
self-similarand thus arefractal antennaarrays. It is normal to
drive alternating elements with a circa180o ( radian) phase shiftfrom the last element. This is normally done by wiring the
elements alternatingly to the two wires in a balanced transmission
line.The length and spacing of the elements of a log- increase
logarithmically from one end to the other.The result of this
structural condition is that if a plot is made of the input impedance
as a function of log of frequency then the variation will be periodic
i.e. the impedance will go through the cycles of variation in such a
way that each cycle is exactly like its preceding one and hence thename.
Log.-Periodic Antenna, 2502400 MHz
Mutual impedance& self-impedanceThe method helps us to compute voltages, currents and
impedances in antenna systems. The method understands the
voltage, which is observed at the input port of every single
antenna element, being induced by the radiation of allthe
antenna elements (including the own element). The voltage
can be composed from contributions of single elements. Each
contribution is proportional to the current of the respective
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element. E.g., voltage U1 at the input of the first antenna
element equals to the summation
whereI1,I2,I3 are currents at the input ports of singleelements,Z11,Z12,Z13 are impedances.Z11 is self-impedance,Z1n are mutual impedances between the first
element and the other elements in the antenna system. These
impedances depend on the mutual position and mutual
distance of antenna elements
Biconical antenna
A biconical antennaconsists of an arrangement of twoconicalconductors,which is
driven bypotential,charge,or an alternatingmagnetic field(and the associatedalternating electric current)at thevertex.The conductors have a commonaxisand vertex.The two cones face in opposite directions. Biconical antennas are broadband dipole
antennas, typically exhibiting a bandwidth of 3octavesor more.
Omnidirectional Biconical Antenna
Microstrip or patch antennas are becoming increasingly useful because they can
be printed directly onto a circuit board. They are becoming very widespread
within the mobile phone market. They are low cost, have a low profile and areeasily fabricated.
Consider the microstrip antenna shown in Figure 1, fed by a microstrip
transmission line. The patch, microstrip and ground plane are made of high
conductivity metal. The patch is of lengthL, width W, and sitting on top of a
substrate (some dielectric circuit board) of thickness hwithpermittivity .
The thickness of the ground plane or of the microstrip is not critically
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important. Typically the height his much smaller than the wavelength of
operation.
(a) Top View
(b) Side View
Figure 1. Geometry of Microstrip (Patch) Antenna.
The frequency of operation of the patch antenna of Figure 1 is determined by
the lengthL. The center frequency will be approximately given by:
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The above equation says that the patch antenna should have a length equal to
one half of a wavelength within the dielectric (substrate) medium.
The width Wof the antenna controls the input impedance. For a square patch
fed in the manner above, the input impedance will be on the order of 300
Ohms. By increasing the width, the impedance can be reduced. However, todecrease the input impedance to 50 Ohms often requires a very wide patch. The
width further controls the radiation pattern. The normalized pattern is
approximately given by:
In the above, kis the free-spacewavenumber,given by . The magnitudeof the fields, given by:
The fields are plotted in Figure 2 for W=L=0.5 .
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Figure 2. Normalized Radiation Pattern for Microstrip (Patch) Antenna.
The directivity of patch antennas is approximately 5-7 dB. The fields are
linearly polarized. Next we'll consider more aspects involved in Patch
(Microstrip) antennas.
Spiral antenna
Inmicrowavesystems, a spiral antennais a type of RFantenna.It is shaped as a two-
armspiral,or more arms may be used.[1]
Spiral antennas operate over a widefrequency
rangeand have circularpolarization.Spiral antennas were first described in 1956.
Applications
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A spiral antenna transmits EM waves having a circular polarization. It will receive
linearly polarized EM waves in any orientation, but will attenuate signals received with
the opposite circular polarization. A spiral antenna will reject circularly polarized wavesof one type, while receiving perfectly well waves having the other polarization.
One application of spiral antennas is wideband communications. Another application ofspiral antennas is monitoring of the frequency spectrum. One antenna can receive over a
wide bandwidth, for example a ratio 5:1 between the maximum and minimum frequency.
Usually a pair of spiral antennas are used in this application, having identical parametersexcept the polarization, which is opposite (one is right-hand, the other left-hand oriented).
Spiral antennas are useful for microwave direction-finding.[2]
Elements
The antenna includes two conductive spirals or arms, extending from the center outwards.
The antenna may be a flat disc, with conductors resembling a pair of loosely-nested clock
springs, or the spirals may extend in a three-dimensional shape like a screw thread. Thedirection of rotation of the spiral defines the direction of antenna polarization. Additional
spirals may be included as well, to form a multi-spiral structure. Usually the spiral is
cavity-backed, that is there is a cavity of air or non-conductive material or vacuum,surrounded by conductive walls; the cavity changes the antenna pattern to a
unidirectional shape. The output of the antenna
Measuring Radiation Pattern
and an Antenna's Gain
Antennas (Home)Antenna Measurements
HomePrevious: Measurements
Ranges
Now that we have ourmeasurement equipmentand anantenna range,we can
perform some measurements. We will use the source antenna to illuminate the
antenna under test with a plane wave from a specific direction. Thepolarization
andgain(for the fields radiated toward the test antenna) of the source antenna
should be known.
Due to reciprocity, the radiation pattern from the test antenna is the same for boththe receive and transmit modes. Consequently, we can measure the radiation
pattern in the receive mode for the test antenna.
The test antenna is rotated using the test antenna's positioning system. The
received power is recorded at each position. In this manner, the magnitude of the
radiation patternof the test antenna can be determined. We will discussphase
measurementsandpolarization measurementslater.
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The coordinate system of choice for the radiation pattern isspherical coordinates.
Measurement Example
An example should make the process reasonably clear. Suppose the radiation
pattern of amicrostrip antennais to be obtained. As is usual, lets let the direction
the patch faces ('normal' to the surface of the patch) be towards the z-axis.
Suppose the source antenna illuminates the test antenna from +y-direction, as
shown in Figure 1.
Figure 1. A patch antenna oriented towards the z-axis with a Source illumination
from the +y-direction.
In Figure 1, the received power for this case represents the power from the angle:
. We record this power, change the position and record again.
Recall that we only rotate the test antenna, hence it is at the same distance from
the source antenna. The source power again comes from the same direction.
Suppose we want to measure the radiation pattern normal to the patch's surface(straight above the patch). Then the measurement would look as shown in Figure
2.
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Figure 2. A patch antenna rotated to measure the radiation power at normal
incidence.
In Figure 2, the positioning system rotating the antenna such that it faces the
source of illumination. In this case, the received power comes from direction
. So by rotating the antenna, we can obtain "cuts" of the radiationpattern - for instance theE-planecut or theH-planecut. A "great circle" cut is
when =0 and is allowed to vary from 0 to 360 degrees. Another common
radiation pattern cut (a cut is a 2d 'slice' of a 3d radiation pattern) is when is
fixed and varies from 0 to 180 degrees. By measuring the radiation pattern
along certain slices or cuts, the 3d radiation pattern can be determined.
It must be stressed that the resulting radiation pattern is correct for a given
polarization of the source antenna. For instance, if the source is horizontally
polarized (seepolarization of plane waves), and the test antenna is vertically
polarized, the resulting radiation pattern will be zero everywhere. Hence, theradiation patterns are sometimes classified as H-pol (horizontal polarization) or
V-pol (vertical polarization). See alsocross-polarization.
In addition, the radiation pattern is a function of frequency. As a result, the
measured radiation pattern is only valid at the frequency the source antenna is
transmitting at. To obtain broadband measurements, the frequency transmitted
must be varied to obtain this information.
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Measuring Gain
Antennas (Home) Antenna Measurements
Back: Measurement of
Antenna Radiation
Patterns
On the previous page onmeasuring radiation patterns,we saw how the radiation
pattern of an antenna can be measured. This is actually the "relative" radiation
pattern, in that we don't know what the peak value of thegainactually is (we're
ust measuring the received power, so in a sense can figure out how directive an
antenna is and the shape of the radiation pattern). In this page, we will focus on
measuring the peak gain of an antenna - this information tells us how much power
we can hope to receive from a given plane wave.
We can measure the peak gain using theFriis Transmission Equationand a "gainstandard" antenna. A gain standard antenna is a test antenna with an accurately
known gain and polarization (typically linear). The most popular types of gain
standard antennas are thethin half-wave dipole antenna(peak gain of 2.15 dB)
and thepyramidal horn antenna(where the peak gain can be accurately calculated
and is typically in the range of 15-25 dB). Consider the test setup shown in Figure
1. In this scenario, a gain standard antenna is used in the place of the test antenna,
with the source antenna transmitting a fixed amount of power (PT). The gains of
both of these antennas are accurately known.
Figure 1. Record the received power from a gain standard antenna.
From the Friis transmission equation, we know that the power received (PR) is
given by:
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If we replace the gain standard antenna with our test antenna (as shown in Figure
2), then the only thing that changes in the above equation is GR- the gain of thereceive antenna. The separation between the source and test antennas is fixed, and
the frequency will be held constant as well.
Figure 2. Record the received power with the test antenna (same source antenna).
Let the received power from the test antenna bePR2. If the gain of the test
antenna is higher than the gain of the "gain standard" antenna, then the receivedpower will increase. Using our measurements, we can easily calculate the gain of
the test antenna. Let Ggbe the gain of the "gain standard" antenna,PRbe the
power received with the gain antenna under test, andPR2be the power received
with the test antenna. Then the gain of the test antenna (GT) is (in linear units):
The above equation uses linear units (non-dB). If the gain is to be specified indecibels,(power received still in Watts), then the equation becomes:
And that is all that needs done to determine the gain for an antenna in a particular
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direction.
Efficiency and Directivity
Recall that thedirectivitycan be calculated from the measured radiation pattern
without regard to what the gain is. Typically this can be performed byapproximated the integral as a finite sum, which is pretty simple.
Recall that theefficiencyof an antenna is simply the ratio of the peak gain to the
peak directivity:
Hence, once we have measured the radiation pattern and the gain, the efficiencyfollows directly from these.
In the next section, we'll look at measuring the phase of an antenn