BACKGROUND OF THE INVENTION
[0001] This invention relates to a radar scanning antenna apparatus which employs a phased
array of directional radiating elements aligned in a segment of a curved line such
as a cylinder and preferably a circular cylinder. The antenna system employs means
for exciting the elements in selected directions over a 360° scan.
[0002] In the prior art it is well known that a single face phased array can scan most of
the hemisphere with plus or minus 45° of azimuthal coverage being typical. Four faces
can then be used to provide 360° of azimuth coverage. Circular or cylindrical arrays
can provide 360° of azimuth coverage with relatively uniform characteristics of beam
width and gain with azimuth scan angle. The problem with both these approaches is
the excessive number of elements and physical size necessary to realize required performance.
[0003] Further in the prior art, U.S. Patent 4,491,845, Rothenberg, discloses a wide angle
phased array dome lens antenna with a reflection transmission switch. An antenna feed
harness is located at the zenith of a dome antenna such that it radiates into a phased
array antenna situated at the opening of the dome. Each radiating element of the phased
array has both an electronic phase shifter and a reflection/transmission switch. For
wide angle scanning the switches are set for the reflection mode, causing the phased
array to radiate into the dome with the antenna beam propagating through the dome
at wide angles. With the switch set for the transmission mode the phased array operates
as a conventional lens array operating in the transmission mode for plus and minus
60° coverage or in the reflection mode with the dome lens to provide as much as plus
or minus 120° of coverage in the opposite field of view. Rothenberg functionally provides
a similar result to applicants concept with a more complex mechanism.
[0004] U.S. Patent 4,489,325, Bauck et al., discloses an electronically scanned antenna
system. An N element excitation array 16 is coupled to a L element radiation array
10 by means of a parallel plate lens 15. The radia tion array is a linear array while
the excitation array lies on a curve which is locally approximately circular but with
decreasing radius at the outer edges. A M element subset 18 of the excitation array
is coupled with transmit received apparatus through a switching matrix digitally controlled
amplitude settings and phase shifters in the power distribution network. A lookout
table receives an indication of the desired scan angle and provides input to the switching
matrix in amplitude/phase shifters to select the proper subset of the excitation array
and the optimum complex way for each element. This is fundamentally a linear array
which only scans 80°, that is plus or minus 40°, and is not really relevant to wide
angle scanning.
[0005] U.S. Patent 4,085,404, Gallant, describes a method of smoothly commutating or moving
a beam in space using a lens and a plurality of probes. It does not address very wide
angle scanning.
[0006] Patent 4,580,140, Cheston, discloses a twin aperture phased array lens antenna. If
it is desired to scan 360° in azimuth two lens antennas 11 and 29 are positioned back
to back. This approach uses complex routing of the signal.
[0007] U.S. Patent 4,044,360, Wolfson et al., discloses a two mode rf phase shifter, particularly
for a phase scanner array, of a type which may be employed in the subject invention
and is assigned to the assignee of the present invention.
SUMMARY OF THE INVENTION
[0008] Accordingly it is one object of this invention to provide a radar scanning antenna
employing a phased array of directional radiating elements aligned in a segment of
a curved line and employing means for exciting the elements in selected directions
over a 360° scan.
[0009] Another object of the invention is to provide such an antenna array in which the
curved line is a cylinder and preferrably a circular cylinder.
[0010] Still another object of the invention is to provide a radar apparatus for scanning
360° employing an array formed of a segment of a cylinder having bidirectional radiators
selectively excitable in selected directions over a 360° scan.
[0011] These and other objects are achieved by providing a radar scanning antenna employing
a phased array of directional radiation elements which are aligned in a segment of
a curved line, or surface of a circular cylinder, and employ a feed subarray for exciting
the elements in selected directions over a 360° scan.
[0012] The novel features which are believed to be characteristic of the invention are
set forth with particularity in the appended claims. The invention and further objects
and advantages thereof can best be understood by reference to the following description
and accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
[0013]
FIG. 1 is a schematic diagram of the invention showing a beam scan of 0°.
FIG. 2 is a schematic diagram illustrating a beam scan of 45°.
FIG. 3 is a schematic diagram showing a beam scan of 90°.
FIG. 4 is a schematic diagram of the invention showing a beam scan of 180°.
FIG. 5 is a schematic diagram of the invention showing a beam scan of 135°.
FIG. 6 is a schematic diagram of the invention showing a beam scan of 120°.
FIG. 7 is a schematic diagram of an element which can be used to transmit in either
the exterior or interior direction employed in the invention.
FIG. 8 is a schematic diagram of an alternate element employing an elemental phase
shifter which could be used to transmit in either the exterior or interior direction.
FIG. 9 illustrates still another alternate approach for providing a bidirectionally
transmitting element.
FIG. 10 is a schematic diagram of a multiple feed arrangement for feeding a half cylinder
such as used in the subject invention showing one of the feeds in blown up form.
FIG. 11 A & B are schematic diagrams illustrating how the F/D ratio may be increased
by conventional sub reflector techniques.
FIG. 12 is a schematic diagram illustrating the different sectors covered by the
antenna of the subject invention.
FIG. 13 is a three dimensional diagram showing a transport configuration of the antenna
of the subject invention.
FIG. 14 is a schematic diagram showing the antenna array main aperature and a sub
array feed with one radiating element shown in blown up form.
DESCRIPTION OF THE PREFERRED EMBODIMENT
[0014] Turning now to the drawings, there is illustrated a preferred embodiment which describes
a half circular array which can be used to provide 360° of azimuthal coverage. When
the array is extended in the vertical plane a half cylinder array is formed with 360°
of azimuthal coverage and elevation scan coverage limited in angle by existing well
known design constraints. The technique to be discussed is also applicable to truncated
half cones and segments of a sphere. FIG.'s 1-6 show how a half cylinder array can
be ultilized to provide 360° of azimuth coverage. To achieve this the illumination
is first moved around the exterior of the cylinder. This provides slightly over a
hundred and eighty degrees of coverage. Then the illumination is moved around the
interior of the cylinder to provide the remainder of the coverage to complete the
360°. Note that in Fig. 3, for example, there is a smaller active aperature on the
exterior. The half cylinder concept requires an element which can transmit in either
the exterior or interior direction. Turning to FIG. 7 this can be accomplished with
an active element array module 20 comprising a power amplifier, a receiver ampli
fier, a phase and other well known devices plus means 22 and 24 for switching the
interior/exterior ports 26 and 28 respectively.
[0015] An alternate approach illustrated in FIG. 8 would use an elemental phase shifter
such as that disclosed in U.S. patent 4,044,360 Wolfson. The diode switch 30 switched
back and forth between the bits below 180° 32 and those from 0° to 180°, 34 which
are transmitted from the interior element 36 and the exterior element 38 respectively
to provide a 360° reflection phaser. FIG. 9 shows an alternate dual state phaser in
which the interior element 40 transmits from the bits below 180° 42 and is controlled
in the following manner. When pin diode 44 is shorted and pin diode 46 is open there
is a phase state 0. When pin diode 44 is open and diode 46 shorted a phase state of
180° is achieved due to current reversal in coupling loop 48. When the pin diode
44 and 46 are in the same state, shorted or open, a reflection without added components
is achieved. This dual state phaser can be used in a half cylinder lens, angle scanning
being provided by the phase shifters.
[0016] The illumination could be moved about the cylinder by switching the input signal
between horn feed such as illustrated in figure 10, where horn 50 would achieve angles
about 0° degrees or 180° degrees, horn 52 angles about 45° or 180° plus 45° degrees,
horn 54 angles about 60° degrees or 180° plus 60° degrees, horn 56 angles about -45°
or -225° and horn 58 angles about -60° or -240°. Note that the cylinder 60 can be
slightly larger or smaller than 180°. More feeds can be used for smaller movement
of the aperture illumination over the phased array surface. Less feeds are used for
coarser aperture illumination control. Feed 50 is shown in blown up form to illustrate
multi-element feed for aperture distribution control as well as multiple clusters
of beams including use for adaptive nulling.
[0017] In some applications the required ratio of the distance of the feed from the aperture
to the radiating aperture width f/d may be larger than is physically practical due
to unique required design parameters. The ef fective f/d can be substantially increased
by using the well known principle of reflection as shown in FIG. 11A and 11B. Here
the feed elements are located near the radiating arc. They direct energy toward a
subreflector 62 shown at the left of FIG. 11B. The energy is reflected from the flat
subreflector 62 to the cylindrical array 64. The apparent or effective feed location
is shown in FIG. 11A on the left arc 66. The focal length 68 shown is approximately
equal to the diameter of the cylinder but the feed elements 70 occupy a much smaller
physical space within the half cylinder.
[0018] The antenna array of the subject invention is characterized by a semi cylinder array
which is space fed and operates in both transfer and reflective modes. This provides
full performance in the 120° forward sector as illustrated in FIG. 12 as well as rearward
coverage with some reduction in performance in a 90° secondary sector. In addition
the aperture affords additional peripheral coverage in side sectors labeled peripheral
sector in FIG. 12, where operational demands can be greatly reduced but where continuous
search coverage is desirable. The peripheral coverage as shown in FIG. 12 can be
good enough for search in these sectors of lesser hostility and can provide continuity
of radar burst communications capability as well in these otherwise unavailable regions.
[0019] Monopulse can be implemented in fore and aft sectors, but assymetries are likely
to occur in the regions of peripheral coverage. A space feed is shown to efficiently
generate a single beam or formed clusters of beams including adaptive nulling in the
primary sector of coverage.
[0020] A partial disadvantage of the subject invention is that full performance can not
be provided over the full 360° of azimuth. However it seems less of an issue since
generally the peripheral regions of coverage where operational demands are the lowest
are the regions of coverage where jamming influence is the least and where performance
increases beyond the immediate requirement. Accordingly if the peripheral regions
can be covered with greater haste and lesser accuracy the more threatened regions
of cover age can achieve proportionally more attention while still adequately covering
the rest. A typical transportable arrangement for an antenna such as employed in the
subject invention is illustrated in FIG. 13 which shows the antenna 72 stowed for
transport on the top of a conventional S-280 shelter 74. Cut out rail 76 on the side
of the shelter allows a lower profile in transport. When erected as shown in the dashed
line 78 the antenna can be trained plus or minus 60° for optimization of threat coverage
without moving the equipment.
[0021] Turning now to FIG. 14 there is illustrated an antenna configuration in accordance
with the subject invention having a space fed shaped array. This configuration has
a space fed main aperture 80 which uses a forward/reverse phased and curved surface
employing elements 82 illustrated in blown up section 84 and employing a phase shifter
86 a wave guide 88 and two radiators 90 and 92. This configuration is similar to that
shown in the referenced patent to Wolfson 4,044,360. The subarray 94, used to space
feed the main aperture, is a curved azimuth scannable array. The secotr beams generated
by the subarray are scanned to different sections of the main aperture depending on
the azimuth angular sector which is being scanned in the far field. Forward coverage
is designed to generate the optimum performance, and, for example, close to one
hundred percent of the main aperture will be used. The scan range can be plus or minus
45° in the azimuth far field. The phase shifters in the main aperture determine the
main aperature scan. Specific sectors of the main aperture can be illuminated and
used in the processing of the main aperature illumination.
[0022] Some of the major performance atrributes of the curved space fed array are its limited
360° azimuth performance, its sectored feed capability and its scanned monopulse
beams in azimuth and elevation planes. Forward coverage is optimum for the array while
reverse coverage will be slightly degraded by aperture blockage and side coverage
will be degraded by a limited aperture size in the azimuth plane. However, the limited
coverage will make available several but not all of the important radar functions.
The sectored feed introduces considerable flexibility into the synthesis of the main
aperture illumination. Several sectors of the main aperture may be illuminated in
order to optimize coverage in the side area of the far field. The monopulse capability
in azimuth and elevation has low sidelobe prformance particularly in the forward direction.
[0023] Phase shifters in the present invention present an impact on system costs due to
the relatively large numbers required. Low cost low loss phase shifters are required
and may be of the diode type, ferrite type, or active element type. Diode phase shifters
for instance have the advantage of low cost. Ferrite phase shifters involve lower
losses and faster switching speeds.