U.S. patent number 3,707,719 [Application Number 05/132,765] was granted by the patent office on 1972-12-26 for scanning aerial systems and associated arrangements therefor.
This patent grant is currently assigned to The Marconi Company Limited. Invention is credited to John Richard Mark.
United States Patent |
3,707,719 |
Mark |
December 26, 1972 |
SCANNING AERIAL SYSTEMS AND ASSOCIATED ARRANGEMENTS THEREFOR
Abstract
An electronic scanning aerial system and associated feeder
arrangement has at least one circular aerial array. Elements of the
array are divided into sets and units, each set comprising the same
number of adjacent equally spaced elements and each unit comprising
a number of different corresponding aerial elements, at least one
in each set. A power dividing system provides power to different
combinations of aerial elements, the combinations depending upon
the general direction of radiation. The power dividing system
includes a four port coupler, the ports remote from the aerial
units being connected to two binary branching arrangements whereby
sum signals are produced at one of the binary branching
arrangements and difference radiation pattern signals at the other
binary branching arrangement.
Inventors: |
Mark; John Richard (Essex,
EN) |
Assignee: |
The Marconi Company Limited
(London, EN)
|
Family
ID: |
10115965 |
Appl.
No.: |
05/132,765 |
Filed: |
April 9, 1971 |
Foreign Application Priority Data
|
|
|
|
|
Apr 18, 1970 [GB] |
|
|
18,642/70 |
|
Current U.S.
Class: |
342/371 |
Current CPC
Class: |
H01Q
3/34 (20130101); G01S 13/4409 (20130101); H01Q
3/242 (20130101) |
Current International
Class: |
G01S
13/00 (20060101); H01Q 3/30 (20060101); G01S
13/44 (20060101); H01Q 3/24 (20060101); H01Q
3/34 (20060101); H01q 003/26 () |
Field of
Search: |
;343/1SA,854 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Borchelt; Benjamin A.
Assistant Examiner: McCabe; Denis H.
Claims
I claim:
1. An aerial and associated feeder system adapted to provide
electronic scanning of space said system comprising an aerial
system consisting of a plurality of aerial elements spaced along a
circular arc, said elements being divided into sets and units each
set consisting of the same plurality of adjacent equally spaced
elements and each unit consisting of a plurality of different
corresponding aerial elements, at least one in each set; and a
power dividing feed system divided into unit feeder arrangements
each leading to the aerial elements of two different units through
switch means whereby different predetermined combinations of aerial
elements may be selected for connection to the unit feeder
arrangement therefor to determine the general direction of
radiation, there also being provided, in the path to at least one
of the two units fed by each unit feeder arrangement, adjustable
phase shifter means for adjusting said general direction of
radiation and wherein each unit feeder arrangement includes a four
port -3db coupler, the first of the two ports remote from the
aerial units of each of the said couplers being connected to a
first binary branching arrangement and the second of the two ports
remote from the aerial units of each of said couplers being
connected via adjustable phase shifter means to a second binary
branching arrangement whereby in operation sum radiation pattern
signals are obtainable by said first binary branching arrangement
and difference radiation pattern signals are obtainable by said
second binary branching arrangement.
2. A transmitting system in accordance with claim 1 wherein signals
applied to the single path of the first binary branching
arrangement are transmitted in accordance with a sum radiation
pattern whilst signals applied to thesingle path of the second
binary branching arrangement are transmitted in accordance with a
difference radiation pattern.
3. A receiving system in accordance with claim 1 wherein sum
radiation pattern signals appear on the single path of the first
binary branching arrangement and difference radiation pattern
signals appear on the single path of the second binary branching
arrangement.
4. A system as claimed in claim 1 wherein each of the adjustable
phase shifter means leading to said second binary branching
arrangement is a two-bit phase shifter adapted to provide a phase
delay of either zero or 2.pi. radians.
5. A system as claimed in claim 1 wherein said phase shifter means
provide zero phase delay when corresponding elements in the units
are selected and a phase delay of 2.pi. radians when elements which
do not correspond in the units are selected.
6. A system as claimed in claim 1 wherein corresponding elements in
adjacent sets are spaced arcuately by 120.degree..
7. A system as claimed in claim 1 wherein each unit feeder
arrangement includes between said -3db coupler and the two units
fed thereby, and prior to said phase shifter means provided to
adjust said general direction of radiation, a hybrid unit whereby
equal power is fed to each of the two units.
Description
This invention relates to scanning aerial systems and associated
feeder arrangements therefor and more specifically to space
scanning aerial systems and associated feeder arrangements therefor
of the kind in which at least one circular aerial array, i.e. an
array comprising aerial elements lying on the circumference of a
circle, is fed through a controllable feeder arrangement which is
such that the aerial can scan space in azimuth without being
mechanically moved. Such scanning, which is usually called and is
herein called "electronic scanning" may simply be scanning in
azimuth or there may be scanning in elevation as well.
FIG. 1 of the accompanying drawings is a schematic diagram of a
known electronic scanning aerial system and associated feeder
arrangement therefor, similar to one of the embodiments of the
invention disclosed in our U.S. Pat. No. 1,171,626, whilst
FIG. 2 of the drawings is a representation of a plan view of the
aerial array of FIG. 1 and incorporates a radiation diagram.
Referring to FIGS. 1 and 2, a plurality of aerial elements in three
sets, a.sub.1 to a(n/3), b.sub.1 to b(n/3) and c.sub.1 to c(n/3),
are arranged around the circumference of a circle, each directed to
radiate radially outward. Although, for convenience in drawing, the
sets of aerials are represented, in FIG. 1, as though they were in
a straight line, it is to be understood that they are not so in
face and that the elements in the set a.sub.1 to a(n/3) are
disposed along a first 120.degree. arc of a circle, the elements in
the set b.sub.1 to b(n/3) along the following 120.degree. arc of
the circle and the elements in the set c.sub.1 to c(n/3) along the
remaining 120.degree. arc of the circle. The subscripts used relate
to the position of the element in its set along the arc of the
circle. The total number of elements provided is normally a
multiple of six.
The aerial elements are arranged to be fed in pairs, in dependence
upon the directivity required. Thus for example, elements a.sub.1
and a(n/6) may be fed together, elements a.sub.2 and a(n/6 + 1)
would be fed together and so on.
The feeding arrangements for the elements shown in FIG. 1 show, on
the left as viewed, the arrangement for feeding in pairs any one of
elements a.sub.1, b.sub.1 and c.sub.1 forming a unit, with any one
of elements a(n/6), b(n/6) and c(n/6) forming a unit. To the right
of the figure as viewed is shown the arrangement for the general
case of feeding in pairs any one of elements a.sub.i, b.sub.i and
c.sub.i forming a unit with any one of elements a(i + (n/6), b(i +
(n/6) and c(i + (n/6) forming a unit, where i is any integral
number from 1 to (n/6).
The aerial elements are fed from a common source CS (which may be a
transmitter or a receiver) via a binary divider B having as many
output paths OP as there are elements in a set, i.e. (n/3). The
output paths OP are applied in pairs to the two input ports of a
different - 3db coupler C.sub.i, of which there are (n/6). One of
each pair of output paths OP is connected to its associated - 3 db
coupler through a different phase shifter .phi.'.sub.i, which, of
course, again there are (n/6), one for each - 3db coupler. The two
output ports of the coupler C.sub.i are connected via respective
phase shifters .phi..sub.i and .phi.(i + (n/6) to the input
terminal of a respective switch S.sub.i and S(i + (n/6).
Switch S.sub.i connects the phase shifter .phi..sub.i to the
elements a.sub.i, b.sub.i or c.sub.i of a unit at will, whilst
switch S(i + (n/6)), corresponding connects phase shifter .phi.(i +
(n/6)) to elements a(i+ (n/6)), b(i+ (n/6)) or c(i + (n/6)) of a
unit.
To explain the operation it will be assumed that a beam is required
to be produced in the direction of the a(n/6) radial. All the
switches S.sub.i are operated to select the "a" elements. The phase
shifters .phi..sub.i are adjusted to give the required power
division between the switches S.sub.i and S(i + (n/6)) appropriate
to the illumination taper required, whilst the phase shifters
.phi..sub.i and .phi.(i - (n/6)) are adjusted to produce in-phase
signals at a reference plane in space which is perpendicular to the
a(n/6) radial. To effect small beam shifts about the direction of
the a(n/6) radial the phase shifters .phi..sub.i and .phi.(i +
(n/6)) may be adjusted. For larger beam shifts, the switches
S.sub.i have to be re-operated. For example, if the beam direction
is moved from the a(n/6) radial to the a((n/6) + 1) radial, the
switch S.sub.1 in the case must be switched from element a.sub.1 to
element b.sub.1, and the phase shifters re-adjusted.
The control of the switches S.sub.i and the phase shifters to
obtain a beam sweep of 360.degree. is well known and will not be
described in further detail herein. In practice the switches
S.sub.i are normally controlled by a computer.
Arrangements as described above provide a sum radiation
pattern.
The present invention seeks to provide improved space scanning
aerial systems and associated feeder arrangements therefor of the
kind referred to in which sum and difference radiation patterns may
be obtained.
According to this invention, an aerial and associated feeder system
adapted to provide electronic scanning of space comprises an aerial
system consisting of a plurality of aerial elements spaced along a
circular arc, said elements being divided into sets and units each
set consisting of the same plurality of adjacent equally spaced
elements and each unit consisting of a plurality of different
corresponding aerial elements, at least one in each set; and a
power dividing feed system divided into unit feeder arrangements
each leading to the aerial elements of two different units through
switch means whereby different pre-determined combinations of
aerial elements may be selected for connection to the unit feeder
arrangement therefor to determine the general direction of
radiation, there also being provided, in the path to at least one
of the two units fed by each unit feeder arrangement, adjustable
phase shifter means for adjusting said general direction of
radiation and wherein each unit feeder arrangement includes a four
port -3db coupler, the first of the two ports remote from the
aerial units of each of the said couplers being connected to a
first binary branching arrangement and the second of the two ports
remote from the aerial units of each of said couplers being
connected via adjustable phase shifter means to a second binary
branching arrangement whereby in operation sum radiation pattern
signals are obtainable by said first binary branching arrangement
and difference radiation pattern signals are obtainable by said
second binary branching arrangement.
The aerial and associated feeder system described above is suitable
for transmission, in which case signals applied to the single path
of the first binary branching arrangement are transmitted in
accordance with a sum radiation pattern whilst signals applied to
the single path of the second binary branching arrangement are
transmitted in accordance with a difference radiation pattern. The
aerial and associated feeder system described above is equally
suitable for reception, in which case sum radiation pattern signals
appear on the single path of the first binary branching arrangement
and difference radiation pattern signals appear on the single path
of the second binary branching arrangement.
Preferably each of the adjustable phase shifter means leading to
said second binary branching arrangement is a two-bit phase shifter
adapted to provide a phase delay of either zero or 2.pi.
radians.
Normally said phase shifter means provide zero phase delay when
corresponding elements in the units are selected and a phase delay
of 2.pi. radians when elements which do not correspond in the units
are selected.
Preferably again corresponding elements in adjacent sets are spaced
arcuately by 120.degree..
Preferably again, each unit feeder arrangement includes between
said -3db coupler and the two units fed thereby, and prior to said
phase shifter means are provided to adjust said general direction
of radiation, a hybrid unit whereby equal power is fed to each of
the two units. Preferably the last mentioned hybrid unit is a
further -3db coupler.
The invention is illustrated in and further described with
reference to FIGS. 3 and 4 of the accompanying drawings which
illustrate one example, in this case a modification of the system
illustrated in FIGS. 1 and 2, of a space scanning aerial system and
associated feeder arrangement therefor in accordance with the
present invention.
Referring to FIG. 3, the arrangement of the aerial elements a.sub.1
to a(n/6), b.sub.1 to b(n/6) and c.sub.1 to c(n/6) in sets and
units, the switches S.sub.i, phase shifters .phi..sub.i and
.phi.'.sub.i and -3db couplers C.sub.i is similar to that shown in
FIG. 1 and like references are used for like parts.
Again the feeding arrangements for the elements shown in FIG. 3
show, on the left as viewed, the arrangement for feeding in pairs
any one of elements a.sub.1, b.sub.1 and c.sub.1 with any one of
elements a(n/6), b(n/6) and c(n/6), whilst to the right of the
figure as viewed is shown the general case of feeding in pairs any
one of the elements a.sub.i, b.sub.i and c.sub.i ; with any one of
elements a(i + (n/6)), b(i + (n/6)) and c(i + (n/6)).
In place of the binary divider B, having (n/3) outputs of FIG. 1,
two binary dividers B1 and B2 are provided, each having (n/6)
output paths. One output path of the binary divider B1 and one
output path of the binary divider B2 are connected in pairs to the
two input ports of a different further -3db coupler D.sub.i of
which there are (n/6). Between each output path of the binary
divider B2 and the input port of the respective coupler D.sub.i is
provided a two-bit phase shifter P.sub.i. Again, of course, there
will be (n/6) two-bit phase shifters P.sub.i. The two output paths
of each further coupler D.sub.i are connected, as the pairs of
output paths of binary divider B in FIG. 1 are connected, to the
input ports of respective ones of the couplers C.sub.i, one of the
two output paths in each case being connected directly and the
other via a respective one of the phase shifters .phi.'.sub.i.
Each two-bit phase shift P.sub.i is such as to produce a phase
change of either zero or .pi. radians.
With the arrangement described above with reference to FIG. 3, each
of the further -3db couplers D.sub.i provide (assuming reception)
the sum Z.sub.i of the signals received through switches S.sub.i
and S(i + (n/6)) at the port connected to binary divider B1 and the
difference W.sub.i at the port connected to binary divider B2. For
a given beam direction, i.e. for given settings of the switches and
phase shifters, the sum signals Z.sub.i will all be in-phase and
add in the binary divider B1 to provide a sum signal Z. The
difference signals W.sub.i whilst in phase with each other, will be
either in phase or in anti-phase with the sum signals in dependence
upon the settings of the switches S.sub.i.
To appreciate this more clearly, assume that a target is in the
direction of the a(n/6) radial. The switches S.sub.i and phase
shifters .phi..sub.i, .phi.(i + (n/6)) and .phi.'.sub.i are set up
to produce a sum pattern with the main beam directed at the target.
If a signal is now transmitted at the target, a reflection from the
target arrives at the aerial to produce a signal in each of the
a.sub.i elements. These signals pass the switches and phase
shifters and are incident at the couplers C.sub.i as in-phase
signals. These may be represented by P.sub.i and P(i + (n/6)).
Analysis shows that
Z.sub.i .alpha.l.sub.i cos 1/2 .phi.'.sub.i + 1(i + (n/6)) sin 1/2
.phi.'.sub.i
and
W.sub.i .alpha.l.sub.i sin 1/2 .phi.'.sub.i - 1(i + (n/6)) cos 1/2
.phi.'.sub.i.
Thus the amplitude factors cos 1/2 .phi.'.sub.i and sin 1/2
.phi.'.sub.i may be seen to be interchanged when the difference
signal W.sub.i is produced as compared to when the sum signal
Z.sub.i is produced.
The effect on the primary illumination is illustrated in FIG. 4. In
order to produce the difference pattern efficiently, the phases of
excitation in the two halves of the aperture should be in
opposition. This condition is met with the initial aerial settings
above described, provided only small beam movements are required.
Consequently, for this initial setting, all of the phase shifters
P.sub.i are set to give zero phase shift. Consider now a beam shift
to the a((n/6)+ 1) radial. The switch S.sub.i moves to element
b.sub.1 and the a(n/6) element moves to the left hand side of the
aperture. The difference signal W.sub.1 is no longer the signal
received from a left hand element minus that received from a right
hand element, but is reversed.
In order to make difference component W.sub.i add correctly to the
other difference components W.sub.i, phase shifter P.sub.1 is
adjusted to provide a radian phase shift of difference component
W.sub.1.
In general terms, if S.sub.i and S(i + (n/6)) are switched to the
same element type (a, b or c) then phase shifter P.sub.i is set to
give zero phase change. In other cases the phase shifter P.sub.i is
set to give a .pi. radian phase shift.
* * * * *