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TRANSCRIPT
Antenna Arrays
Objectives
By the end of this lecture, we will be able to:
• Explain the motive for designing arrays.
• Design a uniform linear array using various constitute elements.
• Recognize various array typologies and their potential applications.
• Explain the impact of mutual coupling between array elements and how to combat
or avoid it.
Note: Boxed sections that start with the word ”Extra” are not required for tests. Neverthe-
less, they are very important to gain concise understanding of the underlying mathematical
and physical concepts.
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Antenna Arrays
1. Why Arrays?
We use antennas to transmit signals between two systems mostly separated by free space.
Our goal is to ensure that the receiver can detect the transmitted signal. As we know, this
type of communication adheres to the well-known Friis transmission equation:
Preceived = PtransmittedGtransmitterGreceiver
(λ
4πR
)2
. (1.1)
Let us assume that we have no control over the transmitted power, there are two ways to
improve the detection of the received signal, control the gain of both transmitter and receiver
and operate at lower frequencies. If we set aside the frequency issue, the gain of an antenna
increases if we can focus its radiation pattern in a single direction. As we narrow the direction
of focus, the antenna gain in that direction increases (of course at the expense of reducing
the gain in other directions but we don’t care about these directions). Focusing the gain can
be done using two methods: Big antenna or an antenna array. Analogously, this problem is
similar to collecting rain using buckets as described by Haupt: ”A big antenna collects a lot
of electromagnetic waves just like a big bucket collects a lot of rain . . .Another approach to
collecting a lot of rain is to use many buckets rather than one large one. The advantage is
that the buckets can be easily carried one at a time. Collecting electromagnetic waves works
in a similar manner.” In this lecture, we will study antenna arrays since big antennas do
not differ from ”regular-sized” antennas. The advantage of arrays over big antennas is that
we can do a lot of ”cool” things with arrays that are not possible using big antennas as well
see in this class.
2. Two-Element λ/2-Dipole Array
At this point in the course, we know the electric field at an observation point (P ) generated
by a half-wave dipole placed at the origin (O) as shown in Figure 1.1, but for the sake of
completeness, let us rewrite it here
Ed = jηI exp (−jkr)
2πr
cos
(π2
cos θ
)sin θ
. (1.2)
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Figure 1.1: A half-wave dipole located at the origin in a three-dimensional space.
Now, let us bring another antenna as in Figure 1.2 and study the the impact on the field
at P . To simplify the math, let us make the antennas symmetric with respect to the y-axis.
Since this problem is a far field problem, the amplitudes of the electric field at P do not
vary that much from one antenna to another, so we assume both antennas have the same
amplitude of the electric field at P . However, this assumption is invalid when we consider
the phase. Therefore, we can write the total electric field at P as
Etot = Ed1 exp jk(r • r1)+ Ed2 exp jk(r • r2)
= Ed
[exp jk(r • d
2y)+ exp jk(r • −d
2y)]
= Ed
[exp jk d
2sin θ sinφ+ exp −jk d
2sin θ sinφ
]= Ed
[2 cos(k d
2sin θ sinφ)
]= Ed︸︷︷︸
element factor
[2 cos(π
d
λsin θ sinφ)
]︸ ︷︷ ︸
array factor (AF)
(1.3)
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Figure 1.2: A two-element half-wave dipole array.
where
r1 = |R1 −R|y = d/2 y; r2 = |R2 −R| − y = −d/2 y
Equation (1.3) reveals a very important property of arrays, which is the total field is
the product of the array factor (AF) with the element factor. At this point in the course,
we know that the radiation pattern (or gain) is related to the power of the electromagnetic
wave, which is related to the square of the field. Thus, we can write the gain (G) of the
array as
Gain ∝ (|Element Factor|)2 × (|Array Factor|)2. (1.4)
The fact that we can decompose the gain of an array into two factors makes it easier to
generalize the concept of arrays to antenna structures that are not half-wave dipoles. The
array factor, as derived in Equation (1.3), does not depend on the elements of the array.
Now, let us study a specific case of Equation (1.3) with the assumption that d = λ/2. Let
us further investigate what happens on the xy-plane. By looking at Equation (1.2), we can
see that the electric field is independent on the variation along the azimuth (xy-plane), so it
is always constant. However, this not the case for the array factor of Equation (1.3), which
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Antenna Arrays
depends on both θ and φ. Since we are only interested in the variation of the electric field on
the xy-plane1, θ = 90. In Figure 1.3, we superimposed the normalized radiation patterns2
of both a single half-wave dipole and a two-element array of dipoles. We notice that the
maximum radiation pattern of the array quadruples compared to that of the single antenna;
it is concentrated on the x direction at the expense of killing the transmitted power along
the y direction. In fact, this phenomenon follows from the law of conservation of energy.
1 2
3 4
y (?=90o)
-y (?=270o)
-x (?=180o) x (?=0o)
Figure 1.3: A comparison between the radiation pattern on the xy-plane of a single half-wavedipole (red) and a two-element array of dipoles (blue). Curves are in linear scale not in decibel.
3. N-Element Array
Now, we have seen how powerful bringing two antennas close to each other to form an array.
The next ”logical” step would be the generalization to an array of N antennas (of course N
is a positive integer; to the best of my knowledge, there is no such thing called one-quarter of
antenna!). Let us derive the array factor for a linear (means elements are distributed along
a straight line), equally-spaced, and identical arrays as depicted in Figure 1.4. The array
1The field at θ = 0 is zero for a half-wave dipole.2We are interested in the radiation patterns ratio rather than the absolute absolute pattern.
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factor is
AF = exp jk(r • r1)+ . . .+ exp jk(r • rN)
=[1 + exp jk(r • dy)+ exp jk(r • 2dy)+ . . .+ exp jk(r • (N − 1)dy)
]=
N∑n=1
exp jk[r • (n− 1)dy] =N∑n=1
exp j[(n− 1)kd sin θ sinφ].
(1.5)
Figure 1.4: An N elements array.
Equation (1.5) resembles a geometric series if we set m = n − 1 and ψ = kd sin θ sinφ.
Therefore, we can write Equation (1.5) as
AF =N−1∑m=0
exp (jmψ) =1− exp (jNψ)
1− exp (jψ)
= exp (jN−12ψ)
exp (−jN2ψ)− exp (jN
2ψ)
exp (−j 12ψ)− exp (j 1
2ψ)
= exp (jN−12ψ)
sin(N2ψ)
sin(ψ2
)(1.6)
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The phase factor (complex exponential) of Equation (1.6) does not affect the radiation
pattern3; thus, we can edit it out for radiation pattern calculations. Moreover—as in the
case of a two-element array—the gain of the array is related to the amplitude squared of
Equation (1.6). In other words,
G(θ, φ) ∝ |AF |2 =
[sin(N2ψ)
sin(ψ2
) ]2, (1.7)
which is a periodic squared sinc function with a period of ψ = 2π as indicated in Figure 1.5
for N = 4 and −3π ≤ ψ ≤ 3π. This property plays an important role for array synthesis
and orthogonal arrays. Unfortunately, such topics are beyond the scope of this class.
Ao
-2: -: 0 : 2:
|AF
|2
0
8
16
Figure 1.5: The amplitude squared of the array factor versus ψ. Curve is in linear scale not indecibel.
3In fact, the phase factor results from choosing the reference point, which is arbitrary. Interestingly, wecan see how to get rid of it when we discuss the relation between DTFT and array theory.
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4. Array Parameters
4.1. Type of constitute elements
The array elements can be any type of antennas. An important consideration is whether
the array factor is going to improve the radiation characteristics or not. For instance, the
two-element dipole array that we discussed in Section 1.2 is not going to radiate on the z
(θ = 0) direction because the dipole configuration in Figure 1.1 does not have any power
radiated in that direction. If we need to force the array to radiate in that direction, we have
to change the orientation of the dipoles (or use another type of antennas that does not have
a null in the z direction).
4.2. Element Spacing
The main beam of an antenna array is called the main lobe, which should point towards the
direction of interest. Choosing the separation distance d is not arbitrary. In fact, it affects
the radiation pattern. As an example, let us study three cases.
4.2.1 Closely-spaced elements (d << λ)
For simplicity, let us assume that we have two elements distributed along the y-axis, so the
array factor is exactly similar to that of Equation (1.3). Let us also assume that d = λ/M ,
where M is any positive number (it does not have to be an integer). Thus, we can rewrite
that array factor of Equation (1.3) as
AF = 2 cos(π
Msin θ sinφ). (1.8)
As M gets larger, the two elements get closer to each other and the argument of the cosine
in Equation (1.8) gets smaller, which allows us to use small angle approximation 4 (cosγ ≈1− γ2/2 for γ << 1). Therefore,
AF ≈ 2(1−( πM
sin θ sinφ)2
2) = 2− (
π
Msin θ sinφ)2. (1.9)
4The approximation is simply the Taylor series expansion of the cosine in which all terms but the firstand second are omitted because the remaining terms are very small.
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1
2
3
4y (?=90o)
-y (?=270o)
-x (?=180o) x (?=0o)
Figure 1.6: A comparison between the radiation pattern on the xy-plane of a closely-spaced two-element array; M = 5 (blue), M = 10 (red), M = 20 (orange), and M = 40 (dashed purple).Curves are in linear scale not in decibel.
The contribution of the second term in the right hand side of Equation (1.9) becomes negli-
gible as M increases. Thus, we can fairly assume that for closely-spaced elements, the array
factor is constant. Figure 1.6 plots four cases for M = 5, 10, 20, and 40 at θ = 90.
4.2.2 d = λ/2
When the elements are spaced half a wavelength apart, the array factor has a null as depicted
by the blue curve of Figure 1.3. The null results from the relationship between the space (d)
and wavenumber (k). Physically, let us think about a particular example, which is the two-
element array of Figure 1.2. Let us assume that the currents of the elements are identical and
in-phase with one another and d = λ/2. At a point (0, y1, 0), where (y1 > 0 and y1 >> d)5,
the waves generated by the two elements are 180 out of phase. Therefore, the waves cancel
5We need to ensure that (0, y1, 0) is a far-field point in order to assume that the amplitude of waves fromeach element is identical.
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each other at (0, y1, 0). We can use the same argument to explain why we have null at a
point (0, y2, 0), where (y2 < 0 and |y2| >> d).
4.2.3 d ≥ λ
This is the situation in which we have lobes that are of the same peak amplitude as the main
lobe. These lobes are called grating lobes.
Exercise
With your neighbor(s), explain physically and mathematically why for N = 2 and d = λ
we have grating lobes? Refer to Figure 1.2, determine the direction of the maximum
power on the yz-plane
Physical explanation:
Mathematical explanation: (Hint: use Equation (1.3) and assume φ = 90)
4.3. Phase of Elements
So far we have assumed that we are feeding the elements with waves of same amplitude
and phase. The question is what happens if we relax these assumptions? Let us start with
relaxing only the phase (feed the array with same amplitude but each element has different
phase 6). Relaxing the phase allows us to steer the main beam towards any direction.
Adding a progressive phase (β)7 to each element of the array requires reformulating the array
6Relaxing the amplitude results in something called ” amplitude tapering”. For example, binomial ta-pering, Dolph-Chebyshev tapering, . . . etc.
7Progressive phase means that the difference between the phase of two consecutive elements is fixed. Forinstance, if we have three elements on any of the principle axes, the phase difference between the element#1 and element #2 should be equal that between element #2 and element #3.
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factor of Equation (1.5) as
AF = exp jk(r • r1)+ exp j[k(r • r2) + β)]+ . . .+ exp j[k(r • rN) + (N − 1)β]
=[1 + exp j[k(r • dy) + β]+ . . .+ exp j[kr • (N − 1)dy + (N − 1)β]
]=
N∑n=1
exp j(n− 1)[kr • dy + β] =N∑n=1
exp j(n− 1)[kd sin θ sinφ+ β].
= exp (jN−12ψ)
[sin(N2ψ)
sin(ψ2
) ],(1.10)
where ψ = kd sin θ sinφ+β. Therefore, Equation (1.10) has two knobs (element spacing and
progressive phase) that control the array factor compared to one in Equation (1.5).
Exercise
So far we derived the array factor when the elements of the array are distributed along
the y-axis. With your neighbor(s), what will be the expression of ψ if the elements are
distributed along:
a. x-axis
b. z-axis
Hint: r • x = cosφ sin θ and r • z = cos θ
5. Polar Plot of Array Factor
An easy way to visualize the array factor is to plot it in polar coordinates. If we look back
at the array factor of Equation (1.10), we notice that it is periodic with respect to ψ, but it
does not give much information about the 3-dimensional pattern shape.
To extract information about the 3D pattern, let’s first assume that the array elements are
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distributed along the z-axis8. So we can write ψ as
ψ = kd cos θ + β, (1.11)
and the normalized array factor9 as
AF (ψ)n =
[sin(N2ψ)
N sin(ψ2
)]. (1.12)
Then we need to fellow these steps:
1. Plot the amplitude of |AF (ψ)n| versus ψ.
2. Below that plot, draw a circle of radius kd and centered at ψ = β. Make sure that
your plot in step 1 is aligned with circle.
3. Since we are using the normalized array factor, the circumference of the circle represents
an array factor of 1. (if we don’t normalize, the circumference would represent an array
factor of N).
4. Starting with the nulls of step 1, draw a vertical line from these nulls to the circum-
ference of the circle in step 2. Then, draw a radial line from the circumference of the
circle to its center. Note that if you cannot draw a vertical line between |AF (ψ)n| plot
and the circle, the point lies in what is so called the invisible region. Otherwise, the
point lies in the visible region10.
5. Now, repeat step 4 for peaks and smoothly connect these points.
These steps are better explained with an example. Let’s assume that we have N = 4,
d = λ/4, β = π/4 and let’s construct the polar plot of the radiation pattern using same
steps as above.
8In this distribution, we have only a variation on the θ direction. We can still plot with other distributionsbut we will have both θ and φ variations.
9Normalized array factor makes it easier to plot.10
• Visible region: The region that is electromagnetically visible, so the shape of the array factor at thatregion determines the radiation pattern of the array.
• Invisible region: Part of the array factor that does not affect the radiation pattern.
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1. The amplitude of the array factor is
AF (ψ)n =
[sin(2ψ)
4 sin(ψ2
)], (1.13)
which is plotted in Figure 1.7 part (a).
2. The next step is to draw a circle of radius r = kd =
(2π
λ
)(λ
4
)=π
2, and centered at
ψ =π
4as shown in Figure 1.7 part (b).
3. Finally, nulls and peaks location are drawn as shown in Figure 1.7 part (b).
4. To find the main beam angle, we use basic trigonometry. In this case, the main beam
is at θ = 180 − cos−1(π/4π/2
) = 120.
5. A final and yet unnecessary step is to mirror the results of the radiation pattern for
0 ≤ θ ≤ π to create the radiation pattern for −π ≤ θ ≤ 0.
It is apparent now why we have grating lobes for d > λ because we are expanding the
circle and hence expanding the visible region . In fact, it fellows from the 2π-periodicity of
the array fact that if d = λ/2, we are putting exactly a period in the visible region and if
d > λ we are putting at least two periods in the visible region.
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A-(3:)/2 -(5:)/4 -: -(3:)/4 -:/2 -:/4 0 :/4 :/2 (3:)/4 : (5:)/4 (3:)/2
|AF|
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1
0.2
0.4
0.6
0.8
1
:/6
-5:/6
:/3
-4:/6
:/2
-:/2
4:/6
-:/3
5:/6
-:/6
: 0:/2
0.2
0.4
0.6
0.8
1
:/6
-5:/6
:/3
-4:/6
:/2
-:/2
4:/6
-:/3
5:/6
-:/6
: 0:/2
(b)
(c)
(a)
Figure 1.7: Polar representation of the array factor for N = 4, d = λ/4, β = π/4; (a). |AF (ψ)|versus ψ. (b). Polar plot of the AF ; note that θ is defined over 0 ≤ θ ≤ π. However, to cover upthe whole space, we can mirror the results of 0 ≤ θ ≤ π to get the polar plot of −π ≤ θ ≤ 0. (c).A magnified polar plot of part (b)
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Exercise
With your neighbor(s), plot the polar plot of array factor for N = 4, d = λ/4, β = −π/4.
Determine angle of the main beam.
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Extra: Relation between DTFT and array factor
Recall that the discrete-time Fourier transform (DTFT) is
X(ω) =∞∑
n=−∞
x[n]e−jωn. (1.14)
We can write Equation (1.10) as
AF (ψ) =∞∑
n=−∞
w[n]e−jψn (1.15)
And letting wn = 0 ∀n ≤ 0 & n > N . Also, for a uniform linear array, w[n] = w ∀n ∈[1, N ].
The question now is how to use this resemblance to help us understand the array? Let
us start with some assumptions:
1. ψ = kd, we removed both phase and angular components.
2. We assume that x[n] is obtained by sampling a continuous time signal.
With that in mind, let us do the following mapping between the variables of Equations
(1.14) and (1.15)
t −→ u, ω −→ k
where u is the spacial coordinate; in other words u can be either x, y, or z. Let us
think about two scenarios under which this relation is helpful.
Choosing a reference point11
In the derivation of the array factor in Equation (1.5), we noticed that there is a
phase factor that results from choosing the reference point to be at the origin. If for
one reason we want to choose the reference point to be the center of the array and
let us assume N is odd, then we have two options: Rederive Equation (1.5) or use
the shift property of DTFT, which is x[n − k] −→ X(ω)e−jωk. In this case, we want
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w[n] −→ w[n+ N−12
] then the array factor would become
AF = exp (j(N − 1)ψ)sin(N2ψ)
sin(ψ2
)Element spacing
As we mentioned before, element spacing d should be at mostλ
2to avoid grating lobes.
In order to relate this condition to DTFT, we know that electromagnetic waves has
both spacial and temporal components. The spacial component defines the relation
between the spacial position u and wavenumber k, which—as we said before—a Fourier
transform pair. Therefore, from Nyquist sampling theorem, the spacing between ele-
ments should be
d ≤ π
Bk
=π2πλ
=λ
2. (1.16)
Reference point is the point that we call the origin
6. Special types of arrays:
6.1. Broadside Arrays
As we mentioned in the previous section, we have two knobs to control the radiation charac-
teristics of the array, phase and spacing. If we desire the array factor to peak on the direction
normal to the array axis, then we call this type of array a broadside array. The condition
under which an array is a broadside array is when ψ = 0 at the broadside. So, all what need
is to set ψ to zero at the broadside direction. For the array of Figure 1.4,
0 = ψ = kd sin θ sinφ+ β|φ=0,180 or θ=0,180 =⇒ β = 0 (1.17)
So, no matter what d is, as long as β = 0, the array will be broadside. However, if d ≥ λ,
there will be a maximum at the broadside along with other maximum or maxima in various
directions.
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Fact: Broadside array factor always has a fan beam.
Exercise
Work with your neighbor(s), what are the broadside radiation angles for an array of
half-wave dipoles if the array is distributed along the
a. x-axis?
b. z-axis?
Hint: Start with the definition of ψ for specific element distribution.
6.2. Ordinary End-Fire Arrays
In this case, we need the main beam to point towards the array axis. In other words, if the
array elements are distributed along the y-axis, we want the main beam to point towards
+y, −y, or both.
Let us start with making the beam points towards the +y. In this case, θ = 90 and
φ = 90; thus, we need to satisfy this condition
0 = ψ = kd sin θ sinφ+ β|φ=90,θ=90 =⇒ β = −kd. (1.18)
Of course, if we want to point the beam towards the −y, the new condition would be
0 = ψ = kd sin θ sinφ+ β|φ=−90,θ=90 =⇒ β = kd. (1.19)
Let us pause here and make the following observations:
(a). Although we think that we have two knobs to control the radiation pattern, we have
only one knob since the phase affects element spacing and vice versa.
(b). If d = λ/2, we will have two main beams, one points towards the +y, and the other
points towards the −y. (Prove it)
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(c). If d = nλ, n = 1, 2, . . ., we will have four maxima: two in the broadside and two along
the array axis.
(d). To get a single main beam, d ≤λ
2
(1−
1
2N
)with β = −kd for +y or β = kd for −y.
In Figure 1.8, we plot the an ordinary end-fire array factor for various spacing (or phasing)
for an array of N = 8 elements.
:/2
-:
: 0
(a) Blue curve is for β = −kd while red curve isβ = kd. In both cases, d = (0.47)λ.
:/2
-:/2
: 0
(b) Blue curve is for d = λ/2 while red curve isd = λ. In both cases, β = kd.
Figure 1.8: Radiation patterns for several ordinary end-fire arrays.
6.3. Hanson-Woodyard End-Fire Arrays
Let us ask the following question: can we make the end-fire array more directive? In other
words, can we make the main beam narrower? In 1938, Hanson and Woodyard derived the
conditions for directive end-fire array as
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β = −(kd+
2.94
N
)≈ −
(kd+
π
N
), For peak at φ = 90
β =
(kd+
2.94
N
)≈(kd+
π
N
), For peak at φ = −90
(1.20)
The spacing between elements should be
d =
(N − 1
N
)λ
4≈λ
4for large N (1.21)
To compare the directivity of Hanson-Woodyard (HW) end-fire array to that of ordinary
(ORD) end-fire array, the half-power beamwidth (HPBW) of these two designs are
ΘHW ≈ 2 cos−1(
1−0.1398λ
Nd
)(1.22)
ΘORD ≈ 2 cos−1(
1−1.391λ
πNd
). (1.23)
Note that, the increase in directivity observed by the Hanson-Woodyard array comes at the
expense of increasing the side-lobe level as shown in Figure 1.9.
Figure 1.9: Comparison between the radiation pattern of ORD and HW end-fire arrays. Thefigure is taken from Balanis
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Exercise
For N = 8, compare the HPBW of both ordinary and Hanson-Woodyard end-fire arrays.
For fair comparison, fix d to the spacing required by the Hanson-Woodyard array. Work
with your neighbor(s)
6.4. Phased Arrays
In Section 5, we had two examples of two identical arrays. They both share same number of
elements and inter-element spacing; however, they have different phase factor (β). We saw
that the radiation patterns of the arrays are identical except that each one points the main
beam towards different direction. This observation gives us an idea on how to rotate the
main beam of an array. The question is what should be the value of β that corrsponds to
rotating (steering) the main beam towards a specifc direction. A simple answer would be to
find the steering angle and set ψ to zero at that angle. For example, let us assume that our
array is distributed along the z-axis and we want to steer the main beam towards θ = θ,
then β is given by
0 = ψ = kd cos θ + β|θ=θ =⇒ β = −kd cos θ. (1.24)
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For example, let’s assume we that have an array distributed along the z-axis with N = 4 and
d = 0.4λ. We want to scan broadside direction and 60 off the broadside from both directions.
Let’s do 30 increments, so the angles that we want to cover are θ = 30, 60, 90, 120, 150.The first step is to simplify the kd expression, so kd = 0.8π. Then, we need to find the phase
shifts associated with these angles, which are listed in Table 1.1.
Table 1.1: Phase factor β for each steering angle
θ β
30 −0.6928π
60 −0.4π
90 0
120 0.4π
150 0.6928π
The plots of the array factor for these cases are shown in Figure 1.10.
30
60
90
120
150
180
0
3=30o
3=60o
3=90o
3=120o
3=150o
Figure 1.10: Phased array radiation pattern.
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Exercise
With your neighbor(s), use the method discussed in Section to extract the polar plot of
the radiation pattern for θ = 60, 90, and 120. What is happening to the circle as the
phase changes?
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Antenna Arrays
Extra: Element spacing of phased arrays
The rule of thumb that we have is the element spacing should adhere to the d < λ2.
However, let us assume that we have an array with its elements are distributed along
the z-axis, if we choose to steer the main beam towards the broadside θ = 90, we
can steer the main beam towards the broadside without any grating lobes even if the
space between elements, say 0.9λ. The general condition for minimum spacing—which
avoids grating lobes—is
d <λ
1 + | cos θ|, (1.25)
where θ is the maximum off broadside scanning angle.
7. Mutual Coupling
So far, we have assumed that the individual element of an array does not have any influence
on its neighbors. This assumption in reality is invalid, there must be an interaction between
array elements. As the spacing between the elements of an array gets smaller, the neighboring
elements become in the near-field region of each other. Thus, energy transfers from one
element to another. This interaction, consequently, impacts the following
1. The phase and magnitude of the element current.
2. As a result from the change in current, the antenna impedance is no longer equals to
the isolated antenna impedance12
3. Different currents alters the radiation pattern of the array; therefore, we need to ac-
count for it when we do the pattern multiplication.
Therefore, for closely-spaced elements, we need to modify the definition of Zin = V1/I1. For
N element array, the input impedance of the mth element is
Zm =VmIm
= Zm1I1Im
+ Zm2I2Im
+ . . .+ ZmmImIm
+ . . .+ ZmNINIm, (1.26)
12Isolated antenna is simply a stand alone antenna that does not belong to an array.
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Antenna Arrays
where Zmn is called the mutual impedance if m 6= n and self impedance if m = n. It is
given by Zmn =Vm
In
∣∣∣∣∣Ii=0, ∀i 6=n
Equation (1.26) is derived from the general matrix that relates currents and voltages of
an array. Let us say that we have an array of N elements, the matrix that relates currents,
voltages, and mutual impedance in an array is an N ×N matrix given by
V1 = Z11I1 + Z12I2 + . . .+ Z1NIN
V2 = Z21I1 + Z22I2 + . . .+ Z2NIN
......
VN = ZN1I1 + ZN2I2 + . . .+ ZNNIN
(1.27)
From reciprocity, Znm = Zmn. For example, we know that λ/2-dipole has an input impedance
that is equal to 73 + j42.5Ω in which the radiation resistance is simply 73Ω. However, if
there are two dipoles separated by a distance of 0.2λ. The input impedance would be
Zin = Z11 − Z221/Z22 = (73 + j42.5)− (67.5)2/(73 + j42.5) = 26 + j70 Ω.13
References
Most of the material here are taken from:
(1). Prof. Gregory Durgin’s previous notes.
(2). Haupt, Randy L. Antenna Arrays: A Computational Approach: https://goo.gl/DzFgQL
(3). Balanis, Constantine A. Balanis Antenna Theory: Analysis and Design: https://goo.gl/ED9EMN
(4). Stutzman, Warren L. and Thiele, Gary A. Antenna Theory and Design: https://goo.gl/5Gi1xY
13Value of mutual impedance is taken from Kraus with the assumption that ratio between length of thedipole and its diameter is 73
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