Antenna Engineering for Mte

7/28/2019 Antenna Engineering for Mte

1/147

INTRODUCTIONAntenna or Aerial :

- is a transducer that transmits or receives

electromagnetic waves

- converts the voltage and current into the

electromagnetic radiation and vice-versa

- is a transitional structure between free-space and a

(Transmission Line) guiding structure

- The American Heritage Dictionary:A metallic

apparatus for sending and receiving electromagnetic

waves.

- Websters Dictionary:A usually metallic device (as a

rod or wire) for radiating or receiving radio waves


2/147

INTRODUCTION

What is an Antenna?

An antenna is a device for radiating and receiving radiowaves. The antenna is the transitional structure betweenfree-space and a guiding device.


3/147

INTRODUCTION

A transmission-line Thevenin equivalent of the antennasystem


4/147

INTRODUCTION

A transmission-line Thevenin equivalent of the antennasystem


5/147

.


6/147

. 1. Low loss line

2.reduce RL

ZL=ZA

INTRODUCTION


7/147

TYPES OF ANTENNAS

Wire antennas

Aperture antennas

Microstrip antennas

Array antennas

Reflector antennas Lens antennas


8/147

Wire antennas

seen virtually everywhere- on automobile,

building, ships, aircraft, and so on. Shapes of wire antennas:

straight wire (dipole), loop (circular), and helix,

Loop antenna may take the shape of a rectangle ,

ellipse or any other shape configuration


9/1479

Aperture-antenna

Note: The aperture concept is applicable also to wired antennas.

For instance, the max effective aperture of linear/2

wavelength dipole antenna is 2/8

EM wave

Power

absorbed: P [watt]Effective

aperture: A[m2]

Aperture antennas derivedfrom waveguide technology

(circular, rectangular)

Can transfer high power

(magnetrons, klystrons)

Utilization of higherfrequencies

Applications: aircraft, and spacecraft


10/147

Microstrip antenna

consist of metallic patch on a grounded substrate

Examples: rectangular and circular shapeApplications: aircraft, spacecraft, satellite, missiles,

cars etc

RECTANGLE

CIRCLE


11/147

Patch Antennas Radiation is from two slots on left and right edges of patch where slot is

region between patch and ground plane

Length d = /r1/2 Thickness typically 0.01 The big advantage is conformal, i.e. flat, shape and low weight

Disadvantages: Low gain, Narrow bandwidth (overcome by fancy shapes and

other heroic efforts), Becomes hard to feed when complex, e.g. for wide

band operation


12/147

Patch Antenna Pattern


13/147

Array antennasa collection of simple antennas

- gives desire d radiation characteristics

- The arrangement of the array may be such that the radiation from the

elements adds up to give a radiation maximum in a particular

direction or directions, minimum in others, or otherwise as desired

- Examples: yagi-uda array, aperture array, microstrip patch array,

slotted waveguide array


14/147

Array of patch Antennas


15/147

Reflector antennas

- used in order to transmit and receive signals that had to travel

millions of miles

- A very common reflector antenna parabolic reflector


16/147

Parabolic Reflectors A parabolic reflector operates

much the same way a reflectingtelescope does

Reflections of rays from the feedpoint all contribute in phase to aplane wave leaving the antenna

along the antenna bore sight(axis)

Typically used at UHF andhigher frequencies

L t


17/147

Lens antennas lenses are primarily used to collimate incident divergent energy to

prevent it from spreading in undesired directions

Transform various forms of divergent energy into plane waves

Used in most of applications as are the parabolic reflectors,

especially at higher frequencies. Their dimensions and weight

bec0me exceedingly large at lower frequencies.


18/147

18

Lens antennas

Lenses play a similar role to that of reflectors in reflector antennas:

they collimate divergent energyOften preferred to reflectors at frequencies > 100 GHz.


19/147

PHYSICAL CONCEPT OF RADIATION

or RADIATION MECHANISMHow is Radiation Accomplished?

Principle of radiationWhen electric charges undergo acceleration or deceleration,

electromagnetic radiation will be produced. Hence it is the

motion of charges (i.e., currents) that is the source of radiation

basic equation of radiation

IL = Qv

Where

Itime varying current

Qcharge

Llength of current element

vtime change of velocity

Radiation Mechanism in a) Single wire, b) Two wire and c) Dipole


20/147

Radiation Mechanism

Single wire:

Conducting wires are characterized by the motion ofelectric charges and the

creation of current flow.electric volume charge density, qv (coulombs/m3),

is distributed uniformly in a

circular wire of cross-sectional area A

and

volume V

qv - volume charge density

A- cross-sectional area

V-Volume


21/147

Radiation Mechanism Single wire:

Instead of examining all three current densities, we will primarily

concentrate on the very thin wire.

The conclusions apply to all three. If the current is time varying.


22/147

Radiation Mechanism


23/147

Radiation Mechanism

Thin wire


24/147

Radiation Mechanism Single wire:

CURVED

BENT DISCONTINUOUS

TERMINATED

TRUNCATED


25/147

Radiation MechanismTwo-Wires:

Applying a voltage across the two-conductor transmission line

creates an electric field between the conductors. The movement of the charges creates a current that in turn

creates a magnetic field intensity.

The creation of time-varying electric and magnetic fields between

the conductors forms electromagnetic waves which travel along

the transmission line.

Voltage creates electric field

Current that produced produces Magnetic field

Together that forms Electro Magnetic Waves that travels along the

transmission line


26/147


The electromagnetic waves enter the antenna and have

associated with them electric charges and correspondingcurrents.

If we remove part of the antenna structure, free-space waves can

be formed by connecting the open ends of the electric lines

If we remove the antenna then in free space it will be like this bcoz they

are actually electromagnetic waves


27/147


If the initial electric disturbance by the source is of a short duration,

the created electromagnetic waves travel inside the transmission

line, then into the antenna, and finally are radiated as free-space

waves, even if the electric source has ceased to exist.

They radiate in free space atleast once evn if the elect field get ceased

If the electric disturbance is of a continuous nature, electromagneticwaves exist continuously and follow in their travel behind the others.

pattern will follow one after another

However, when the waves are radiated, they form closed loops and

there are no charges to sustain their existence.

No electrical presence since they forms closed loop

Electric charges are required to excite the fields but are not needed

to sustain them and may exist in their absence.

Electric field is required to excite not to continue or sustain the field


28/147

Radiation MechanismDipole Antenna:

A radio antenna that can be made of a simple wire, with a

centre-fed driven element

Consist of two metal conductors of rod or wire,

oriented parallel and collinear

with each other (in line with each other), Small Space

with a small space between them.

Consider the example of a small dipole antenna where the

time of travel is negligible

Driven Element


29/147

Radiation MechanismFormation and detachment of electric field line for short Dipole Antenna

T=T/4,T/2,T/2+

Di l


30/147

Dipole


31/147

Current Distribution on a thin wire antenna

Let us consider the geometry of a lossless two-wire

transmission line

The movement of the charges creates a traveling wave

current, of magnitude I0 /2, along each of the wires.

When the current arrives at the end of each of the wires,

it undergoes a complete reflection (equal magnitude and

180 phase reversal)

The reflected traveling wave, when combined with the

incident traveling wave, forms in a each wire a pure

standing wave pattern of sinusoidal form.


32/147

current = I/2+I/2

reflected and 180 phase reversal

incidented wave forms standing waves

b h


33/147

Current Distribution on a thin wire antenna

For the two-wire balanced (symmetrical) transmission line, thecurrent in a half-cycle of one wire is of the same magnitude but 180

out-of-phase from that in the corresponding half-cycle of the

otherwire

Current same but 180 out of phase

b h


34/147

Current Distribution on a thin wire antenna If s is also very small, the two fields are canceled

The net result is an almost ideal, non-radiating transmission line.

When the line is flared, because the two wires of the flared section

are not necessarily close to each other, the fields do not cancel each

other

Therefore ideally there is a net radiation by the transmission linesystem

C Di ib i hi i


35/147

Current Distribution on a thin wire antenna When the line is flared into a dipole, if s not much less than , the

phase of the current standing wave pattern in each arm is the same

through out its length. In addition, spatially it is oriented in the same

direction as that of the other arm

Thus the field s radiated by the two arms of the dipole (vertical parts

of a flared transmission line) will primarily reinforce each other

toward most directions of observation

C Di ib i hi i


36/147

Current Distribution on a thin wire antenna The current distributions we have seen represent the maximum

current excitation for anytime. The current varies as a function of time

as well.

T=T/8,T/4,T/2,T

R di ti tt


37/147

Radiation pattern

Mathematical function or Graphical representation of radiation

properties of an antenna as a function of space coordinates.

Radiation properties include power flux density, radiation intensity,field strength, directivity, phase or polarization.

(RIFSD PHASE)

Radiation pattern usually indicate either electric field intensity or

power intensity. Magnetic field intensity has the same radiation

pattern as the electric field intensity

A directional antenna radiates and receives preferentially in some

direction

Depicted as two or three-dimensional spatial distribution ofradiated energy as a function of the observers position along a

path or surface of constant radius

Lobes are classified as: major, minor, side lobes, back lobes

R di ti tt


38/147

Radiation pattern

Coordinate system for antenna analysis

Graphical representation of radiation properties of an antenna

R di ti tt


39/147

Radiation pattern

For an antenna

The Field pattern(in linear scale):

typically represents a plot ofthe magnitude of the electric or

magnetic field as a function of the angular space.

The Power pattern(in linear scale):

typically represents a plot of the square of the magnitude of theelectric or magnetic field as a function of the angular space

The Power pattern(in dB):

represents the magnitude of the electric or magnetic field, in

decibels, as a function of the angular space.


40/147

Radiation pattern

HPBW(FIELD,

POWER,DB )

R di ti tt


41/147

Radiation pattern

various parts of a radiation pattern are referred to as a lobes

Total electric fieldis given as

Three dimensional polar pattern

R di ti tt


42/147

Radiation pattern

various parts of a radiation pattern are referred to as a lobes

Two dimensional polar pattern

Radiation pattern lobes


43/147

Radiation pattern lobes

Various parts of a radiation pattern are referred to as lobes

Major lobe (main lobe):

The radiation lobe containing the direction of maximum

radiation

Major lobe is pointing at =0 direction in figure

In spilt-beam antennas, there may exist more than one

major lobes

Minor Lobe is any lobe except a major lobe

all the lobes exception of the major lobe

Side lobe: a radiation lobe in any direction other than intended lobe

Usually it is adjacent to main lobe

Back lobe:

a radiation lobe whose axis makes an angle of

approximately 1800 with respect to the beam of antenna

usually it refers to a minor lobe that occupies the

hemisphere in a direction opposite to that of major lobe

R di ti P D it


44/147

Radiation Power Density

Poynting Vector or Power density(w)

The instantaneous poynting vector describe the power

associated with electromagnetic wave

Poynting vector defined as

W = E x H

W- instantaneous poynting vector (W/m2)

E- instantaneous electric field intensity (V/m)H-instantaneous magnetic field intensity (A/m)

R di ti P D it


45/147

Radiation Power Density The total power crossing a closed surface can be obtained by

integrating the normal component of poynting vector over the entire

surface.

p= instantaneous total power (W)

n = unit vector normal to the surfaceda = infinitesimal are a of the closed surface (m2 )

we define the complex fields E and H which are related to theirinstantaneous counter parts Eand Hby

R di ti P D it


46/147

Radiation Power Densityidentity

W = E x H =The first term of is not a function of time, and the time variations of the

second are twice the given frequency.

Average Power Density:

The average power density is obtained by integrating the

instantaneous Poynting vector over one period and dividingby the period.

Wav=the real part of represents the average (real) power densitythe imaginary

part Must represent the reactive (stored) power density associated with the

electromagnetic fields

Radiation Po er Densit


47/147

Radiation Power DensityThe average power radiated by an antenna (radiated power)

can be written as

Radian and Steradian


48/147

Radian and Steradian

A radian is defined with the using Figure ( a)

It is the angle subtended by an arc along the

perimeter of the circle with length equal tothe radius.

A steradian may be defined using Figure (b)

Here, one steradian (sr) is subtended by an

area r2 at the surface of a sphere of radius r.

The infinitesimal area dA on the surface of

radius r is defined as

dA =r2 sin d d (m2)

A differential solid angle, d, in sr, is given

by

d = dA/r

2

= sin d d (sr)= sin d d

Unit of plane Angle is a radian

Unit of Solid Angle is a steradian

Isotropic antenna


49/147

Isotropic antenna Isotropic antenna orisotropic radiatoror

isotropic source oromnidirectional radiatororsimple unipole

is a hypothetical (not physically realizable)lossless antenna having equal radiation in all

directions

used as a useful reference antenna todescribe real antennas.

Its radiation pattern is represented by a

sphere of radius (r) whose center coincides

with the location of the isotropic radiator.

All the energy(power) must pass over the

surface area of sphere=4r2

Isotropic antenna


50/147

Isotropic antenna Poynting vector or power density(w) at any point on the sphere

power radiated per unit area in any direction

The magnitude of the poynting vector is equal to the radial componentonly(because p = p=0)

|w|=wr

The total radiated power

PTrad = w.ds

= wr.ds= wrds

= wr4r2

or wr= PTrad /4r2 watt/m2

where

Wr radiated power of average power density

PTrad total power radiated

Isotropic antenna


51/147

Isotropic antenna The total power radiated by it is given by:

The power density is given by:

which is uniformly distributed over the surface of a sphere of radius r.

Isotropic means ALL OVER THE SURFACE THEREFORE SS ds =

4 |=| R^2

0 ---- 2pi and 0 ---- pi

a^r r^2 sinx dx dphi

Isotropic antenna


52/147

Isotropic antenna

g

Directional antenna


53/147

Directional antenna

is an antenna, which radiates (or receives) much more

power in (or from) some directions than in (or from) others

RECEIVES OR RADIATES IN SOME SPECIFIED

DIRECTION ONLY

Note:

Usually, this term is applied to antennas whosedirectivity is much higher than that of a half-wave dipole

Principal Patterns


54/147

For linearly polarized antenna performance is often described

in terms of its principal E-and H-Plane patterns

E- Plane : the plane containing the electric field vector and the

maximum radiationH- Plane : the plane containing the magnetic field vector and the

maximum radiation x-z elevation plane contain principal E- planex-y azimuthal plane contain principal H- plane

Principal Patterns

Principal E and H plane pattern for a pyramidal horn antenna

Field Regions


55/147

The space surrounding an antenna is usually subdivided into three

regions:

Field Regions

DISTIBUTION)


56/147


regions:

Reactive near-field region:That portion of the near-field region

immediately surrounding the antenna wherein the reactive field

predominates.

Radiating near-field (Fresnel) region:That region of the field of an

antenna between the reactive near-field region and the far-field region

wherein radiation fields predominate and wherein the angular field

distribution is dependent upon the distance from the antenna

Far-field (Fraunhofer) region:That region of the field of an antenna

where the angular field distribution is essentially independent of the

distance from the antenna.

DISTIBUTION)

Field Regions


57/147


regions:

Field Regions

Radiation Intensity


58/147

Radiation intensity in a given direction is defined as the power

radiated from an antenna per unit solid angle.

U = Prad/d

Where

Pradradiated power

=d solid angel

The radiation intensity is a far-field parameter, and it can be obtainedby simply multiplying the radiation density by the square of the

distance.

U = r2WradWrad radiation density (W/m

2)

r distance (m)U - radiation intensity (W/ unit solid angle)

Radiation Intensity

Radiation Intensity


59/147

The radiation intensity is also related to the far-zone electric field of

an antenna, by

The total power is obtained by integrating the radiation intensity,

over the entire solid angle of 4. Thus

Radiation Intensity

Radiation Intensity


60/147

Radiation patterns may be functions of both spherical coordinate

angles and

Let the radiation intensity of an antenna be of the form

The maximum value of radiation intensity

The total radiated power is found using

Radiation Intensity

DirectivityDi ti it (D)


61/147

yDirectivity (D):

the ratio of the radiation intensity in a given direction from the antenna to

the radiation intensity averaged over all directions

the directivity of a nonisotropic source is equal to the ratio of its radiation

intensity in a given direction over that of isotropic source

The average radiation intensity (U0) is equal to the total power radiated by

the antenna divided by 4.

If the direction is not specified, it implies the direction of maximum radiation

intensity (maximum directivity) expressed as

U = radiation intensity (W/unit solid angle)

Umax = maximum radiation intensity (W/unit solid angle)

U0= radiation intensity of isotropic source (W/unit solid angle)

Prad = total radiated power (W)

D = directivity(dimensionless)

D0= maximumdirectivity(dimensionless)

Directivity


62/147

yThe general expression for the directivity and maximum

directivity (D0) using

Directivity


63/147

Directivity

,,

,

n

n avg

P

PD

The directive gain,, of an antenna is the ratio of the

normalized power in a particular direction to the

average normalized power, or

max

max max

,

,,

n

n avg

PD D

P

The directivity, Dmax, is the maximum directive gain,

max

4

p

D

Directive gain

,

,4

n p

n avg

P dP

d

Where the normalized powers average value taken

over the entire spherical solid angle is

max

1,nP Using

Directivity


64/147

Partial Directivity of antenna:

Partial directivity of an antenna for a given polarization in a given direction as

that part of the radiation intensity corresponding to a given polarization

divided by the total radiation intensity averaged over all directions.

With this definition for the partial directivity, then in a given direction

the total directivity is the sum of the partial directivities for any two

orthogonal polarizations

For a spherical coordinate system, the total maximum directivity D0 for theorthogonal and components of an antenna can be written as

While the partial directivities D and D are expressed as

Directivity


65/147

Directional Patterns:

In Figure2.14(a). For a rotationally symmetric pattern, the half-power beam widths in

any two perpendicular planes are the same, as illustrated in Figure2.14(b).With this approximation, maximum directivity can be approximated by

Directivity


66/147

Directional Patterns:

With this approximation, maximum directivity can be approximated by

Antenna Gain


67/147

Antenna Gain The ratio of the intensity, in a given direction, to the radiation

intensity that would be obtained if the power accepted by the

antenna were radiated isotropically

The radiation intensity corresponding to the isotropically

radiated power is equal to the power accepted (input) by the

antenna divided by 4

In equation form this can be expressed as

Antenna Gain


68/147

Antenna Gainthe ratio of the Power gain in a given direction to the power

gain of a reference antenna in its referenced direction

The power input must be the same for both antennas

Mostly Reference antenna is a lossless isotropic source. Thus

When the direction is not stated, the power gain is usually taken in

the direction of maximum radiation.

We can write that the total radiated power related to the total input

power

Antenna Gain


69/147

Antenna Gain

Antenna Gain


70/147

Antenna GainPartial gain of an antenna

For a given polarization in a given direction

Total gain

A t G i


71/147

Antenna Gain

Relationship between antenna gain and effective area

G = antenna gain

Ae= effective area f= carrier frequency

c = speed of light (3x108 m/s)

= carrier wavelength

2

2

2

44

c

AfAG ee

Antenna Efficiency


72/147

Antenna Efficiency

In general, the over all

Efficiency can be written as

Radiation Resistance & Antenna Efficiency


73/147

Radiation Resistance & Antenna Efficiency

Radiation resistance (Rrad) is a fictitious resistance,

such that the average power flow out of the antenna isPav = (1/2) I2 Rrad

Using the equations for our short (Hertzian) dipole we find that

Rrad = 80 2 (l/)2 ohms

Antenna Efficiency

o = Rrad/(Rrad+ Rloss)

where Rloss ohmic losses as heat

Gain = ox Directivity

G =o D

Beamwidth


74/147

Half-power beamwidth (HPBW) (H)

is the angle between two vectors from the patterns origin to the

points of the major lobe where the radiation intensity is half itsmaximum

Often used to describe the antenna resolution properties

Important in radar technology, radioastronomy, etc.

Power pattern of U()=

First-null beamwidth (FNBW) (N)

is the angle between two vectors, originating at the patterns origin

and tangent to the main beam at its base.

Often FNBW 2*HPBW

Beam efficiency


75/147

Beam efficiency

To judge the quality of transmitting and receiving antennas

If 1 is chosen as the angle where the first null or minimum

occurs, then the beam efficiency will indicate the amount of

power in the major lobe compared to the total power.

Bandwidth


76/147

Bandwidth: the range of frequencies within which the performance of

the antenna, with respect to some characteristic, conforms to a

specified standard

For broadband antennas, the bandwidth is usually expressed as the

ratio of the upper-to-lower frequencies of acceptable operation

F.E. 10:1 bandwidth indicates that the upper frequency is 10 times

greater than the lower

For narrowband antennas, the bandwidth is expressed as a

percentage of the frequency difference (upper minus lower) over the

center frequency of the bandwidth

F.E. a 5% bandwidth indicates that the frequency difference of

acceptable operation is 5% of the center frequency of the

bandwidth

gain, side lobe level,

beamwidth,

polarization, and

beam direction

Pattern

bandwidth

inputimpedance andradiationefficiency

Impedancebandwidth

Polarization


77/147

Polarization of an antenna:

the polarization of the wave transmitted (radiated) by the antenna

When the direction is not stated, the polarization is taken to be

the polarization in the direction of maximum gain

Polarization of the radiated energy varies with the direction from

the center of the antenna, so that different parts of the pattern

may have different polarizations

Polarization may be classified as linear, circular, or elliptical

Polarization


78/147

Polarization of a radiated wave

is defined as that property of an electro magnetic wave

describing the time varying direction and relative magnitude ofthe electric-field vector; specifically, the figure traced as a

function of time by the extremity of the vector at a fixed location

in space, and the sense in which it is traced, as observed along

the direction of propagation.

Polarization then is the curve traced by the end point of the

arrow (vector) representing the instantaneous electric field. The

field must be observed along the direction of propagation. A

typical trace as a function of time is shown in Figure

Polarization of EM Waves


79/147

Clockwise rotation of the E vector= right-hand polarization

counterclockwise rotation of the E vector = left-hand

polarization



80/147


Horizontal polarization

Vertical polarization

Circular polarization

(RCP)

Circular polarization

(LCP)



81/147

AR: The ratio of the major axis to the minor axis is referred to as the axial ratio (AR)

,and it is equal to

Polarization Electromagnetic wave


82/147

Polarization Electromagnetic wave



83/147


The instantaneous field of a plane wave, traveling in the

negative z direction:

Instantaneous components are related to their complexcounterparts by

where Exo and Eyo are, respectively, the maximum magnitudesof the x and y components.

Linear Polarization:


84/147

A time-harmonic wave is linearly polarized at a given point in

space if the electric-field (or magnetic-field) vector at that point

is always oriented along the same straight line at every instantof time.

This is accomplished if the field vector (electric or magnetic)

possesses:

Only one component, or

Two orthogonal linear components that are in time phase or 180

(or multiples of 180) out-of-phase.

the time-phase difference between the two components mustbe

linearly polarized plane waves


85/147

linearly polari ed plane waves

)(tan

)cos(e)cos(e

0

01

2

0

2

0

00

x

y

yx

yyxx

E

E

EEEE

kztEkztEE

Any two orthogonal plane waves

Can be combined into a linearly

Polarized wave.

Conversely, any arbitrary linearlypolarized wave can be resolved

into two independent Orthogonal

plane waves that are in phase.

[2-15]

Circular Polarization:


86/147

C cu a o a at o : A time-harmonic wave is circularly polarized at a given point in

space if the Electric (or magnetic) field vector at that point

traces a circle as a function of time

The necessary and sufficient conditions to accomplish this are ifthe field vector (electric or magnetic) possesses all of thefollowing:

a. The field must have two orthogonal linear components,and

b. The two components must have the same magnitude, and

c. The two components must have a time-phase difference ofodd multiples of 90.



87/147


magnitudes of the two

components are same

the time-phase difference

between components is odd

multiples of /2

Circular Polarized wave:


88/147

polarizedcircularlyleft:-polarized,circularlyright:

2&:onpolarizatiCircular 000

EEE yx[2-17]

Optical Fiber communications, 3rd ed.,G.Keiser,McGrawHill, 2000

Elliptical Polarization:


89/147

A time-harmonic wave is elliptically polarized if the tip

of the field vector (electric or magnetic) traces an

elliptical locus in space.

At various instants of time the field vector changes

continuously with time at such a manner as to

describe an elliptical locus.

It is right-hand (clockwise) elliptically polarized if the

field vector rotates clockwise, and it is left-hand

(counterclockwise) elliptically polarized if the fieldvector of the ellipse rotates counterclockwise



90/147

magnitudes of the two components are NOT same the

time-phase difference between components is odd

multiples of /2

Or when the time phase difference between the two

components is not equal to multiples of /2

(irrespective of their magnitudes)



91/147

The necessary and sufficient conditions

The field must have two orthogonal linear components, and

The two components can be of the same or different

magnitude

(1) If the two components are not of the same magnitude, thetime-phase difference between the two components must not

be 0 or multiples of 180 (because it will then be linear).

(2)If the two components are of the same magnitude, the time-

phase difference between the two components must not be

odd multiples of 90 (because it will then be circular).

Elliptically Polarized plane waves


92/147

2

0

2

0

00

2

00

2

0

2

0

0

cos2)2tan(

sincos2

)cos(e)cos(e

Eee

yx

yx

y

y

x

x

y

y

x

x

yxx

yyxx

EE

EE

E

E

E

E

E

E

E

E

kztkztE

EE

[2-16]

Polarization


93/147

Typical Applications

Vertical polarization is most commonly used when it is

desired to radiate a radio signal in all directions over ashort to medium range.

Horizontal polarization is used over longer distances to

reduce interference by vertically polarized equipmentradiating other radio noise, which is often predominantly

vertically polarized.

Circular polarization is most often used in satellitecommunications.

Polarization Loss Factor & Efficiency


94/147


Usually, polarization of the receiving antenna polarization of

the incoming (incident) wavepolarization mismatch.

The amount of power extracted by the antenna from the

incoming signal will not be maximum because of thepolarization loss

Assuming that the electric field of the incoming wave can be

written as

unit vector ofthe wave



95/147

Polarization of the electric field of the receiving

antenna

Polarization loss factor (PLF)

angle between the twounit vectors



96/147

Polarization efficiency

= Polarization mismatch = loss factor:

the ratio of the power received by an antenna from a given

plane wave of arbitrary polarization to the power that would be

received by the same antenna from a plane wave of the same

power flux density and direction of propagation, whose state of

polarization has been adjusted for a maximum received power

Polarization Loss Factor & Efficiency (Cont)


97/147

PLF for transmitting and receiving aperture antennas



98/147

PLF for transmitting and receiving linearwire antennas

Input Impedance (Transmitting mode)


99/147

Input impedance:

the impedance presented by an antenna at its terminals or

the ratio of the voltage to current at a pair of terminals or the ratio of the appropriate components of the electric to

magnetic fields at a point

We are primarily interested in the input impedance at the input terminalsof the antenna

Input Impedance


100/147

Ratio of the voltage to current at these terminals, with no load

attached, defines the impedance of the antenna as

Input Impedance


101/147

Assume that the antenna is attached to a generator with

internal impedance

We can find the amount of power delivered to Rr for radiation by

the amount of power dissipated in RL as heat by

Input Impedance


102/147

Current developed within the loop is

Input Impedance


103/147

Magnitude of current developed within the loop is

The power delivered to the antenna for radiation is given by

and that dissipated as heat by

Input Impedance The remaining power (Pg) is dissipated as heat on the


104/147

The remaining power (Pg) is dissipated as heat on the

internal resistance Rg and it is given by

The maximum power delivered to the antenna occurs when

we have conjugate matching

For this case

Input Impedance From equations (2 81) (2 83) It is clear that


105/147

From equations (2-81)(2-83), It is clear that

The power supplied by the generator during conjugate

matching is

Antenna in the Receiving Mode


106/147

The incident wave impinges upon the antenna, and it

induces a voltage VT

All the formulation is same as the transmitting mode (just

replace subscript g with T)

Antenna in the Receiving Mode Under conjugate matching


107/147

j g g

Powers delivered to Rr ,RL ,and RT are given, respectively,

by

While the induced (collected or captured) is

Under conjugate matching of the total power collected or captured (Pc) half is

delivered to the load RT and the other half is scattered or reradiated through Rr

and dissipated as heat through RL

Antenna Radiation Efficiency


108/147

Remember that antenna efficiency that takes into account the

reflection, conduction, and dielectric losses

The conduction and dielectric losses of an antenna are very

difficult to compute

Even with measurements, they are difficult to separate and theyare usually lumped together to form the ecdefficiency.

The resistance RL is used to represent the conduction-dielectric

losses

Antenna Radiation Efficiency


109/147

power delivered to the radiation resistance

the power delivered to Rrand RL

Conduction-dielectric efficiency

where

RrRadiation ResistanceRLLoss Resistance

Equivalent areas


110/147

With each antenna, we can associate an umber of equivalent areas.

These are used to describe the power capturing characteristics of the

antenna when a wave impinges on itEffective area (aperture) Ae

Scattering area (aperture) As

loss area (aperture) AL

Capture area (aperture) Ac

Effective area (Aperture) Ae (Power available at input/wave

incidented on the antenna)the ratio of the available power at the terminals of a receiving

antenna to the power flux density of a plane wave incident on the

antenna from that direction, the wave being polarization matched tothe antenna. If the direction is not specified, the direction of

maximum radiation intensity is implied.

Equivalent areas


111/147

Effective areaAe

The effective aperture is the area which when multiplied by

the incident power density gives the power delivered to the

load

Equivalent areas


112/147

Effective areaAe

Under conjugate matching

The maximum effective area Aem

Equivalent areas


113/147

The scattering area As

is defined as the equivalent area when multiplied by the

incident power density is equal to the scattered orreradiated power.


As

Equivalent areas

Th l A


114/147

The loss area AL

is defined as the equivalent area, which when multiplied by

the incident power density leads to the power dissipated asheat through RL


Equivalent areas


115/147

Capture area Ac

is defined as the equivalent area, which when multiplied by

the incident power density leads to the total power

captured, collected, or intercepted by the antenna


In general, the total capture area is equal to the sum of theother three

Capture Area = Effective Area+Scattering Area+Loss Area

Ac = Ae + AS+ AL

Equivalent areas


116/147

Aperture Efficiency: apis defined as the ratio of the maximum effective area Aem

and of the antenna to its physical area Ap

the maximum effective aperture of any antenna is related to itsmaximum directivity D0 by

Antenna Temperature


117/147

The brightness temperature emitted by the different sources is

intercepted by antennas, and it appears at their terminals as an

antenna temperature

The temperature appearing at the terminals of an antenna is that

given by

Antenna Temperature


118/147

Antenna temperature (effective noise temperature of the

antenna radiation resistance Rr; K) TA

Assuming no losses or other contributions between the antenna

and the receiver, the noise powertransferred to the receiver isgiven by

Antenna Temperature


119/147

Antenna Noise Power (Pr)

Antenna TemperatureAntenna temperature at the receiver terminals


120/147

Antenna temperature at the receiver terminals

Antenna TemperatureThe effective antenna Temperature (T ) at the receiver


121/147

The effective antenna Temperature (Ta) at the receiver

terminals is given by

Antenna Temperature The antenna noise power


122/147

The antenna noise power

The system noise powerIf the receiver itself has a certain noise temperature Tr(due to

thermal noise in the Receiver components), the system noise

power at the receiver terminals is given by

Antenna Temperature


123/147

Antenna Temperature


124/147

Arrays


125/147

INTRODUCTION

Enlarging the dimensions of single elements often leads to

more directive characteristics (very high gains) to meet the

demands of long distance communication

An other way to enlarge the dimensions of the antenna,

without necessarily increasing the size of the individualelements, is to form an assembly of radiating elements in

an electrical and geometrical configuration. This new

antenna, formed by multi elements, is referred to as an

array

ArraysINTRODUCTION

Th t t l fi ld f th i d t i d b th t dditi f


126/147

The total field of the array is determined by the vector addition of

the fields radiated by the individual elements

To provide very directive patterns, it is necessary that the fields

from the elements of the array interfere constructively (add) in

the desired directions and interfere destructively (cancel each

other) in the remaining space

There are at least five controls that can be used to shape theoverall pattern of the antenna

1. The geometrical configuration of the overall array (linear,

circular, rectangular, spherical, etc.)

2. The relative displacement between the elements

3. The excitation amplitude of the individual elements

4. The excitation phase of the individual elements

5. The relative pattern of the individual elements

ArraysApplications

A th t i id l d


127/147

An array that is widely used

as a base-station antenna for

mobile communication.

It is a triangular array consisting

of twelve dipoles, with four

dipoles on each side of the

triangle.

Each four element array, on

each side of the triangle, is

basically used to cover anangular sector of 120 forming

what is usually referred to as a

sectoral array.

ArraysTWO-ELEMENT ARRAY:

T i fi it i l h i t l di l iti d l th


128/147

Two infinitesimal horizontal dipoles positioned along the z-

axis, as shown in figure 6.1(a)

Figure 6.1 Geometry of a two element array positioned along

the z-axis.


Th t t l fi ld di t d b th t l t i


129/147

The total field radiated by the two elements, assuming no

coupling between the elements, is equal to the sum of the

two and in the y-z plane it is given by

Phase difference between the elements adjacentelement

k=2/

The magnitude excitation of the radiators is identical (I0)

Phase difference=(2/)x Path difference


Assuming far field observations and


130/147

Assuming far-field observations and

referring to Figure 6.1(b)

Equation 6-1reduces to



131/147

The total field of the array is equal to the field of a singleelement positioned at the origin multiplied by a factor

which is widely referred to as the array factor.

Thus for the two-element array of constant amplitude, theArray Factoris given by

which in normalized form can be written as



132/147

The array factor is a function of the geometry of the arrayand the excitation phase.

By varying the separation d and /or the phase between

the elements, the characteristics of the array factor and ofthe total field of the array can be controlled.


Pattern Multiplication:


133/147

Pattern Multiplication:

The far-zone field of a uniform two element array of

identical elements is equal to the product of the field of asingle element, at a selected reference point (usually the

origin), and the array factor of that array. That is,

ArraysN-ELEMENT LINEAR ARRAY: Uniform Amplitude and

Spacing


134/147

Spacing

Let us generalize the method to include N elements. Referring to

the geometry of Figure 6.5(a),

Let us assume that all the elements have identical amplitudes

but each succeeding element has a progressive phase lead

current excitation relative to the preceding one.

An array of identical elements all of identical magnitude

and each with a progressive phase is referred to as a

uniform array


Spacing


135/147

Spacing


Spacing


136/147

Spacing

The Array factor (AF)

By applying pattern multiplication rule on arrays of identicalelement . The array factor is given by

Total phase difference = Phase difference due to path difference + =kdcos+Phase difference=(2/)x Path difference=kdcosPhase difference between the elements adjacent element


Spacing


137/147

Spacing

Multiplying both sides by ej

subtracting Eq 6.6 from Eq 6.8

Which can also be written as

6.6


Spacing


138/147

Spacing

AF

If the reference point is the physical center of the array, the array

factor of (6-10) reduces to

if is small


Spacing


139/147

Spacing

maximum value of array factor is equal to N

Normalized Array Factor

ArraysN-ELEMENT LINEAR ARRAY: Uniform Amplitude and Spacing

Nulls of the Array:


140/147

Nulls of the Array:

(AF)n=0| = n

To find the nulls of the array,

Eq (6-10c) or (6-10d) is set equalto zero

= 2n/N(kdcosn+) = 2n/N

cosn= (/2d)(- 2n/N)

For n = N,2N,3N,..., (6-10c) attains its

maximum values because it reduces to a

sin(0)/0 form.

The values of n determine the order of the

nulls (first, second, , etc.)

ArraysN-ELEMENT LINEAR ARRAY: Uniform Amplitude and Spacing

Maximum


141/147

Maximum

The maximum values of normalized array factor occur when

sin(/2) =0| = m

First Maximum or Principal Maximum

The first maximum of the array factor occurs when m = 0

/2 = 0 or = 0

ArraysOn the basis of the main lobe array

Broadside Array


142/147

y

Ordinary End-fire Array

Broadside Array:The maximum radiation of an array directed normal to the axis

of the array (broadside; =900)

The first maximum of the array factor occurs when

= 0 or kdcos+ = 0

kdcos900+ = 0 or = 0

Since it is desired to have the first maximum directed toward =900

Thus to have the maximum of the array factor of a uniform linear array

directed broadside to the axis of the array, it is necessary that all theelements have the same phase excitation (in addition to the same

amplitude excitation). The separation between the elements can be of

any value.

ArraysBroadside Array:

To ensure that there are no principal maxima in other directions,


143/147

p p ,

which are referred to as grating lobes, the separation between

the elements should not be equal to multiples of a wavelength

(dn, n=1,2,3,.) and =0.

If d=n, n=1,2,3,. And =0, then

Thus for a uniform array with = 0 and d = n, in addition to having themaxima of the array factor directed broadside ( = 90 ) to the axis of the

array, there are additional maxima directed along the axis ( = 0 ,180 ) ofthe array (end-fire radiation).


Grating Lobes: multiple maxima, in addition to the main maximum


144/147

g p ,

To avoid any grating lobe, the largest spacing between the elements

Should be less than one wavelength(dmax


145/147

where L is the overall length of the array


Directivity:


146/147

y

where L is the overall length of the array

Arrays


147/147

Antenna Engineering for Mte

Documents

Transcript of Antenna Engineering for Mte