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PATTERN SYNTHESIS OF LINEAR AND CIRCULAR ARRAYS
by
Chuang-Jy Wu ,B.Eng.
A thesis submitted to the Faculty of Graduate Studies and Research in partial fulfillment of the requi~ments for the degree of Master of Engineering.
Department of Electrical Engineering, McGill University, Montreal. August, 1962
ABSTRACT
Methods of pattern synthesis for the linear and curved
array are examined and several new methods have been developed.
Based on the stationary value characteristic the optimum pattern
of the linear array with preassigned amplitude distribution
and arbitrary space distribution is studied. The amplitude
distribution of a curved array for a specified pattern which can
be approximated by a truncated Fourier series is obtained by
solving a set of simultaneous linear equations. The method is
applicable to any curved array if the specified pattern and the
array configuration are symmetrical with respect to the
reference axis. The circular array with anisotropie elements is
discussed and a simple experiment bas been performed to investigate
the characteristics of such array. An extensive bibliography of
pattern synthesis for antenna array is appended.
i
ACKNOWLEDGEMENTS
The author wishes to express his sincere gratitude to
Dr. T~J.F.Pavlasek for his patient guidance and constant
encouragement in the course of this research. He is also
greatly indebted to Mr. Y.F.tum for critical commenta and
invaluable help in preparing and reading the final draft of
the thesis. The author is grateful to the technical staff
at the Department of Electrical Engineering, McGill University
for their assistance, especially to Messrs. M.Zegel, P.Conroy,
E.Hauck, and J.Simms; to the staff of the Engineering
Library for their help in securing numerous inter-library
loans, to the staff of the Computing Centre for processing
the programmes, and to Mrs. J.R.Horner for doing such a fine
job in typing this thesis.
The author also gratefully acknowledges assistance from the
National Research Council, Ottawa, who provided the author with
two summer supplements and who financed the whole research
project (Grant No. A-515).
ii
TABLE OF CONTENTS
Ahstract
Acknowledgements
I. INTRODUCTION
II. LINEAR ARRAY PATTERN SYNTHESIS
2.1 General Space Factor
2.2 Polynomiale for Linear Arrays
2.2.1 Complex Polynomiale
2.2.2 Tschebyscheff Polynomiale
2.3 The Optimum Pattern of Unequally Spaced Linear Array
i
ii
1
6
7
9
9
12
18
2.3.1 Optimum Pattern Criteria 19
2.3.2 General Equations of Optimum Pattern 20
2.3.3 Examp1es 21
2.3.4 The Equivalence Between Amplitude Distribution and Space Distribution 29
2.3.5 Some Design Considerations for Unequally Spaced Arrays. 32
2.4 Summary 34
III. CIRCULAR ARRAY PATTERN SYNTHESIS 35
3.1 Curved Array of Isotropie Sources 36
3.1.1 ~Pattern Synthesis 37
3.1.2 Examples 40
3.1.3 The Convergence of the Space-Phase Series 46
3.2 Continuous Distribution and Circular Array
3.2.1. Pattern Synthesis by Using Continuous Distribution
3.2.2 The Upper Limite of m
50
51
54
3.3 Circular Array of Anisbtro~ic Elements
IV. EXPERIMENTAL STUDY OF THE CIRCULAR ARRAY WITH ANISOTROPie 'ELEMENTS
4.1 Introduction
4.2 Experimental Arrangement
4.3 Measurements: The Circular Array with A~is6tro~ic· Elemeftts
V. CONCLUSION
BIBLIOGRAPHY
57
62
62
62
66
74
76
I. INTRODUCTION
The theory of pattern synthesis is concerned with
determining the relationsbip between the far-field pattern
of an array and the amplitudë and phase distribution of the
individual elements and their spacing. This is of utmost
importance in antenna design since if a single antenna is
unable to produce a desired pattern, it is usually feasible
to construct and use a system of antennas. This thesis is
restricted to the case of sources located on a straight
line or eurve.
In recent years, considerable attention bas been
given to the problem of synthesizing the patterns of linear
arrays and ring quasi-arrays. Most of the papers on pattern
synthesis in the early days of directional antenna design
dealt with broadcast antenna arrays witb equal magnitude
excitation of the elements, or with Yagi-type antennas
21 57 . (see Foster and Southworth • An extended bibl~ography of
antenna arrays before 1930 also appeared in Southworth 1 s
paper). Hansen and Woodyard 24 demonstrated that the gain of
a uniform endfire array could be increased by using an array
with larger values of phase differences between each element
than was customarily used. It was Schelkunoff 51 who first
introduced the polynomial formulation of the linear array problem.
By utilizing the correspondance between the pattern of an array
and the value of a complex polynomial on the unit circle, he
obtained an improved pattern by equally spacing the zeros of the
polynomial on an appropriate arc of the unit circle. The
optimum pattern was not achieved until Dolph 74 devised a
method using the characteristics of Tchebyscheff polynomials
to synthesize the broadside array with half-wavelength spacing
82 75 79 between elements. Later Riblet , DuHamel , Pritchard ,
Rhodes 81 and Sinclair and Cairns 84 extended Dloph's method
to the linear array with greater or less than half-wavelength
spacing, to the end-fire array and to the array with anisotropie
elements, 61 Recently, Unz proposed a method for pattern
synthesis of unequally spaced array by expanding the space-
phase terms of the space factor in an infinite series. Using
the stationary value method, the pattern of a linear array
with equal excitation and unequal spacing was obtained by
Pokrovskii45
• Most of the theoretical anaylses of linear arrays
rell on the assumption that the element patterns are identical,
in which case the pattern multiplication method can be applied.
Hines, Rumsey and Tice 28 attempted to modify the usual pattern
multiplication method which was useful only for obtaining the
first approximation for linear arrays.
Because of difficulties of analysis of the linear array
2
with .discrete elements. the theoretical study of continuous
distribution might be useful. It is a reasonable assumption
in the analysis that if the number of discrete elements is
large enough a continuous distribution can substitute for a
discrete array. Woodward and Lawson 67 investigated the
uniform amplitude line distribution with progressive phase
variation, and utilized the resulta to synthesize an arbitrary
pattern. By controlling the variation of the amplitude
distribution with known uniform phase or controlling variation
19 of phase with known amplitude distribution, Dunbar showed
that a specified beam shape may be obtained. 59 Taylor studied
line-source by means of function theory, and an ideal pattern
was established. 55 Shanks suggested a method of pattern
synthesis using variation of amplitude but with a specified
non-linear phase distribution. The technique might be useful
for large antenna design.
The prob1em of pattern synthesis of a circu1ar array
has been so1ved for some particu1ar cases. Expanding the
space-ph~se factor to a Fourier-Bessel series, Hansen and
24 114 96 101-106 Woodyard , Page , Harrington and Lepage and Knudsen
have analysed the circular array extensively. The difference
of array characteristics between uniform distributed elements
and the continuous distribution has been investigated in detail.
119 Taylor suggested a method whereby any prescribed pattern
representable by a truncated Fourier series can be obtained.
3
94 DuHamel derived the optimum pattern for antenna arrays on a
circular surface of small diameter. Using the fact that the
far-field pattern of the form cos n9 can be obtained by the
unifurm clrcular array with total progresslng phase distribution
2n1f 1 th i f Patton and Tillman llS a ong e c rcum erence~
introduced a method to syntheslze any specified pattern which
could be expanded in a Four~er series.
Although the subject of pattern synthesis has been
investigated for a long time, it is surprising that there are
not many methods available for synthesis of linear or curved
a:rrays. In fact very few problems can be solved by using
known methods. However, several known methods of pattern
synthesis for antenna array are described here, and their
applicability and the effectiYeness discuss~d.
There are two parts to the present work; the first
part (Chapter 2) deals with the optimum pattern of the
linear array, the second part (Chapters 3 and 4) is devoted
to the pattern synthesis of the curved array in general and
the circt\_lar array in pat·ticular.
Based on the existing theory of equally spaced linear
arrays, the relationship between the antenna array and the number
4
of nulls of the space factor will be discussed in Chapter 2,
and then the criteria of the optimum pattern for the linear
array will be stated. By using the stationary value character-
istic, the broadside optimum pattern can be obtained for the
unequally spaced linear array with known amplitude distribution.
From the calculated results of the optimum pattern, the
relationship between the space distribution and amplitude
distribution will be examined qualitatively.
In Chapter 3 a new method of pattern synthesis for the
curved array is derived by expressing the space-phase term
in a Fourier-Bessel series. The method is applicable to
any type of curved array so long as the geometrical
configuration is symmetric with respect to the pattern axis.
5
It is shown that the usual pattern synthesis method of the equally
spaced circular array by using continuous current distribution
is a special case of the new method.
Since a suitable analytical method of pattern synthesis
for the circular array with anisotropie elements cannot b~
established, an experimental method is performed, to investigate
the characteristics of such arrays. The experimental arrange
ments and the results are shown in Chapter 4.
II. LINEAR ARRAY PATTERN SYNTHESIS
According to the beam shape, antenna beams can be
classified as pencil-beam, fanned-beam, shaped beam and
omnidirectional beam. A fanned-beam can usually be
obtained by simply reducing the corresponding dimension of
the aperture of a pencil-beam antenna, and an omnidirectional
beam may be produced by a half-wave antenna or an aperture
antenna. For the shaped-beam pattern, the method of synthesis
depends on the particular beam shape. However, these various
cases will not be discussed here and only the case of
pencil-beam antennas will be considered.
In order to simplify and generalize the methods of .
p•ttern synthesis, it is assumed that the pattern multiplication
method is valid and each elemental source bas an omnidirectional
pattern in the plane in which the pattern is synthesized.
Since the space phase difference between consecutive elements
for an equally spaced array is always the same, one can consider
the array factor as a (n-l)th order polynomial for an n-element
array and the variable of the polynomial varies along the
circumference of the unit circle in the complex plane. The
problem of pattern synthesis is then completely reduced to a
study of the properties of the complex polynomial. If the
spacing between each element is known, the amplitude
6
distribution of the arr~y, i.e. the coefficients of the
polynomial, can be simply determined by specifying the
position of the nulls in the specified pattern, i.e. the
ro~ts of the polynomial.
Since the space-phase differences of the successive
elements are different for an unequally spaced array, the space
factor becomes an irregular polynomial which cannot be
determined by specifying the roots of the polynomial. The
m-ethods of pattern synthesis for equally spaced arrays are
not applicable in this case. If the amplitude distribution
of the array is known, the space distribution may be determined
by using the stationary value characteristics of the specified
pattern.
In the following sections~ the methods of pattern
synthesis for equally spaced arrays will be discussed. .The
method of design for the optimum pattern of the antenna array
with specified amplitude distribution will be given and the
relationship between the space and amplitude distribution
will be studied.
2.1 General Space Factor
The field strength (in RMKS system) at any point from
an array with isotropie elem~nts is:
7
N-1
E(9) = - t.ô ~ 4TI'r n
volts/me ter
where An is the current amplitude (magnitude and phase) of the
nth element in Amperes.
r is the distance between the nth element and the n
observing point, in meters.
is the permeability of free space, 4'fl'xl0- 7 henry/meter.
(3 = 2if/'A
À is wavelength in meters.
For a distant observing point, the phase factor becomes
r = (l -X ) • '1.:/R n n
8
= R -X cos 9 .....•••• 2.2 n
where R is the distance between the reference and observing
point.
/
G AH-1
~-----:-----il1,..;-------
Figure 2.1 Space Phase Difference Between any Element and Rèference Point
9
The field strength is then
N-1
~ J./5X. cos9 A e . n ..... 2.3
n
Since we are interested in the shape of far-field pattern only,
the space factor is proportional to
If the reference point is chosen at the position of the
zeroth-element, the space factor with equal spacing d is
2.2
2.2.1
F(9) = N-1 2:_ A ejty.3d n=O n
cos9 ·
Polynomiale for Linear Arrays
51 58 Complex Polynomiale '
Let Z = eldd cos9
tbea Eq.(2.5) becomes:
F(9)=A 0 + A1 z + A2 z2 + •••• + A ZN-1 N-1
••••• 2. 5
•..•• 2.6
. • • • • 2 • 7
which is a polynomial with order N-1 for the N-element array.
There are N-1 roots in (Eq.2.7) and the polynomial is uniquely
determined if all the roots are known. However, the implication
of the relationship between the shape of F(9) and the
corresponding roots have not yet been fully developed.
l' •.
Since Z is a complex variable with unit absolute
value, it is always on the circumference of the unit circle.
d=-"./4
(Cl)
Figure 2.2
d=3J\./4-
(C)
The Relations Between the Range of Z
and the Spacing d. (The values in the figure show the corresponding directions in space .. )
As 9 varies from 0° to 180°, Z moves from ej;.3d to e -j~d
in the clockwise direction. So the path of Z may be a portion
of the unit circle or several circuits of it depending on
whether the spacing d is smaller or larger ~han A/2,
(Figure 2.2).
If the roots of (Eq.2.7) are z1 , z2 ••••• ZN-l' then
10
0 •••• 2 .. 8
If the roots are on the circu•ference of the unit circ1e (i.e.
"Ad ·Ad unit •agnitude) within the region eJ,~ to e-Jr , then for d
less than or equal to ~/2, F(9) experiences N-1 zeros when 9
travels fro• 0° to 180°. There are at •ost N-1 lobes of the
space factor. If d is larger than ~/2, the point on the unit
circle corresponds to many values of the direction in physical
space. The nu•ber of nulls of the space factor may thus
exceed N-1, and correspondingly the number of lobes may also
be greater than N-1.
The value of F(9) is the product of the distances
from the corresponding value of Z to the roots. From this
property one can find that the relative value of F(9) is
largely influenced by the distance from Z to the nearest zero
of F(9) and the more re•ote zeros have less effect. It is
then obvious that the directivity can be increased by increasing
the number of zeros in the range, It should also be noted
that the spacing d of the endfire array, which has a main beam
in the direction 9=0 cannot equal or exceed À/2. If this
does happen, then as 9 varies from 0 to ~ , Z will pass through
the point (9•0) of maximum value more than once as shown in
Fisure 2.2 (b) and (c). The space factor then will have
several main beams and this is not desirable in most cases.
Since the main lobe of the broadside pattern is in the direction
9= rr/2, therefore the spacing d of such array cannot be equal to
or larger than À.
11
12
From the above discussion, the following conclusions
are arrived at:
(a) The spacing d must be less than À/2 for the endfire
array and, obviously, the maximum number of nulls will
be equal to N-1.
(b) The spacing d must be less than ~ for the broadside
array, and the maximum number of nulls in the space factor
can be equal to 2(N-l).
2.2.2 Tchebyscheff Polynomiale
For a symmetrically distributed linear array, the
resulting space factors are
(N-1)/2 F (9) = A + 2 ~ An cos 2n(,8d2 cos 9}
0 0 ~
for odd number of N, and
for even number of N. Let
and
()d cos9 =X 2
cosX =LI.·
the space factors become
F (~) = A + 2 0 0
(N-1)/2 2:. An cos 2n.X= P
0 ( tk
2)
n=l
••••• 2. 9 a
••••• 2. 9 b
••••• 2.10a
•••• 2.10b
•••• 2.lla
13
N/2 and Fe(9) • 2 2: An cos (2n-1)7'.S= U Pe(ll)
n•l •••• 2.llb
2 where P is a polynomial of U with degree (N-1)/2, and
0
2 P is a polynomial of U with degree N/2-1. e
The most desired features of pattern synthesis are
that a specified beam width and minor lobe level can be
obtained by adjusting the complex ratios of the currents in
the antenna elements. Although the complex polynomial
method can preassign the beam width accurately, the minor
lobe level is unknown until one calculates the extreme values.
Another problem of the usual space factor is that the minor
lobe level near the main beam is always the largest among
the minor lobes. If the first minor lobe level is decreased,
the level of other minor lobes is decreased simultaneously.
However, it is seldom necessary to decrease these side lobes
much below the first minor lobe, and in this sense the pattern
is not. bptimal.
Since the space factor of a symmetric array can be
expressed as a real polynomial, it is then possible to equate
the space factor F(9) to a known polynomial which has the
desired properties, and the amplitude distribution of the
antenna array can be obtained by using the method of
undet~rmined~ coefficients. Dolph74
used the properties of
Tchebyscheff polynomials for obtaining the optimum distribution
which bas minimum beam width if the minor lobe is assigned,
or a minimum magnitude of minor lobes if the beam width
is specified.
The Tchebyscheff polynomial is defined by
= cos (n cos-l V)
-1 = cosh (n cosh V)
which bas some important properties.
wh en IVI!::l.
wh en lVI~ 1.
Its maximum absolute
value in the range -1 :!f V~ 1 is smaller than any other real
polynomial of the same degree whose leading coefficient is
unity .. The extreme values of the Tchebyscheff polynomial in
the range -l!GV~l are equal, and the absolute value is
monotonically increasing outside this range. Clearly this
is the desired property for the space factor provided the range
of minor lobes can be made to coincide with the minimized range
of the polynomial. It will be found that not all
configurations can satisfy this condition. According to the
direction of the main lobe and the spacing four classifications
the can be recognized, but onlyAtwo broadside array cases will be
discussed and the two endfire array cases would be considered
in a similar fashion.
14
15
(a) For N-element broadside arrays in which the spacing d
between elements equalsor exceeds À/2, the space factor
is a (N-l)th order function of u as shown in (Eqs. 2-11).
The amplitudes An can be found by equating the space
factor to a corresponding Tchebyscheff polynomial with
variable V. That is:
F(U) '"' TN-l (V)
in wh i ch V = U U 0
where TN_1
(V) is the Tchebyscheff polynomial of (N-l)th
degree and R is the ratio of the main lobe level to the
miner lobe level.
-1 C'
1 1
z Ts(V)
1 1
(U •• R)
1
1 1
-1 1
•••• 2. 12
•••. 2. 13
•••. 2. 14
9=0 ~---------~ 1 . )9=7t/2
9:JLL----------- 1
9=0 ----------~ L- ___ ---------19::1t/2
: 1 jQ=n 1
lO.) l bJ
Figure 2.3 The Tchebyscheff Polynomial of Fifth Degree with the Coordinate Transformations (a) V=u 0 U (for 6 elements broadside array). (b) V=aU+b (for 11 elements broadside array). The loop in each figure is the path of V as 9 varies from 0° to Jt. •
16
The transformation (Eq.2.13) constitutes a scale amplification
which makes the range of U (=cos(~~ cos9)) equivalent to
the range C ~v ~U0 , where C =U0
cos(~d/2) and C=O when
d = Â/2. (Figure 2.3(a)). The minimized range of the
Tchebyscheff polynomial is thus covered by using
transformation (Eq.2.13). The number of nulls of the
space factor, in this case, is equal to,or larger than,
N-1 depending on whether d = .:J\../ 2 or d >./\./ 2.
(b) If the spacing d is less than Â/2 the variable U will not
be equal to zero when 9 varies from 0° to 90°. This means
that the minimized range of the corresponding Tchebyscheff
polynomial cannot be covered if the simple transformation
(Eq. 2.13) is used. For the broadside array with odd
number of elements the space factor can be written
F (9) = 0
A 0
(N-1}'2 + 2 ~ A cos(npd cos9)
n=l n
which is the same as (Eq.2.9a). Let
•.•• 2. 15
U = cos(~d cos9) •••• 2.16
th en N-1 the function F
0(U) will be a (---2-)th arder polynomial
with 2 variable U (not U as it should be in (Eq. 2.lla)).
The Tchebyscheff polynomial T~_ (V) is used with a 2
transformation
V=aU+b •••• 2. 17
17
where a and b are constants which are determined by the
conditions
-1 = a cos ~ d + b ••• 2.18a
Ua= a + b .•. 2.18b
and ••• 2.18c
The values An can then be solved by the following equation:
T·~t [ a cos ( ~ d cos 9) + b J = F 0
[cos (Pd cos 9) J (Eq.2.17) is a linear transformation which enables the range
of U =cos (~d cos9) to be equivalent to the range -1!::: U !:": U0
of the Tchebyscheff polynomial T~ (U) as 9 varies from 2.
0° to 90° (as shown in Figure 2.3(b)). There are thus
exactly N-1 nulls in the space factor.
All the transformations~ which are used in the different
array configurations ensure that the main beam will point in the
desired direction and the number of nulls of the space factor
is equal to or greater than N-1, where N is the number of
elements. If the number of nulls is less than (N-1) the
space pattern is not optimum even if the minor lobes are of
equal magnitude. This is the reason why transformation (b) is
introduced.
It should be noted that in the Tchebyscheff distribution
the amplitude in the inner elements is usually larger than the
amplitude of the outer elements except when R (ratio of main
lobe to minor lobe level) is small. The amplitude ratio of the
center elements to the edge elements reaches maximum when
R ~oo which is the so-called binomial distribution. The
amplitude ratio will be equal to zero when R = 1, in this case~
the amplitude of all the elements are equal to zero except
the edge elements. Thus both the binomial and edge distributions
are the limiting cases of the Tchebyscheff distribution, and the
a•plitude ratio decreases when R decreases.
2.3 The Optimum Pattern of Unequally Spaced Linear Array
The space patternF(cos9) of an antenna array is a
function of the amplitude distribution and spacing. In the
investigations carried out so far, the spacing is usually
specified and one then adjusts the amplitude of the elements to
obtain a desirable pattern. The spacing in most cases is
equal at some arbitrary value. However, if the amplitude and
spacing ean both be adjusted, the optimum utilization of these
two parameters might be achieved. In the following section, a
general method of optimua pattern synthesis with arbitrary
spacing and non-uniform excitation is developed. The
relationship between amplitude and space distribution is
qualitatively studied in terms of an example.
18
2.3.1 Optimum Pattern Criteria
In the section 2.2~2 it was shown that for an equally
spaced linear array with a fixed number of elements and
specified spacing, the optimum amplitude distribution is
usually defined in such a way that, if the minor lobe is
assigned, the beam widtp is a minimum, or conversely, if the
beam width is spe~ified, the minor lobe level is minimized
and thus the space pattern bas equal magnitude minor lobes
and (N-1) nulls.
~t was also shown qualitatively that the larger the
nvmber of nulls that the space pattern bas, the more directive
it is. The maximum number of nulls of an N-element equally
spaced array is usually equal to N-1, and may exceed N-1 in
some cases, but not over 2(N-l). Thus the most important
19
factors for the optimum pattern are the number of nulls which
effects the directivity of the space pattern, and the characteristic
of equal magnitude minor lobes. Bence we shall define the
optimum pattern as one which possesses the following character
istics.
(a) The space pattern bas at least N-1 nulls for N-element array.
(b) The space pattern bas one main lobe and equal level minor
lobes.
The problem of optimum pattern synthesis then centres on the
20
aua\ysis of the function properties instead of dealing with the
polynomial characteristics as is done in the equally spaced
ar ray;
2.3.2 General Equations of Optimum Pattern
Define:
••• 2. 19
where 9 is the direction of the main beam 0
9i is the direction of the ith minor lobe, and
i =~1, 2 ••••• 2(N-l).
Let the ratio of the main lobe level to the minor lobe level
be R. Then the conditions for the optimum pattern can be
described by the following equations:
F ( C( 0
) = R
F( <Xi) = (..:l)i 1 • 1, 2, ••••• 2(N-l)
Ft (cl.) 1 • 0( =<Xi aF j d =0( == o aa 1
i,.. O,l, ••• (2N-3)
••• 2.20a
••• 2.20b
••• 2.20c
Since there are at most 2(N-1) nulls in the space pattern,
the number of equations in the form of (Eqs. 2.20b and 2.20c)
may be 2(N-l). The maximum number of unknowns may be 4N-3 with
2N-3 unknown directions ~1 • In order to obtain the non-trivial
solutions, a set of independent and consistent equations should
21
be chosen from (Eqs. 2.20).
In order to simplify the discussion, a broadside pattern
is used. Since the broadside pattern is symmetrical with respect
to the normal of the array, there are at most N-1 nulls at each
side of the main beam. Equations (2.20) consequently reduce
to the following form:
F(O) = R ••• 2.21a
F(CXi) = (-l)i i = 1' 2, ••• N-1 ••• 2.21b
F' ( O:i) = 0 i = 1,2, •••• N-2 .•. 2.2lc
If the amplitude distribution is specified, there are N/2
or (N-1)/2 unknowns in the spacing between elements depending
on whether N is even or odd. In order to utilize the maximum
number of minor lobes, the following set of conditions is
suggested:
A•F(O) = R
A"F(0:1 ) = -1
A•F'(a.) = 0 :. 1
A•F(.l) = (-l)N/2 (-I)(N-1)/2
where A is a normalizing constant.
2.3.3 Examples
for N is even for N is odd
The following simple examples are given in order to
••• 2. 2 2
22
illustrate the appliAability of the above theory.
A four•element array is chosen with amplitude
distribution A1
and A~ and space distribution ~l and ~2 radians
as show~ in Figure 2.4.
-----~z·--__.}
Figure 2.4 Four~element Array
The space pattern then is
••• 2. 2 3
The normalizing constant is A= R/(A 1+A 2).
Example 1: If the amplitude distribution is uniform, i.e.
A1 = A2 = 1, then (Eq.2,22) becomes
••• 2.24a
.•. 2.24b
cos i'fl +cos 7! 2 "" 2/R ••• 2.24c
The resultant patterns are shown in Figure 2.5, with R=10,20,
30 and 40 and the relationship between R and ~l and 4 2 are
shown in Figure 2.6.
It is worthwhile to note that the spacings ;1 1 and ?J 2
decrease as R increases (Figure 2.6). If R approaches
infinity, it means that there are no minor lobes in the space
pattern. Then the spacing ~l approaches zero and the spacing ~2 approaches n, and the amplitude of the centre element becomes
2. (The centre elements are squeezed together). This is the
binomial distribution with half wavelength spacing. If R is
equal to unity, then ~l = ~2 = 2~ , and the array degenerates
to a two-element one with one wavelength spacing (edge
distribution). These two limiting cases are the same as the
Tchebyscheff distribution.
The total length of the array is generally shorter
than the equally spaced array with half wavelength spacing
except when R is apprionmately smaller than 5 as shown in
Figure 2.6, and the beam width is larger than the array with
Tchebyscheff distribution. This result agrees with the general
theory of antennas, that is, for equal number of elements, the
smaller the aperture, the larger the beam width. However, the
uniform amplitude distribution can be easily obtained in
practice, and the beam width can always be reduced by using
more elements in the array. Thus the optimum pattern of
unequally spaced array may be useful in practical application.
23
E
E
(Q)
t.o..--::----.---,----,--......---------...,.-----ï
1
1
~-------;-----~~-· ---·
l 1
---1--.----tn:--R=~O-·_j_·---i----+-----~-r--·--
1 1 ! 1
·l·--·-·-··--·-· ··-·· . -···· --·······-----l----,-------t--------1
Figure 2.5 Optimum patterns of four-element array with
different value of R.
24
a
25
~0~~+-~~~~--~--------+--------+--------r-------~
4·4-1----
,... z <( ~ 3.8
0:
(!J
z ..... t) 1. 5 ._-4----~ (j)
--+------·---~--1' __ ---~, ---------t----+----+----· --·-·---- . 1 1 1
1 ' 1 :
0.9 ~------~------~--------+--------+--------r-------~------_, __ ___
--~----r----+-----~---~ : 1
0 20 40 GO
R
Figure 2,6 Relationship between spacings and the value
R for the optimum pattern of four-element
array with uniform amplitude distribution • . }
1 1
26
Example 2: If the amplitude distribution is non-uniform,
and the amplitude ratio is A1 /A2 , then (Eq.2.22) becomes:
.•. 2.25a
••• 2.25b
•.• 2.25c
The resulting patterns are shown in Figure 2.7 with R=lO and 30
The spacings .711 and 712 when A1
/A2
::: 0.95 is shorter
th an the spacings at uniform distribution and the spacings -"'1
and 7J2 when A1 /A 2 = 1.4 are larger th an the spacings at
uniform distribution as shown in Table 2.1.
TABLE 2.1 Variations of Spacings ,.1
and ?1 2
with Different
Values of A1 /A 2 and R.
~1 (radian) Jf2
(radian)
R==lO 0.7338 4.1766
R•30 0.2074 3.6680
R=lO 0.8510 4.2353
R=30 0.4310 3.7116
R=lO 1.'4246 4. 7 484
R=30 1.0551 4.0558
1.0~~~----~--~----~----,---~----~--~----~
E
E
1
1 1
R 'Zo.' 1
~------<--+--·-«--+++ :.., ----r·----1
1-----!----~-+----t---t-----L-·-r---. i
Figur~ 2.7 Optimum patt~rns of four-element array with
non-uniform amplitude distribution. (a)«
A1/A 2=0.95, (b) A1
/A2=1.4 .
27
e
e
EXAMPLE 3: If the amplitude distribution A1 and A2
and space
distribution 7}1
and 7{2
are variables, then (Eq.2.21) becomes:
28
••• 2.26
A1 cos ~l + A2 cos ~2 • 1
It is found that the array behaves as an equally spaced
one with Tchebyscheff amplitude distribution. The spacing which can
be easily determined from· transformation (a) Section 2.2.2, depends
..i.. on the minor lobe level R and is larger than J\../2. If the
spacing is d, then for four-element array
u cos 0
~d 2= cos 2n:
3
where U is the same as the definition in Section 2.2.2, 0
transformation (a). 0 This means that, when c< is equal to l(or 9•0 ) •
J F(~)f is equal to 1 which is the extreme value of the Tchebyscheff
v polynomial a=t point C'. as shawn in Figure 2.3(a).
c.orre:spond inj +o +he
2.3.4 The Eq~ivalence Between Amplit~de Distrib~tion and Space Distribution,
The spatial frequency conception, i.e. the equivalence
between the frequency of the radiation and the spacing of the
antenna elements is well known in antenna theory, but the
equivalence between amplitude distribution and space
29
distribution, so far as the author knows, bas not been investigated.
This is done in the present section. However, the problem
is e~tremely difficult to tackle in a rigorous way mathematically,
bence the problem will be investigated graphically based on
Example 2, in Section 2.3.3.
For different values of A1 /A 2 and R, the spac1ngs ~l
and ?f 2 can be obtained by solving Equations (2. 25). The
re 1 a ti ons hi p be tween A1 1 A
2 and })'
1 and 7$
2 are shown in
Figure 2.8. The spacings JJ1
and· 7$2
increase as the value
of A1 /A 2 increases. If A1 /A 2 is less than unity, the spacing
decreases rapidly, and 7$ 1 becomes zero for certain values of
A1
/A2 which depend on the minor lobe levels (1/R).
is larger than unity, the spacing /fl is approximately a,
linear function of the value A1
/A2
•
The above situation can be illustrated by drawing an
analogy to a simple cas~ of a chemical sol~tion. The concentration
of a solution can be increased in two ways; by adding the
A Az
1.4•~------1----·-l------- J i 1
1.2. 1-------·
1.1
o.g
0.8
Figure 2.8 Relationship between A1 /A 2 and spacings x1
and x 2 for the
optimum pattern of four-element array,
4.7 1 7f SPACING
(RADAIN)
w 0
substance which is dissolved in the solution or decreasing the
amount of solvent. The amplitude of each element is analogous
to the substance in the solution and the spacing to the solvent.
For an optimum pattern (or Tchebyscheff distribution in equally
spaced array), it bas been shown in Section 2.2.2 that the
amplitude ratio of the inner elements to the outer elements
increases if R increases and the value is larger than 1 in
most cases. In other words, if the sum of the amplitudes is
constant, the concentration of the amplitude in the inner
elements will be increased by increasing the value of R. If the
amplitude distribution is fixed, as in a uniform distribution,
the only possible way to increase the amplitude concentration
for the inner elements is by reducing the spacing of the inner
elements. This is the reason why, for a four-element array with
uniform distribution, the spacing 2~1 between the two inner
elements is smaller than the spacing ( »2 - ~1 ) between the
inner element and the outer element, and ~ 1 is decreased
as R is increased. If the value of A1 /A2 is less than unity,
the spacing ~l must be smaller than the corresponding spacing
in the uniform amplitude distribution in order to compensate
for reduced amplitude. It is obvious that the spacing ~l will
be equal to zero at a certain value of A1 /A2 • If the value
A1 /A2 is below this critical value, no optimum pattern can
' be obtained by adjusting the spacing. There is also a
similar limitation as ~l is increased. Since the spacing ~l
is limited by two factors: i.e.
31
(a) the spacing 16 2 and
(b) the fundamental characteristics of the single main beam
linear array, namely, the spacing between successive
elements must be less than one wavelength.
Thus the value of A1
/A 2 cannot be increased indefinitely, and
..L the maximum value of A
1/A
2 depends on the minor lobe level R.
Although the analysis is based on the example of a four-element
array, it is believed that the concept is valid for the linear
array with elements more than four.
2.3.5 Sorne Design Considerations for Unequally Spaced Arrays
The design of an antenna system is a manifold problem
which involves the radiation resistance, mutual coupling,
the characteristic of the transmitter, efficiency, accuracy,
etc., and a complete discussion is beyond this thesis.
Ignoring the effect of radiation impedance which is very
important in the practical applications, a qualitative dis-
cussion of pattern formation will be given.
If the spacing is determined according to a uniform
amplitude distribution, the main beam is hardly affected
if the amplitudes or the spacings have ten percent deviation
from the design value, and in some ca~es the half-power beam
width might be narrower than the design value at the expense ,..
of a largely increased minor lobe level; but the minor lobe
32
33
level and the shape of the minor lobe region changes a considerable
amount for large R. The magnitude of the first and second
minor lobes and the half-power beam width corresponding to the
different amplitude and spacing deviations are given in Table 2.2.
A1 /A 2=1, min or lobe level: - 2 0 db ( R= 1 0 ) ' Design values
0 J$1=0.85104, ~2=4.2353 BWH.f. =30.6 '
Factors Deviation Mi nor lobe level (db) BWH.P. % First Second
Al/A2 .. 10 -23 -16.7 29.8°
+10 -17.9 -24.9 31.4°
7fl -10 -17.7 -21.8 30.8°
+10 -23.5 -18.4 30.2°
+10 -10.4 -21.6 28.0°
712 The re are no nulls in -10 the mi nor lobe region. 34.0°
The maximum value cor-responding in the minor lobe region is -18.2 ..
Al/A2 +10 -47.3 -44.8 35°
}.fl & })2 -10
Al/A2 -10 -12 -16.7 27°
/11 & lf2 +10
'\
TABLE 2.2 The minor lobe levels and half-power beamwidth corresponds to the different amplitude and spacing deviations.
It is interesting to note that if A1 /A 2 increases ten
percent and both nl and ~2 decrease ten percent, the minor
lobe level is far below the design value, conversely, if A1/A 2
decreases ten percent and both ~l and ~ 2 increases ten
percent, the minor lobe level increases.
2.4 Summary
A general definition of an optimum pattern has been
introduced based on the characteristics of complex polynomials
and the properties of Tchebyscheff polynomial amplitude
distribution. It has been shawn that the optimum pattern of
a linear array with known amplitude distribution can be
obtained by adjusting the inter-element spacing. If the
relationship between the space distribution and the amplitude
distribution can be further developed, it may be possible in the
future that the unequally spaced array can be considered as an
equally spaced one with non-uniform amplitude distribution.
34
III. CIRCULAR ARRAY PATTERN SYNTHESIS
An array of rotational symmetry with respect to an axis
perpendicular to the horizontal plane is useful in applications
requiring an omnidirectional field or a rotating beam. The
circular geometry has the desired characteristic and a
configuration of a number of identical antennas uniformly
distributed along the circumference of a circle bas been used
in radio direction finding, radar and other applications.
Three variations are used in practice; the vertical dipoles
equally spaced on a circle either with or without a concentric
reflecting cylinder and the slot antennas on a cylinder.
Since the radiation pattern of the array depends not only
on the number of elements, spacing and amplitude distribution
but also on the orientation of the antennas, there are two
problems in the analysis of the curved array, or the circular
array. First of all the antennas of the curved array are
oriented in different directions, and the element pattern and the
space factor are not separable. The usual pattern multiplication
method, which simplifies the analysis in the linear array is
no longer useful. Secondly, the curved array is a two
dimensional problem and the exponential part of the space-
phase term is not a linear function of position. The polynomial
character~stic which is used in the linear array, is not
applicable in this case. As a first approach, a series
35
expression of the element factor and the space phase term is
attempted for the curved array pattern synthesis. This method
is of course limited by the convergence of the series. In
practice, the physical conditions may not fully satisfy the
mathematical conditions which are necessary for the existing
analytical methods. On the other hand, the numerical or the
experimental method for pattern synthesis seems to be promising.
A new method of pattern synthesis for the curved array
will be given in this chapter. The method is valid for any
type of two-dimensional array which is symmetric with respect
to the pattern axis provided that the number of elements is
large enough. The convergence of the Fourier-Bessel series
will be investigated. The circular array with an~stropic
elements will be discussed based on the theoretical analysis of
the circular array with isotropie elements.
3.1 Curved Array of Isotropie Sources
The method of pattern synthesis for the curved array
of isotropie sources to be developed in this section is based
~n a series expansion of the space-phase term. It is applicable
to almost any curved array which is symmetric with respect to the
major axis.
36
3.1.1. Pattern Synthesis
Figure 3.1 Antenna array on a Symmetrical Cl~sed Curve
From Eqs.(2.1) and (2.2) the far field pattern of an
N-element antenna array with amplitude distribution A and n
position vector (dn,an) (n=O, +1, +2 ••• ) as shown in
Figure 3.1 is given by
37
••• 3. 1
where d is the physical distance measured in the same units as n
the wavelength and P= 2X/~. Given the mathematical indentity
jJScos~ e = .m jm~ J (/J)
J e m ••••• 3. 2 m=-œ
where Jm(~) is the Bessel function of the first kind of order m,
and substituting (Eq.3.2) into the general array factor (Eq.3.1),
we obtain:
Jm(~d-1) +. • • •
+Al ~jmejm(9+1Xl) A L._. 3m(rdl) + ...... m•-œ
• • • • • 3 .. 3
If the antenna array is sy~metrical with respect to the
axis 9=0, i.e. A-n= An, and 0( -n = (X n (bence d = d ) then -n n
(Eq. 3. 3) becomes
where)..(N = 1 if the total number of elements N is even
= 0 if the total number of elements N is odd.
By using the identity
m J-m(~) = (-1) Jm(~)
Equation 3.4 can be written as
••••• 3. 4
••••• 3 .. 5
38
where E = 1 for m = 0
= 2 for m ~ 0
F(&) above is the pattern produced by a physical antenna
array (Figure 3.1). However. the amplitude distribution
A and bence F(&) are yet undefined. In pattern synthesis, the n
aim is to find an amplitude distribution that produces a
desired pattern for a given antenna system.
If the desired pattern S(&) is symmetric with respect to
the axis &=0, and also expressible as a Fourier series, then
00
S (&) = ~Sm cosm& ••••• 3. 6 m=o
where S are the Fourier coefficients and are determined by m
the pattern specification.
Equating 1
Eqs .. (3.5)and(3.6) we have
S /J.me = A J (Ad ) + 2A a J (Rd ) 2A a J (Ad ) m 0 m r 0 1cosm 1 m r 1 + zcosm z" m r 2
••••• 3. 7
where m = 0, 1, 2 ••• Since d and d are known, there are n n
(N+2)/2 (when N is eve~) or (N+l)/2 (when N is odd) number
of unknowns of the amplitude A , in other words, the number n
of equations is dependent on the number of elements used.
39
40
In order to illustrate the applicability of the above theory,
the following examples will be considered.
3.1.2 Examples:
In the following a specified pattern is synthesized by
using different geometrical configurations of the array, and
(Eqs. 3.7) will be used throughout this section.
Assuming the specified pattern to be defined by
8 (9)= 1
=0 - 7t < 9 < - i' and ~ < 9 < 1C ••••• 3. 8
then the Fourier expansion of 8(9) is
8{9)= di j~+ cos9 + ~ cos29-! cos49-; cos59 + ••• } ••••• 3.9 11: l3J3
Mathematically the Fourier series should have an infinite
number of terms. In practice, the specified pattern S(9) can
usually be approximated, to a sufficient accuracy, by means of
the first few terms of the Fourier expansion. The above
ideal specified pattern and its approximation with five terms
of the Fourier expansion are shown in Figure 3.2~. Because
the pattern is symmetrical with respect to 9=0, only half of
the pattern is shown in the Figure. In order to simplify
the calculations, some simple array configurations are
illustrated in the following.
CONFIGURATION I: Ten-element array equally distributed on
the circumference of a circle with radius d=~/2.
If the curve is a circle, then d0
= d 1 = d 2 ••• :d,
and (Eq. 3.7) becomes
41
••••• 3. 10
For the 10-element array, the number of equations will be
equal to six. Since it is equally distributed, then
a = n1C/ 5 n
The relative currents are
A0
= -2.576 - j 0.3712, A1= -0.535 - j 2.217,
A2= -0.9194 + j 0.6173, A3= -0.9194 - j 0.6173,
; A 4 = -o. s 3 s + j 2. 211 , A5= -2.576 +f o.3712.
The r esu 1 tàn t normal i z ed pat te rn i s .shown in Fi gu re
3.2b, and it is fairly near to the approximated Fourier
expansion. Although the minor lobe level is slightly higher
E
{Q)
Figure 3.2 Resultant patte~ns of different array configu
rations.(a) The specified pattern and the
approximated pattern by using five terms of
Fourier expansion, (b) The equally spaced
circular array.
42
th an the specit.fi ed pat te rn, ne ver the 1 es s, the shape of the
main lobe is almost the same.
Configuration II: Let the elements be unequally distributed
along the circumference of the circle with d•J\/2, and let
the corresponding angular distribution (chosen arbitrarily)
0 Cl( 5 = 180 •
By solving (Eqs. 3.10) the relative amplitude can be obtained
as follows:
A = - 0.412 + j 1. 0441, Al = 0.1795 - j 1.580,: 0
A2 = 0.226 + j 0.03887, A3 = - 0.134 + j 0.0914,
A4 = 0.276 + j 0.114, A = 5 0.681 + j 0.291.
The resultant normalized pattern is shown in Figure 3.2c.
Although the resultant pattern is not as good as the pattern
of equally distributed array as shown in Figure 3.2b, it is
felt strongly that a pattern with small ripple and small minor
lobe level may be obtained by properly adjusting the spacing.
Configuration III: lü-element array, equi-angular distribution
along the sides of a square with diagonal 0.954 ~ (Figure 3.3).
43
As
Figure 3.3 10-element Array Equi-angu1ar Disttibution Along the Sides of a Square.
The distances from the centre 0 of the square to the
elements are
d = 0.477 >.. 0
dl= 0.342J\. • d2 = 0.379 À.
Then (Eqs. 3.7) become
44
••••• 3. 11
where m = 0, 1, 2, 3, 4 and 5. Solving (Eqs.3.11), the
following relative amplitude distributions are obtained.
A0
= -0.39995 + j 0.46603, A1 = 0.22487 - j Q.71552
A2 = -0.00452 + j ~.67279, A3 = 0.00452 - j 0.67279,
A4 = 0.22487 + j 0.71552, A5 = -0.39995 - j 0.46603.
E
E
0oL---------30~--------6~o---------g~o----~----~2~o---J----~,s~o--~----~~eo 9
(C)
oL---~--~----L---~~~--~----~--~--~----L---~--~ e 0 60 90 120 ISO 180
(d)
Figure 3.2 (c) The unequally spaced circular array,
(d) The equi-angular spaced square-array.
45
The resultant normalized pattern is shown in Figure 3.2d. It
will be noticed that the main lobe is quite close to that of
the approximate specified pattern of Figure 3.2a, but the
minor lobes are larger.
From the above examples, it is shown that (Eqs.3.7)
can be used in the synthesis of antenna arrays of a·.variety
of geometrical configurations. It is evident that the agreement
of the resulting pattern with the specified pattern depends on
the geometrical configuration concerned.
3.1.3 The Convergence of the Space-Phase Series
It should be noted that the above pattern synthesis
method is general in that it is not restricted only to arrays
of simple geometrical shape (i.e. circular or square arrays),
but is applicable also to arrays of arbit~ary shape as ,long as
the geometrical configuration of the array is symmetrical with
respect to 9=0. However, the number of elements used in
the array is not arbitrary. Since the derivation is based on
the series expansion of the space-phase term, therefore the
minimum number of terms used must be such that the space-phase
term ls. reasonably represented by the series expression.
Otherwise, a large~ror will be introduced.
example illustrates this.
The following
46
47
Consider a 10-~lement array with equally distributed
elements on the circumference of a circle of radius one
wavelength. (Eqs. 3 .10) become
Where m=O, 1 ••••• 5. The resultant normalized pattern is
shown in Figure 3.4a. Although the main lobe is almost the
same as shown in Figure 3.2a, nevertheless the minor lobe levels
are rather high. This can be shown to be due to the poor
approximation of the space-phase term:
Consider the space phase term
••••• 3. 12
Since, for the 10-element array, there are only six unknowns in the
amplitude distribution, then only six terms of the expansion
(Eq.3.12) are utilized. However, from Figure 3.5, it is evident
that the higher order coefficients are still appreciably large
and hence our approximation (Eq.3.12) of the space-phase term is
poor.
If a 14-element array is used, then the space-phase
term will be given by eight terms of the expansion (Eq.3.12)
and it can be seen from Figure 3.4 that the last coefficient
1.0
E
1.0
E
"" v !\ 1
.~ '
1 1
1 1
1 i ' 1 ; ! 1
. ·--··'
1 i
1
------ 1 1 !
1 1 1
1 \ 1 1 1 1 ' 1 1
!
\ ! 1 1
1 l --
i \ n~/1\Vv~/ 180 ° 120 !50
Figure 3.4 Resultant patterns of the circular array;
(a) 10-element array, (b) 14-element array.
48
JT(2~) of the series (Eqs.3.12) is sufficiently small sa that
the higher arder terms can be neglected. The designed pattern
for the 14-element array is shown in Figure 3.4b and is
definitely far superior ta that of the lü-element array shown
in Figure 3.4a.
A general "rule-of-thumb 11 for the minimum number of
elements required for a circular array of any radius can be
obtained as follows. From the theory of Bessel functions,
Renee in the expansion 1
(Eq.3.12) terms of order higher than m may be ignored, where
m is the nearest integer larger than ~ d.
elements is then given by 2m.
The number of
3.2 Continuous Distribution and Circular Array.
It has been shown in Section 3.1 that any pattern which
can be approximated by a truncated Fourier series can, in
principle, be obtained from the curved array by adjusting the
amplitude distribution. If the closed curve is one of the
simple geometrie curves, such as the circle, ellipse etc.,
the antenna array is often discussed by using contin~ous
distribution. The equivalence between the discrete array and
the continuous distribution has been investigated by many
50
51
authors, and the method, which uses the amplitude of continuous
distribution as the envelope of the amplitude of equi-spaced
circular array has been used for a long time. Nevertheless,
the problem of minimum number of elements to replace the
continuous distribution has never been fully investigated. In
this section the relationship between the methods of continuous
distribution and the discrete array will be discussed.
3.2.1 Pattern. Synthesis by Using Continuous Distribution
Let the current be continuously distributed along the
circumference of a circle with radius d, amplitude A(a) and
phase ~(a). The far field pattern on the horizontal plane is
2n:
F(9)·J A(a)eJ(fd ••••• 3. 13
0
p
6=0, 01=0
Figure 3.6 Continuous Distribution with Amplitude A(ot) and Phase y(cc) •
52
If the amplitude is constant along the circumference and
the phase distribution is a linear function with total phase
shift 2m~, where mis any integer, then (Eq.3.13) becomes
21[
F(ll)• Am J ej (,dcos(ll-«)-mOtJda
0
••••• 3. 14
If the amplitude distribution is A cosm« , and the phase is m
constant, then the far-field pattern is
F ( 9) • 2 Jt € j mA J ( R d) c os m9 mm f"'
••••• 3. 15
If the specified pattern is symmetric with respect to the
axis 9=0. and ~t can be expanded as a eosine series, such that
00
S(9)= L m=O
S cosm9 m
••••• 3. 6
then the current distribution along the circumference will be
cosma" ••••• 3. 16
(Eq.3.16) is the solution for the continuous current distribution
provided that the series is convergent. In practice the number
of terms is usually finite for a reasonable design.
If the continuous distribution is represented by the
discrete array of 2N elements, then from (Eq. 3.16) the ampli-
tude of the nth element at the angular coordinate ex is n
53
Sm cosm<X
n ••••• 3. 17
The upper limit in (Eq.~3.17) is chosen to be equal toN. The
reason for this will be discussed in Section~3.2.2.
(Eq. 3.17) is equivalent to (Eqs.3.l0) if the 2N elements
are s .. paced equally along the ci r cumference. The proof is
given as follows.
Assuming 2N elements are used in the circular array, then
there are N+l equations in the form of (Eqs. 3.10)
••••• 3. 18
where m=O, 1, 2 ••• N. Since the elements are equally s~aced,
th en
and (Eqs.3.18) become:
m=O,l,2 ••• N.
Multiplying both sides of the above equations by cosmKa and
sqmming all the equations, we have
i {A0+2A1 cosmOl +2A2cos2m0l + ••• +ANcosNmOl} cosml<IX
m•O
N
54
-L cosmKOC ••••• 3. 19 m==O
N Si nee 2, cosmKCX =0
m=o
when NCX = 7t and ~ is integer. Therefore (Eq. 3.19) yields the
following:
N
Nl ~
AN = ~ m•o
s m cos mn()( ••••• 3. 20
' It is clear that (Eq.3.20) is the same as (Eq.3.11) except for
a constant multiplying factor which has no consequence on the
pattern.
3.2.2 The Upper Limit of m
It has been assumed in (Eq.3.17) that the upper limit of
m is N where N is half the number of elements. It will be shown
that this upper limit need only beN and not higher. To do this,
55
suppose the upper limit is N+l, then from (Eq.3.17) the
amplitude of the nth element is
N+l -m
A n
1 = 2:n: 2:: j cos mor
n ••••• 3. 21
m=O
Since there are 2N elements equally distributed on the circumfer-
ence then
and hence cos(N+l)Ql = cos(ll}{+()() = cos(n7C-Cif) n n n
= cos ( N -1) CXn ••••• 3. 22
With the help of (Eq.3.22), the last term of (Eq.3.21) i.e. the
term m=N+l, is reduced to the form
cos(N+l)<Xn = j-(N+l)
cos (N-1)0( n
In other words, the term m=N+l can be combined with the term
m=N-1 and in general terms of order higher than N can be
combined with terms of order correspondingly lower than N.
Renee the upper limit need only be N. In fact if the upper
limit exceeds N, the pattern will degrade as illustrated by
' the following example:
The amplitude distribution of a 14-element equ~angular
circular array is given by (Eq.3.17)
A n
1 --2n j
-m
If the specified pattern is the same as in Section 3.1.2, and
the radius d is one wavelength, then the resultant pattern will
be the same as shown in Figure 3.3b.
includes two extra terms:
1 27t
9
~ m=8
j -m s
m
If the expression of A n
the resultant pattern is shown in Figure 3.6. Comparing with the
pattern ~n Figure 3.3b it is found that the minor lobe level
in Figure 3.6 increases by a large amount.
3. 3 Circular Array of AnLsotrQpi.c · Element;s
If the element pattern of each antenna is f(~), the
far-field pattern of an N-element equally spaced circular
array with amplitude distribution A is given by (Eqs.2.1 and n
2.2) whereby each term is multiplied by its respective pattern f.
57
.,-P
-----8=0" Ao
Figure 3. 7 Circular Array wi th ~tsotrqp.ic .Element;s
58
••••• 3. 23
where CX = 27C/N.
d is the radius of the circle.
In practice, it is usually possible to express the
element pattern approximately by a truncated Fourier series.
Since the element pattern is symmetrical with respect to the
axis of the element antenna, then f(9) cau be written in the
following form:
K
f(9)= L k-K
••••• 3. 24
where ~k=fk. By using the mathematical identity {Eq.3.2)
and with the symmetric condition A =A , the far-field pattern -n n
of the array becomes:
59
••••• 3. 2 5
Since the antenna system is symmetrical with respect to
the axis 9=0, th en the final exp res si on of the far -field pat t.ern
is in the following form:
1!(9)=± fA0
J!m+2A1 •Fm"cosmOC +2A 2 •J!m"cos2mfX+ •••
m•O
••••• 3. 26
where F m In fact (Eq.3.26) is
in the same formas (Eq.3.4) when d0
=d1=d
2= ••• Although the
constants Fm are more complex than the constants Jm(Pd} in the
circular array with isotropie sources, nevertheless the series
Fm is just an algebraic combination of fk and Jp(~d) and it
suffers the same defects as the series Jm(Pd) in the
circular array, i.e. slow convergence of the series. Because
of this it is impractical to apply the method to the design
of circular arrays at microwave frequencies using conventional
aperture antennas as the an~sotro~ic ·elemerits. The limitation,
however, is purely physical as discussed below.
In Section 3.1, it has been shown that for the
circular array with equally spaced isotropie elements the
minimum number of elements required is the nearest integer larger
The length of the circumference is equal to 2nd, and
hence the spacing between each element is approximately equal
to 2~d/2~d or Â/2. If we stipulate that the convergence of
Fm and Jm(~d) be roughly the same then it is reasonable to
expect that the number of elements in the circular array with
ani~tropic sources will be approximately the same as that with
isotropie sources, and therefore the spacing between each
element will also be equal to Â/2. This spacing is too small
for most aperture antennas when used as the antenna element
in the anisotrop1c arra,y •• However, this does not rule out
the possibility of using aperture antennas for the circular
array. It only means that the above theoretical approach
60
cannot be applied. When theory fails, it is perhaps natural
to aonduct some simple experimente to see if it is possible
to obtain some idea as to the best future approaah.
61
IV. EXPERIMENTAL STUDY OF THE CIRCULAR ARRAY WITH~NlSOXROPIC
ELEMENTS.
4.1 Introduction
In the previous chapter, it has been shown that the series
expansion method fails if aperture antennas such as horns or
parabolic reflectors are used as the elements for the circular
array. Since no other analytical method seems to be readily
available, it may be useful to investigate experimentally the
characteristics of the circular array wi th ani'.s:o:t-rqpi~ 'e.leme.n:t:s
to see if a correct approach could be devised. In this chapter,
the far-field pattern of a set of horns which are equally
distributed along the arc of a circle will be measured and
based on the measured results, several conclusions will be
drawn.
4.2 Experimental Arrangement
The problem of far-field pattern measurement consista of
two parts: the site of the transmitting and receiving antennas,
and the detecting equipment. For a small aperture antenna
system with moderate beamwidth, two factors have to be
considered for the choice of a site: (a) the distance between
the transmitting and receiving antennas and (b) the freedom
from ground and other reflections.
62
It is well known that to approximate a plane wave
condition the distance R required between the transmttting and
2 receiving antennas must be larger than or equal to 2D /À where
Dis the aperture dimension of the tested antenna and~ is·
the wavelength of the radiation, both measured in the same
units. For the circular array, the aperture may be defined
as the largest distance measured in a straight 1ine between
any two of the antennas in the array. For instance, if the
antennas are distrmbuted on the arc which is 1arger than the
ha1f circle, the aperture will sti11 be equa1 to only the
diameter of the circle. In the fol1owing measurements, the
largest aperture of the tested antenna system is approximately
equa1 to 46 cm and the operating frequency is 9.34 KMc/s.
(X-baad), i.e. ~-3.2/cm, thus
2x46 2 R ~ • 13.2 meters.
? 3.21
In Figure 4.1, it is shown that the actua1 distance between the
transmitting and receiving antennas is approximately equal to
63
17 meters, which means that the site satisfies the phase criterion
for the far-field measurement •.
In the measurement of a far-field pattern, complete
freedom from ground and other reflections is impossible.
However, the ref1ections can usually be minimized by c~rtain
methods, such as tilting one of the antennas upwards so that the
r ' l
1 e' lfl .....
~~~~~~~~~~~~~-~~~--~'.-. ~~~~~~~~~~~~~~~~, APPROX. 40M
64
ABOVE GROUNO
Figure 4.1 The physical dimensions of the transmitting
and receiving antenna towers.
Klystron Power f---Supply
Tested
Antenna
Power
Di vider
Rotary
Joint
Isolator
V-55 B
Klystron
Parabolic
Reflector
Crystal
De tee tor
Rota ting
Table
A. F.
Amplifier Il Il
D. c. Selsyn
Mot or Mo tor
1 f Intensity
Variable Position o.c. Power
Supply Indicator Indicator
Figure 4.2 Block diagram of the equipment arrangment.
Single line representa electrical connection
and double line representa mech~ical coupling, A
first null of the vertical beam points towards the reflection
point, or placing absorption screens or diffracting edges
halfway between the two sites. Since the test range is
located on the roof of the highest building on the campus,
there are no reflections from surrounding objecta. The heights
of both antenna towers is 4.3 meter above the roof, and both
the transmitting and receiving antennas are highly directive
in the vertical plane, so that groundward radiation from the
transmitting antenna and the groundward reception of the
receiving antenna are very small.
The detecting equipment consista of two parts; the
position indicator and the crystal detector. The position
indicator is synchronized to the rotating table by selsyn
motors. The crystal detector is an ordinaryone used in X-band.
Its output is connected to a VSWR meter which is used as
an a-f amplifier and intensity indicator. The crystal detector
and VSWR meter combination are calibrated by means of the r-f
substitution method. The patterns obtained here were measured
manually, since a fully automatic recording system was not
yet completed.
The source of r-f power is a modulated reflex klystron
V-55B with an output of 240 mw. The radiated frequency is
9.34 KMC. A block diagram of the equipment is shown in
Figure 4.2.
65
66
4.3 Measurements: The Circular Array with Anistropic Elements.
The antenna system consists of three horns and a power
divider. The power divider is made up of two tees, so
connected that there are three outputs and one input. A
variable attenuator and a variable phase shifter are connected
between each output and each horn. Connection to the horn
itself is by means of a coaxial cable in order to facilitate
positioning the horn. The intensity and phase of each horn
can be adjusted separately. The adjustments are carried out
with the aid of the automatic phase and intensity recorder
in the Microwave Optics Laboratory**· (This equipment is
capable of measuring phase and intensity independently and it should
be noted that without it the experiments here would have been
virtually impossible!).
The array configur,tion is shown in Figure 4.3
~~\ / : \. ,' 1 1 \ /
1 \ ' ,..r
A --~~ . .ffi ..... -----~ odb
Figure 4.3 •. The Array Configuration of the Circular Array with Anistropic Elements. A is the intensity ratio of the two outer horns to the centre horn.
**T.J.F.Pavlasek, "An Automatic Phase Plotter for the Measurement of Microwave Fields" Ph.D.Thesis, McGill University, April, 1958.
T.S .. Kho, "Automatic Recording of Microwave Field Intensities" M.Eng~Thesis, McGill University, April, 1962.
Two series of measurements were carried out, the phase of the
horns being kept equal in both cases. In the first case the
amplitude distribution of the array was varied with the radius
of the circle, or the arc, kept constant. The measured patterns
with d=21.3 cm and variable A are shown in Figures 4-6. In
the second series of measurements the radius d was varied but
the amplitude distribution was kept constant at (-6 db, 0 db,
-6 db). The measured patterns are shown in Figures 4-5. From
these two series of measurements, the following conclusions
can be drawn:
(a) The ripples at the main beam increase as d increases.
(b) The ripples at the main beam increase as A increases.
(c) There are always two very low minimum points in the main
67
bearn, the beam width between these two points being
approximately constant except for the cases of d=40.4 cm and
A=O db.
(d) The beam width of the resultant pattern is slightly larger
than the bea~~idth of the element antenna.
(e) The number of ripples is constant except for the cases d=40.4cm
and A=O db.
The main disadvantages of the resultant pattern is the violent
fluctuations at the main lobe. From the results, it seems
possible that the fluctuating effect can be reduced by
-+------+-----+---±"----t----t----1-
180 60
>~ ..... tl} 2 w 1-z H
---- ----------- -------- - :lO. ---
- 0 0
Figure 4.4 Far-field pattern of single horn.
0
-30 0
(C\)
1
1
i
120
68
e
Figure 4.5 Far-field pattern of three-element array with fixed
amplitude distribution A=-6 db; (a) d=21.3 cm.
1-1-4 [1) z w ...
0
~-20
69
__ .[ __
...... ~--L....L..--:-*.;:::-----'-~~--.....L-~-3::..::::0_.L-._~__......__"I?!;;:;----fr~ o ISO e tb)
0
(C)
Figure 4.5 (b) d=22.6 cm, (c) d=25.4 cm.
8
A--•>no•
1
!
---~·-· 1
1
i 1
(1 f'l
ni\ n n 1 180 1 20
-r-- 1
i 1 1 1
····t .. 1 -"''""-·
1
1
1 1
...
~ " J 1
1 1 180 120
n
1 ·-------~~--~··-·
Q
.
" rv
..
60
J
1 1
1
1
1
! 1
1
60
"' r,
,
·10
-2()
~ >-.... ..... Il)
z w 1-:z H
-30 0
0 .. ,.
.- ... ::-IC
l-2t ...Q
"0
>-..... ..... Cil z I.U 1-z ....
-3D 0
te,
70
1 - 1 -
,.,
r\ --·-
' 1
1
1
U1 1 t
·1 1 1 1 1
·---- ------1 1
1
1 1
f ~~ \1\ fl 1\ A
60 120 ISO fi
1 ~ . i i
1 1
1
1
'
IJ'I1
__ _lo ~
' :
60 120 180 \J
Figure 4.5 (d) d=27.7 cm, (e) d=40.4 cm,
1 -r--- -----+
>-1-H (/) z w .... z ......
71
20 -· j
-~()
0 12C tao e (Q)
0 - J __ !
·20
=@ )-
1 ,_
~--~~~-~~~0~~~~~ IGù 120 60 0 60 120
<b> Figure 4.6 Far-field pattern of three-element array with
fixed radius d=21.3 cm; (a) A=O db, (b) A=-9 db,
... ~ 1-2 1-1
72
0
--~~~----~----~~~--------~-3~0------~~~------~--------~~9 120 0 60 120 180
180 120 60
(Ç)
_0 __ ~~-
.0 "0
).. ... .... Il) z
i
!
-20
Figure 4.6 (c) A=-12 db, (d) A=-15 db.
--------·-1 l 1
180
reducing the radius d, but d is limited by the physical dimension
of the element antenna. Although the resultant pattern is no
better than the pattern of a simple horn, however, there exista
the possibility of steering the resultant pattern of the array
by varying the amplitude of è~ch antenna. For instance, for
the four-element array if the geometrical configuration is
defined.'.by 9=30'0
and d=21.3 cm and thé ampÙtude distrlbution
is (-"6· db, ·o d·b, ..,'6db) w·ith one edge element non-excited, the
resultant pattern is shown in Figure 4.7a. If the amplitude
distribution changes to (-9.5 db, 0 db, 0 db, -9.5 db), the
resultant pattern is shown in Figure 4.7b. It is evident that
the direction of the main pattern is changed as expected.
This fact should form the basis of an extensive experimental
investigation.
73
V. CONCLUSION
Although the problem of pattern synthesis of antenna
arrays has been tackled for several decades, it is surprising
that only few successful methods are available. In particular,
74
the problem of the unequally spaced linear array, of the curved
array and of the circular array wi th anLs:d:trop.i-c re.lement:,s have
seldom been discussed in the literature. It has been the purpose
of this thesis to investigate possible methods of pattern
synthesis for the antenna arrays mentioned above. Sever al
methods have been examined but further research is required.
Hitherto, the optimum pattern of an antenna array has
been designed for the equally spaced array by adjusting the
amplitude distribution. In this work, a new method of optimum
pattern synthesis has been devised. It has been shown that the
optimum pattern of a linear array with fixed amplitude
distribution can be obtained by adjusting the antenna spacing.
The relationship between the space distribution and the
amplitude distribution has also been discussed by means of an
eKample. The rigorous mathematical analysis is extremely
difficult and needs further development.
The author has developed a pattern synthesis method for
the general curved array with isotropie sources. The method
ii applicable to any array configuration as long as the array
is symmetric with respect to the pattern axis. It is believed
that for a fixed number of elements and a specified pattern
there is an optimum array configuration which will result in the
best agreement between the resulting pattern and the specified
pattern. The series expansion method is unworkable if applied
to arrays with ani.s'Otropic .source:s_, due principally to the physical
size of such antennas. A simple experiment has been performed
to substantiate certain salient points of such arrays.
The ultimate objectives for the present study of pattern
synthesis for antenna array is to solve the problem of electronic
0 steering of the antenna beam through 360 • If a suitable
element antenna can be obtained for the circular array of
ani.sotr.op.ic ·sour.ces,, it is quite possible to achieve a scanning
pattern by v~rying the amplitude of each element. Alternively,
other theoretical approaches should be investigated such as
expansion of the space-phase term and the specified pattern by
some other series that have better convergence properties
than the Bessel-Fourier series used in this work. Certainly
the proDlem is a very difficult one and is no-where near a
,EiOlution. It is hoped, however, that the work here is a
small contribution towards that end.
75
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80
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81
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