Radiating Elements for Shared Aperture
Tx/Rx Phased Arrays at K/Ka Band
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Article
Authors
Sandhu, Ali Imran; Arnieri, E.; Amendola, Giandomenico; Boccia,
L.; Meniconi, Erika; Ziegler, Volker
Citation
Radiating Elements for Shared Aperture Tx/Rx Phased Arrays
at K/Ka Band 2016:1 IEEE Transactions on Antennas and
Propagation
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DOI
10.1109/TAP.2016.2552550
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Institute of Electrical and Electronics Engineers (IEEE)
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IEEE Transactions on Antennas and Propagation
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1
Radiating Elements for Shared Aperture
Tx/Rx Phased Arrays at K/Ka Band
A.I Sandhu, E. Arnieri, Member, IEEE, G. Amendola, Senior Member, IEEE,
L. Boccia, Member, IEEE, E. Meniconi and V. Ziegler Senior Member, IEEE
Abstract— A dual band, Tx/Rx, self-diplexing phased array is
presented. The antenna has been designed to cover Tx/Rx satellite
communications at K/Ka band with a frequency ratio 1.5:1. To
obtain dual band operations with a single radiating surface, a
novel dual band radiator is adopted and placed in a configuration
in which dual band and single band elements are interleaved. The
proposed configuration reduces the number of radiating elements
required by other solutions while avoiding the insurgence of
grating lobes. The tightly packed arrangement of the elements
poses many integration issues, which are solved with a novel
integration technique. The array elements are optimized to scan
the beam in excess of
° in both bands. A subarray with 49 Rx
elements and 105 Tx elements was built and measured confirming
the results obtained in simulations.
Index Terms—Microstrip antennas, multi-frequency antennas,
phased arrays, planar arrays
I. INTRODUCTION
M
ODERN communication systems
require highly integrated
user terminals operating in the millimeter wave region
embedding antennas with beam steering capability. Examples
include K/Ka band SatCom on-the-move (SOTM) terminals [1]
and 60 GHz high-capacity communications in complex indoor
scenarios [2], [3]. It is also foreseen that 5G technology for next
generation wireless communication networks will rely on
sophisticated beam-forming capabilities in which hand held
terminals and base-stations communicate through optimum
line-of-sight/ Non-line-of-sight (LOS/NLOS) millimeter wave
links [4]. In all these applications, radiation boards,
interconnects, beam forming networks, Tx and Rx modules and
other circuitry have to be included in a reduced volume
increasing the complexity of the integration process. A
significant milestone in this direction has been achieved with
the recent introduction of multifunctional chipsets capable to
contain many reconfigurable transmit (Tx) and Receive (Rx)
chains. However, there are still functionalities that are
intrinsically space consuming. At the antenna level one of the
main issues is that Rx and Tx operations are usually obtained
with two separate radiating apertures thus considerably
increasing the actual space occupied by the system. The design
of arrays able to integrate both Tx and Rx operation in a single
aperture is cumbersome, albeit essential. Two solutions may be
devised: arrays of elements with a bandwidth large enough to
cover both Tx and Rx or arrays of dual band elements. The first
Manuscript received November 15, 2015. This work was supported by EU
commission under the FP7 project FLEXWIN. E. Arnieri, G. Amendola and L.
Boccia are with the University of Calabria, Rende (Italy), (e-mail:
solution has been largely explored [5], [6]. For example, arrays
of tightly coupled dipoles with ultra-wide band performance
have been recently studied [7] for Ku-band SOTM applications
showing excellent scanning behavior in a wide angular range.
Nevertheless, this approach suffers from three inherent
drawbacks. Firstly, the tightly coupled dipoles configuration
corresponds to a very small cell size (less than 0.3 wavelength
at the highest frequency) which makes the integration of the TR
modules difficult. Secondly, the reduced cell size results in an
increased number of elements and, consequently, of control
signals thus making significantly more critical the manifold
design. Thirdly, as the array is not self-duplexing some
mechanisms to discriminate between the two bands would be
required.
Other dual band phased-arrays have been proposed in literature
mainly for Synthetic Aperture Radar instruments operating at
multiple bands [8], [9]. Small multiband arrays have been also
designed for mobile telecommunications base-stations [10].
Wide-angle scanning was recently taken into account in [11],
[12] designing dual-band radiating elements for X/Ku phased
arrays with beam steering capability down to 60/50 degrees.
In this paper, a new concept of compact dual-band phased array
supporting wide-angle beam steering is presented. The
a Rx
bTx
y
aTx
x
Tx Antenna
Dual Band (Tx,Rx) Antenna
Fig. 1. Dual-band array lattice with interleaved Tx and Rx elements.
luigi.boccia@unical.it). A. I. Sandhu is now with KAUST, Jeddah (Saudi
Arabia). E. Meniconi is now with Qorvo, Inc., Munich (Germany) and V.
Ziegler is with Airbus Group Innovations, Munich (Germany).
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TABLE I
NUMBER OF ELEMENTS OF A DUAL-BAND ARRAY
FOR DIFFERENT LATTICE CONFIGURATIONS
Number of array
Array Configuration
elements
N λ Rx
0.5 λTx
N λ Rx
N λTx
N λTx
0.5 λ Rx
=4
=4
Two single-band arrays with square cells
N λ Rx
0.575 λ Tx
0.575 λ Rx
N λ Rx
N λTx
N λTx
≈ 3.5
≈ 3.5
Two single-band arrays with hexagonal cells
N λ Rx
N λ Tx
N λ Rx
0.33 λ Rx =0.5 λTx
≈9
2
radiating elements and to the ratio between the Tx and Rx center
frequencies (1.5:1), the design of the radiating elements is
particularly challenging for the following inherent reasons.
Firstly, the array lattice and the cell size have to be selected to
avoid grating lobes in the whole scanning region. Secondly,
although the frequency ratio between the Tx and Rx bands
could be covered with wide-band radiators they would not be
self-duplexing thus making the chip integration significantly
more complex [15]. On the other hand, the frequency ratio is
not wide enough to facilitate the design of dual band elements.
To solve the two problems, a novel radiating element based on
coaxial printed rings is introduced in this paper. As it will be
shown, the new element can be made compact enough to be
embedded in arrays with small cell sizes, it can be optimized to
achieve wide scan angle and it can be easily integrated with
multi-core MMICs. Although the specific context of this work
is related to K/Ka-band SOTM user terminals, its scope can be
extended to other dual-band phased arrays with large frequency
ratio and wide scanning.
The paper is organized as follows. The concept of
superimposed array and the lattice definitions are described in
Section II. The dual- and single-band elements are presented in
Section III. Simulated and measured results are shown in
Section IV and V demonstrating very good performance in
terms of scanning impedance in both the E- and H-plane.
=4
II. DUAL BAND ARRAY LATTICE
Shared aperture array with square unit cells.
0.575 λ Tx
N λ Tx
N λ Rx
N λ Rx
≈7
≈ 3.5
N λ Tx
Shared aperture array with hexagonal cells
0.575 at 30 GHz
Shared
aperture
array
configuration in Fig. 1)
(interleaved
≈4
≈ 3.57
The definition of the array lattice influences the design of a
dual-band phased array in several ways. The most direct impact
is on the radiation performance. Indeed, the proper elements’
location on the radiating surface is the main means to avoid
grating lobes arising within the entire scanning range and in
both bands. Moreover, from the array lattice depends also the
number of elements present in a given radiating aperture and,
in turn, the number of Rx and Tx RF chains required to
implement the electronic beam control. Finally, the
inter-element spacing is also crucial to allow the integration of
the active chips and to enable a feasible radiating element
design.
Different strategies can be adopted to identify the best
topology for the dual-band phased-array. For the case at hand,
a comparative evaluation of different lattices was performed as
proposed configuration mainly targets applications with large
frequency ratios, wide scanning range and full electronic
control. The array illustrated in this work has been conceived
taking as a reference case K/Ka-band SOTM applications (Rx
20.2-21.2 GHz, Tx: 29.5-30.8 GHz) with a scan angle of ±60°.
The proposed array has been designed to be integrated with
multicore, SiGe BiCMOS 3.8x3.8mm^2 chips containing two
Rx and four Tx chains designed in the framework of the EU
FP7 project FLEXWIN [13], [14].
For the application at hand, due to the tight arrangement of the
v
The number of array elements (in the Tx and Rx band) is calculated for
an aperture equal to Nλ where N is an integer number and λ is the
free-space wavelength on each band.
3
3
2
2
1
1
0
0
v
N λ Tx
-1
-1
-2
-2
-3
-2
0
u
2
-3
-2
0
u
2
(a)
(b)
Fig. 2. Grating lobes diagrams for the 20 GHz array on a rectangular
lattice (a) and for the 30 GHz array on a triangular lattice (b). Scan angle
is = 60° in both cases. Shaded region included in black dots is the
visible space.
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summarized in Table I. The radiating aperture was defined for
and
each band in terms of the wavelength as
where N is an integer number and where
and
are the Rx and Tx wavelengths respectively. The first example
taken into account is a based on two single aperture uniform
arrays, namely a square and a hexagonal lattice, designed to
meet the grating lobes’ constrain. A square array with a 0.5 ×
elements for each aperture
0.5 unit cell would require 4
whereas a hexagonal arrangement with a radius of 0.575
would limit the number of elements to about 3.5 . For a
shared aperture Tx/Rx phased array, the simplest configuration
is to design dual-band elements small enough to be placed in a
cell fulfilling the grating lobes’ constrains at the highest
frequency. As an example, dual-band radiating elements could
be placed in a square lattice with a cell size of half a wavelength
at 30 !" which will correspond to a cell of a third of a
wavelength at 20 !", as it is shown in the third case presented
in Table I. Although this solution fulfills the grating lobes’
requirements, it would increase the number of required
elements leaving limited space for the integration of the chips.
On the other hand, a hexagonal lattice would reduce the number
of required elements by 13% at both frequencies. As an
alternative solution, the hybrid lattice shown in Fig. 1 is here
proposed to limit the overall number of array elements and to
keep the cell size at 20 GHz and at 30 GHz independent one
from the other. The proposed solution is based on two arrays of
Rx and of Tx elements superimposed. The Rx elements are
placed on a square lattice with a cell size equal to $ aligned
to the x-y axis. The Tx elements are placed on an isosceles
triangular lattice having base $ and height % . The unit cell
of the dual band lattice is constituted by the set of three radiators
highlighted in the lower part of Fig. 1, namely one dual-band
and two Tx antennas.
It is worth noticing that the proposed arrangement can be
adapted to different dual-band arrays but it requires single band
Tx interleaved with dual-band unit-cells. For the case at hand
and for any other application having a frequency ratio of 1.5:1,
=
the optimal configuration would lead to $ = 0.5
0.75
=$ .
Both configurations fulfil the conditions on grating lobes
derived as in [16]
$
$
<
<
√2
1 + sin
'
1 + sin
/'
-
,
(1)
-
%
1
=$
1 /2
(2)
where - and - is the main beam elevation for the Rx
and Tx array respectively. The second condition can be easily
derived from the first one considering the triangular lattice as a
square one rotated of 45° and with a spacing of 0.53 .
Considering a scan angle of 60° at both bands (i.e. - =
= 60°) it can be verified that grating lobes do not arise
when $ < 0.539
and $ < 0.7579 . As a further
3
Microstrip line
Slot
Microstrip line
Slot
y
x
(b)
(a)
Via
TX Microstrip line
Slot
Via
Tx Slot
Microstrip line
Rx Slot
Rx Microstrip line
(d)
(c)
Fig. 3. Basic concept of the elementary cells required to
implement the lattice of Fig. 1: a) single band Rx antenna; b)
single band Tx antenna; c) dual Band Tx/Rx antenna; d) antenna
stackup.
validation of the proposed configuration, grating lobe diagrams
for both frequencies are shown in Fig. 2. As it can be observed,
grating lobes are outside the visible region for scan angles <
60° and for any azimuth angle.
III. RADIATING ELEMENTS
In this section are described the dual-band (Tx/Rx) and the
single-band Tx radiating elements required to implement the
previously introduced dual-band array lattice. In the first part,
the basic concept of the array cells and their radiation
characteristics is introduced while in the second part the design
is actualized for the application at hand in an infinite-array
context.
A. Radiating element concept
The design of the array elements required for the
implementation of the lattice described in Fig. 1 is based on two
single-band radiating elements as shown in Fig. 3. Both the Rx
(Fig. 3-a) and the Tx (Fig. 3-b) single band radiators are made
by an annular aperture surrounded by a cylindrical cage of
metalized via holes forming a radiating cavity. These
conducting walls help to minimize the impact of mutual
coupling effects thus limiting the insurgence of side lobes. The
antenna operating in the lower band (Rx) has an additional
shorted inner boundary implemented through a coaxial ring of
via holes. The inner pad of the Tx radiator is instead not
grounded and it is used for fine frequency tuning and to better
matching. Each ring apertures are electromagnetically coupled
to a microstrip by means of a rectangular slot.
The two single band structures can be combined as shown in
Fig. 3-c by accommodating the radiator of Fig. 3-b inside the
one of Fig. 3-a in such a way that the inner wall of metallized
vias is shared between the two elements. As already shown by
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Layer
name
D1
G1
Stack-up structure
Thickness
Material
0,250mm
0,033mm
FastriseDS
Copper
D2
1,5mm
Multiclad HF
G2
0,033mm
Copper
D3
0,200mm
Multiclad HF
0,018mm
Copper
4
Via
Microstrip
ML
Fig. 6. Cross sectional view of the single band and dual band element.
outside the radiator. Moreover, as it will be shown in the
following paragraphs, the inner coaxial via cage allows the
radiators in the two bands to be designed almost independently
thus significantly simplifying the overall design process.
Fig. 4. 3D view of the of the Tx single-band element: R1=1.65mm,
R2=0.7mm,W1=1.4mm, H1=1.05mm,
B. Radiation characteristics
The radiation properties of the antennas presented in the
previous-subsection were evaluated by taking into account a
simplified model of PCB multilayer circuit as shown in
Fig. 4-6. Two types of radiating cells were taken into account,
namely the single band (Tx) and the dual-band (Tx/Rx) cell.
Antennas were fed through a dog-bone slot cut in the ground
0 dB
30
330
-10
-20
300
60
-30
270
90 deg
G , φ=0 deg
240
120
x
G , φ=90 deg
x
G , φ=0 deg
y
Gy, φ=90 deg
210
150
180
Fig. 5. 3D view of the dual band, Tx-Rx dual-band element: R3=3.5mm,
R4=1.84mm, W2=2.8mm, W3=1.6mm, H2=1.4mm, H3=0.95mm.
Fig. 7. Single-band Tx antenna, simulated co-polar and cross-polar
radiation patterns in the two main plane cuts.
0 dB
the authors in [17], the dual-band antenna can be thus
designed by optimizing the geometry so as the external and
the internal antenna operate in the Rx and Tx band
respectively. In the Rx case, due to the coaxial geometry, the
antenna may propagate TEM, non-radiating, modes.
However, if properly designed, a radiating TM mode can be
excited [18].
The proposed configuration has several unique features
which are explained as follows. Dual-band (Tx and Rx)
antennas and single-band Tx cells can be implemented as in
Fig. 1 using the same 3-layer stack-up. The radiation
properties of the Tx single-band radiator are similar to the
ones in the dual-band configuration thus perfectly fitting the
requirements of the array lattice proposed in Section II.
Furthermore, the presence of the outer via cage is crucial in
avoiding leakage and excitation of parallel plate mode
30
330
-10
-20
300
60
-30
270
90 deg
240
Gx , φ=0 deg
120
Gx , φ=90 deg
Gy , φ=0 deg
210
Gy , φ=90 deg
150
180
Fig. 8 Dual-band antenna in Rx mode, simulated co-polar and cross-polar
radiation patterns in the two main plane cuts.
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plane and coupled to a microstrip line printed in the lower part
of the stack-up. Each antenna is thus linearly polarized being
the Tx and Rx polarization orthogonal to each other. Dual
polarization or circular polarization, thought already
demonstrated in [18], [19] for similar antenna configurations,
was not taken into account for this work. Interestingly, the
dual-band cell is fed through two independent microstrip lines
thus resulting in a self-duplexing behavior which is highly
effective in the design of the array beam forming network [15].
The material chosen for the design is a Rogers Multiclad HF
with 34 = 3.45 and 5$67 0.009. The overall thickness is
1.5mm. A dielectric cover of Fastrise DS 0.250mm thick is
placed on the radiating surface. Notice that some of the vias are
indented into the slot to reduce the cell size. The configurations
shown in Fig. 4 and 5 were analyzed as isolated cells using a
commercial finite element simulator [20]. The size of the
single-band and dual-band cells are taken with $ 1 $ 1
7.588. The simulated [20] radiation patterns for the two
antenna types are shown in Fig. 7-9. The single-band Tx
antenna presents (Fig. 7) a broad beam with a peak gain of
4.83 dBi and cross-polarization isolation greater than 30 dB in
the broadside direction. It is important to note that the Tx
radiation properties remain almost unchanged from the
single-band to the dual-band design though the latter
configuration presents a slight degradation of the polarization
properties. The Rx radiator in the dual-band cell has a gain of
4.6 dBi and cross-polar radiation greater than 30 dB in the
whole upper hemisphere. As it can be observed in Fig. 10-11,
within the Rx and Tx bands the gain variation of both antennas
is less than 0.5 dBi. In the same figures, are also reported the
reflection coefficients and, for the dual-band configuration, the
coupling between the Tx and Rx radiators. The geometry of
both antennas was optimized to obtain good impedance match
to 50 Ohm in the whole bands without requiring additional
matching networks. As noticed in the previous section, the two
antennas are highly isolated especially in the lower band
because at this frequency the inner radiator is in cut-off.
5
0 dB
330
30
-10
-20
300
60
-30
90 deg
270
240
120
Gx, φ=0 deg
Gx, φ=90 deg
Gy, φ=0 deg
210
Gy, φ=90 deg
150
180
Fig. 9. Dual-band antenna in Tx mode, simulated co-polar and cross-polar
radiation patterns in the two main plane cuts.
Fig. 2. Exploded 3D view of the Single-Band Cell (SBC) integrated with
a simple beam forming network: R3=3.2mm; H6=0.85mm; H7=1.5mm;
H8=2.1mm; W8=1.6mm; W9=3.5mm; W10=3.1mm;
Fig. 10. Simulated single-band Tx antenna: reflection coefficient and
gain.
IV. ARRAY DESIGN
The radiating elements were designed in view of their
integration in a dual-band beam steering array implemented
through the chips introduced in [13]–[15]. As discussed in [21],
the proper implementation of this type of architecture requires
adopting a complex multilayer stack-up comprising different
types of vertical transitions. In particular, the reduced grid size
leaves limited routing space to implement the Distribution
Network (DN) and to integrate the multicore chips. For this
reason, in this work the DN was split into two parts: a microstrip
at the base of the stack-up and a stripline in the intermediate
layer SL. A complete stackup used for the design of the array is
shown in Fig. 12. The nth ground metal layer is indicated with
the symbol Gn, while the nth dielectric layer with Dn. Each cell
is fed through a stripline which is connected to a vertical
transition (Via 3 in Fig. 12) to give access to the microstrip ML
and to the active devices (MMIC).
Fig. 11. Simulated dual-band antenna gain, reflection and transmission
coefficient: a) Rx port; b) Tx port.
A. Stack-up configuration
In Fig. 13- 14 the cross sectional view is reported along with an
exploded view of the Dual-Band Cell (DBC) and of the
Single-Band Cell (SBC) integrated with a simple DN.
(a)
(b)
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Dimensions given in the caption are relevant to a radiating
element optimized in an infinite array configuration. As it can
be noticed, the structure is divided, and fabricated, in two parts:
a radiation board (layers D1, G1, D2, G2) and a DN manifold
(G3, D3, D4, G4, D5, G5 and D6). The possibility to have two
independent stackups allows the implementation of more
complex via configurations which will be essential in the design
of the final phased array prototype where additional layers have
to be included to allocate the digital bus, the control and the bias
lines (D5 in Fig. 13). Indeed, by using the conducting adhesive
layer the radiation board (RB) and the DN manifold (DNM) can
be fabricated with two separate processes making easier the
realization of complicated multilayer structure. The two parts
are glued together by means of an adhesive conducting foil
(Loctite AbelstickTM) placed between metal layers G2 and G3.
The glued ground planes (G2 and G3) have twin slots through
which the radiators are coupled to the feeding striplines. To
allow the twin slots to couple, rectangular non-resonant cavities
are realized in the conducting adhesive layer as shown in
Fig. 12 - 14. A detailed description of the stackup is shown in
Fig. 12 while Table II summarizes the proprieties of the three
types of via used in the demonstrator presented in this work.
A number of vias have been used between G1 and G2 (see Via
1 in Fig. 12 and Table II) to implement the coaxial structure
required for the dual-band and single band radiating elements
described in Section III-A. Blind vias between G3 and G4 (see
Via 2 in Fig. 12 and Table II) have been used to realize a cage
surrounding the striplines and the slots on G3 to avoid the
excitation of unwanted parallel plate modes and to reduce
coupling between the two slots. The lower part of Figs. 13-14
show the quasi coaxial vertical transition [22] used to connect
6
Fig. 13. Exploded 3D view of the Single-Band Cell (SBC) integrated with
a simple beam-forming network: R3=3.2mm; H6=0.85mm; H7=1.5mm;
H8=2.1mm; W8=1.6mm; W9=3.5mm; W10=3.1mm.
Via 1
Via 2
Via 3
Bondwire
Fig. 12. Description of the array multilayer stackup.
TABLE II
PROPRIETIES OF THE VIA HOLES SHOWN IN FIG. 13
Name
Via hole type
Diameter
[mm]
Via 1
Via 2
Via 3
Through via (RB)
Blind via (DNM)
Through via (DNM)
0.3
0.5
0.25
Fig. 14. Exploded 3D view of the dual-band array cells (DBC) integrated
with a simple beam-forming network: R1=3.5mm; R2=1.7mm;
H1=1.4mm; H2=0.65mm; H3=1.5mm; H4=1.8mm; H5=2.7mm; W1 =
2.8mm; W2=1.68mm; W3=2.2mm; W4=3.5mm; W5=0.27mm;
W6=4.5mm; W7=7.5mm
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7
a Rx
y
y'
y
x'
bTx
x
x
(a)
(a)
(b)
Fig. 15. Simplified infinite array set-up configurations for the analysis of
the Tx radiator. The unit cell is identified rotating the axes around the zaxis of 45 deg: a) unit cell definition; b) master/slave condition.
(b)
Fig. 16. Simplified infinite array set-up configuration for the analysis of
the Rx radiator. Two sets of master/slave conditions have been used as the
BFN stackup is shifted along the y axis with respect to the radiating boarda) unit cell definition; b) master/slave conditions.
the feeding striplines to the microstrips under D6 where active
devices can be placed. Vias between G3 and the layer
containing microstrips (Via 3 in Fig. 12 and Table II) have been
used to realize the quasi-coaxial transition. In particular, the
realization of these transitions requires two different types of
vias: grounding vias (from ML to G3) and a central signal via
(from ML to SL). In order to reduce the manufacturing
complexity, a single type of via (Via3 from ML to G3) has been
used for all vias. In a second manufacturing phase, a backdrilling process has been used to remove the unused section
(from G3 to SL) of the central signal via.
B. Active impedance analysis
The active impedance of the proposed radiating elements
shown in Figs. 13-14 was evaluated within the entire scanning
range by means of HFSS simulations in infinite array
configurations. It is worth noticing that, as shown in Fig. 1, the
smallest unit cell of the dual-band lattice is constituted by a
subarray of three radiators, namely one DBCs and two SBCs.
However, the evaluation of the active impedance at various
scan angles with this type of cell is not straightforward [23]. In
fact, the Floquet analysis applied to this elementary cell would
give results valid for the subarray but not for the single element.
In particular, in a master-slave linked boundary configuration,
like the one used in HFSS, the phases of each radiator in subarray cell can not be directly linked to the phase difference
between the vertical master and slave boundaries which are in
turn used to identify the scan angle. For this reason, two distinct
set-ups, shown in Fig. 15 and 16, were used to validate the array
performance.
Considering the lattice shown in Fig.1, the Rx radiator was
simulated in a DBC configuration with a cell size of $ 1
7.588 while the Tx radiator was analyzed in a cell
0.5 '
having a side of % 1 5.388 and rotated of 45° with respect
to the main axis. As it will be shown in the next section,
although this simulation set-up does not fully reflect the array
lattice shown in Fig. 1, it proved to be sufficiently accurate in
predicting the input impedance and the radiation characteristics
of all radiating elements.
Simulation results in two configurations are shown in Fig. 17
(a)-(d) where the input impedances are represented in the Smith
chart for scanning angles
0°, 20°, 40°, 50°, 60° in the two
main planes. As it can be observed, for the Rx element
configuration results are acceptable in both 9 and ! planes in
the whole scanning range. The Tx element has an excellent
matching on the 9 plane but presents severe mismatch on the
! plane at scan angles larger than 30 deg. To improve the Tx
cell performance, a wide-angle impedance matching layer
(WAIM) was introduced as suggested in [24] by adding a
dielectric layer of thickness 0.13mm and with 3: 6.15, (i.e.
Rogers RO3006) 0.94 mm above the radiating cells. As it can
be observed in Fig. 17 (e)-(h), the presence of the WAIM
improves the scanning capabilities of the array, in particular on
the H plane, for scan angles down to 60°.
To better appreciate the behavior of the array elements, in figure
18 (a)-(b) and figure 19 (a)-(b) are shown the active reflection
coefficients at the input port for the cases presented in Fig. 17
for the case with WAIM layer in place. Spikes due to unwanted
resonances [18] are present in the Rx band for scanning angle
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8
Rx - E plane - WAIM
Rx - E plane - WAIM
(a)
(e)
Rx - H plane - No WAIM
Rx - H plane - WAIM
(b)
(f)
Tx band - E plane - No WAIM
Tx band - E plane - WAIM
(c)
(g)
Tx band - H plane - No WAIM
Tx band - H plane - WAIM
(d)
(h)
θ=0 deg
θ=20 deg
θ=40 deg
θ=50 deg
θ=60 deg
Fig. 17. Smith Chart representation of the simulated active input impedance of the Rx and Tx elements embedded into an infinite array for different scan
angles (
0°, 20°, 40°, 50°, 60°) on the E- and H-planes. Plots in a, b, c, and d in the left column are obtained without WAIM; plots e, f, g and h in the right
column are obtained including a 0.13 mm thick WAIM layer placed at a distance of 0.94 mm from D1 and with 3: 6.15 ;<=>? @3006 . Square and
circular markers indicate start and stop frequencies edges respectively.
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0
0
-5
-5
-10
-10
-15
S11 (dB)
S11 (dB)
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θ=0 deg
θ=20 deg
θ=40 deg
θ=50 deg
θ=60 deg
-20
-25
θ=0 deg
θ=20 deg
θ=40 deg
θ=50 deg
θ=60 deg
-15
-20
-25
-30
-30
19
19.5
20
20.5
21
21.5
29
22
29.5
30
0
-5
-5
-10
-10
S11 (dB)
0
θ=0 deg
θ=20 deg
θ=40 deg
θ=50 deg
θ=60 deg
-20
-25
31
31.5
32
(a)
(a)
-15
30.5
Frequency (GHz)
Frequency (GHz)
S11 (dB)
9
θ=0 deg
θ=20 deg
θ=40 deg
θ=50 deg
θ=60 deg
-15
-20
-25
-30
-30
19
19.5
20
20.5
21
21.5
22
Frequency (GHz)
(b)
Fig. 18 Active S11 of the Rx elements scanning on the E plane (a) and on
the H plane (b).
+-60° in both E and H planes while, in the Tx band, the antenna
is unmatched when scanned to 60° even if no scan blindness
spikes are observed. No further optimization has been
attempted to improve scan properties at 60°.
V. EXPERIMENTAL VALIDATION
The experimental validation of the scanning performance of the
Rx and Tx antenna elements was carried out measuring their
active radiation patterns and evaluating the scanning range as
done in [11], [12]. The array prototype used to measure the
active patterns is shown in Fig. 20, where the radiators (layer
G1 in Fig. 14) are revealed without the dielectric cover. The
prototype is composed by a 7x7 square array of Rx/Tx elements
interleaved with an array of Tx elements. In total, the array is
populated by 49 Rx-Tx and 56 Tx cells. Only the central dualband array element is connectorized while the other cells are
terminated to 50 Ohm chip resistors as shown in Fig. 20-c. This
configuration allows to validate the presence of blind angles
through the measurement of the active element radiation pattern
of the central element embedded into a relevant array
environment. In this test scenario, scan blindness in a phased
array configuration can be revealed by the presence of nulls
measured radiation patterns of the embedded element.
The prototype was built through a sequential build-up PCB
process requiring three production stages. In the first and
second phase, the radiating board (from D1 to G2) and the BFN
manifold (from G3 to D6) were fabricated independently. In a
third phase, the two boards were aligned and bonded through a
29
29.5
30
30.5
31
31.5
32
Frequency (GHz)
(b)
Fig. 19 Active S11 of the Tx elements scanning on the E plane (a) and on
he H plane (b).
conductive adhesive layer, CA, in a thermally controlled press.
The layer CA was implemented using the Loctite Abelstik™
material which provides high electrical and thermal
conductivity as well as low curing temperature.
The bonding procedure, involved three types of slots, namely
one of the Tx and two of the dual-band antennas. The same slot
layout was replicated identically in layers G2 and G3 (Fig. 20b) while slightly larger apertures where created in the adhesive
conducting layer CA. The effectiveness of the proposed
integration approach was firstly validated through X-rays and
cross-section measurements of the bonded layers. As it can be
observed in Fig. 21, the maximum measured misalignment
between the two boards in the horizontal plan is equal to 19µm.
It has been verified through simulations that misalignments up
to 50µm have no effect on the antenna performance.
The simulated and measured reflection coefficient of the
embedded element are shown in Fig. 22 and 23. The Rx and Tx
element’s performance are well consistent with the numerical
results showing a measured bandwidth equal from 20.15 to
21.86 GHz and from 29.6 to 31.28 GHz for the Rx and Tx case
respectively.
The embedded co-polar and cross-polar radiation patterns along
the E- and H-plane were measured for the Rx and Tx elements
as shown in Fig. 24 and 25 respectively. In both cases, co-polar
radiation patterns present broad beams without any null within
the hemispherical coverage which in turn results in wide-angle
scanning performance. A gain of 4.4 dBi was determined for
both the Tx and Rx embedded elements by using the Friis
formula and a standard gain horn. In both operational bands the
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10
cross polarization levels are well below 20 dB for the Tx
antenna whereas values higher than the simulated ones can be
observed in the Rx antenna in the H plane. This behavior is
ascribed to an imperfect shielding of the outer conductor which
deviates the electric field lines. The evaluation of the scanning
performance of the arrays was done using the embedded
radiation patterns shown in Fig. 24 and 25 to generate array
patterns pointing down to θ=60° in both E and H planes.
Results, presented in Fig. 26, were obtained simulating a
uniformly excited array. Superimposed to the array pattern are
the element pattern and the ideal cosθ pattern. As it can be seen,
grating lobe free patterns are obtained for scan angle up to 50°.
At 60° grating lobes appear in Rx because cell size is exactly
λ/2 at 20 GHz.
Fig. 21. X-ray image of the conductive adhesive layer between G2
and G3 with two side views of the same layer.
0
Simulations
Measurements
(a)
S11 (dB)
-5
-10
-15
-20
-25
-30
19
19.5
20
20.5
21
21.5
22
Frequency (GHz)
Fig. 22 Return loss of the central Rx element (circled in red) of the
array shown in Fig. 20.
(b)
0
Simulations
Measurements
S11 (dB)
-5
-10
-15
-20
-25
-30
29
29.5
30
30.5
31
31.5
32
Frequency (GHz)
Fig. 23 Return loss of the central Tx element (circled in red) of the
array shown in Fig. 20.
(c)
Fig. 20. Array prototype test structure: a) layer G1; b) layer G2 or G3,
blind vias used to create cavities around the slots are also visible; c)
bottom view.
VI. CONCLUSIONS
In this paper a dual band phased array configuration, operating
at K/Ka band has been studied and experimentally validated.
The proposed solution consists of dual-band radiating elements
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330
0 deg
11
0
30
-5
60
270
-20 -10 0
10 dB
Array radiation pattern (dB)
-10
300
-15
-20
-25
-30
θ=0 deg
θ=10 deg
θ=20 deg
-35
θ=30 deg
θ=40 deg
θ=50 deg
θ=60 deg
Element pattern
cosθ pattern
-40
-45
240
120
-50
-80
210
-40
-20
0
20
Elevation angle (deg)
40
60
80
(a)
150
180
0
0 deg
30
300
60
-5
Array radiation pattern (dB)
Fig. 24 Co-polar and cross-polar radiation patterns at 20 GHz of the
central Rx element of the array shown in Fig. 21-a. Solid line: E-plane;
dashed line: H-plane.
330
-60
-10
-15
-20
-25
-30
θ=0 deg
θ=10 deg
θ=20 deg
-35
θ=30 deg
θ=40 deg
θ=50 deg
θ=60 deg
Element pattern
cosθ pattern
-40
-45
270
-50
-30 -20 -10 0 10 dB
-80
-60
-40
-20
0
20
40
60
80
Elevation angle (deg)
(b)
120
240
0
-5
Fig. 25 Co-polar and cross-polar radiation patterns at 30 GHz of the
central Tx element of the array shown in Fig. 21-a. Solid line: E-plane;
dashed line: H-plane.
interleaved with single band elements. The interleaved
configuration limits the number of elements in the array and it
avoids the use of multiband or wideband radiators which may
be cumbersome to design and to integrate. The radiating
elements are designed to be integrated with multicore SiGe
BiCMOS chips and they are optimized to scan the beam to more
than 50° in both the E plane and the H plane. A new integration
technique was introduced to enable more complex and dense
PCB configuration. With the proposed integration technique it
is possible to split the realization of the radiation board and of
the BFN manifold in two separate processes, facilitating the
realization of the antenna and the integration of the multicore
chips. While the paper focused on K/Ka band satellite
communications, the solution proposed has a more general
validity and it may be applied to different applications which
require dual band highly integrated arrays with a large bands
separation.
-10
-15
-20
-25
-30
θ=0 deg
θ=10 deg
θ=20 deg
-35
θ=30 deg
θ=40 deg
θ=50 deg
θ=60 deg
Element pattern
cosθ pattern
-40
-45
-50
-80
-60
-40
-20
0
20
Elevation angle (deg)
40
60
80
(c)
0
-5
Array radiation pattern (dB)
180
Array radiation pattern (dB)
150
210
-10
-15
-20
-25
-30
θ=0 deg
θ=10 deg
θ=20 deg
-35
θ=30 deg
θ=40 deg
θ=50 deg
θ=60 deg
Element pattern
cosθ pattern
-40
-45
-50
-80
ACKNOWLEDGMENT
The authors are thankful to Prof. Steven Gao and the staff of
the Antenna Laboratory at the University of Kent (UK) for their
support in antenna measurements.
-60
-40
-20
0
20
Elevation angle (deg)
40
60
80
(d)
Fig. 26 Array scanning performance based on the measured embedded
element patterns: a) scanning along the E-plane at 20 GHz; b) scanning
along the H-plane at 20 GHz; c) scanning along the E-plane at 30 GHz;
d) scanning along the H-plane at 30 GHz.
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0018-926X (c) 2015 IEEE. Personal use is permitted, but republication/redistribution requires IEEE permission. See http://www.ieee.org/publications_standards/publications/rights/index.html for more information.
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Ali Imran Shandu received the B.S. degree in
electronics engineering from COMSATS Institute
of Information Technology (CIIT), Pakistan, in
2007 and the M.S. degree in communication
engineering from CHALMERS University of
Science and Technology, Gothenburg, Sweden in
2010. He is currently pursuing the Ph.D. degree in
electrical engineering at the Division of Computer,
Electrical, and Mathematical Sciences and
Engineering (CEMSE), King Abdullah University
of Science and Technology (KAUST), Thuwal,
Saudi Arabia.
Since September 2007, he has been a Lecturer with the Department of Electrical
Engineering, CIIT Lahore, Pakistan. From September 2011 to March 2013, he
worked as a Research Engineer with the Microwave Lab, University of
Calabria, Italy. His research interests include inverse electromagnetic
scattering problems with emphasis on sparsity-promoting regularization
schemes and micro-strip antennas.
Emilio Arnieri was born in Cosenza, Italy, in 1977.
He received the degree (with honors) in Information
Technology Engineering from the University of
Calabria, Rende, Italy, in 2003 and the Ph.D.
Degree in Electronic Engineering from the
University “Mediterranea” of Reggio Calabria, in
2007. Currently, he is an Assistant Professor with
the Department of Informatics, Modeling,
Electronics and System Engineering (DIMES),
University of Calabria (Italy). His main research
activities concern the development of dual-band antennas and millimeter-wave
components, synthetic aperture radar (SAR), development of numerical
methods for the electromagnetic modeling of microwave, and millimeter-wave
circuits (substrate integrated circuits, slotted substrate-integrated waveguide
arrays, and substrate-integrated waveguide resonators).
Giandomenico Amendola (M’96, SM '15) received
the Electrical Engineering degree from the Università
della Calabria, Rende (CS), Italy, in 1987. From 1988
to 1992, he was a Research Fellow with the Proton
Synchrotron Division, European Center for Nuclear
Research (CERN), Geneva, Switzerland. He is with the
Dipartimento di Elettronica, Informatica e
Sistemistica, Università della Calabria, where he is
currently an Associate Professor. His main research
interests are in the area of antennas, phased arrays and
microwave and millimeter-wave circuits.
Luigi Boccia (S’00 - M’03) was heart born in Lungro,
Italy, in 1975. He received the degree in Information
Technology Engineering from the University of
Calabria, Rende, Italy, and the Ph.D in Electronic
Engineering from the University "Mediterranea" of
Reggio Calabria, Italy, in 2000 and 2003 respectively.
Since January 2005 he has been Assistant Professor in
electromagnetics at the Faculty of Engineering of the
University of Calabria. His current research interests
include low-multipath GNSS antennas, reflectarrays,
beam scanning antennas, micro- and millimetre-wave
IC design. Dr. Boccia is also member of the European
Microwave Association (EuMA) and of the Società Italiana di
Elettromagnetismo (SIEm). He serves as a technical reviewer for many
international journals and conferences. He is the co-editor of the “Space
Antenna Handbook” (Wiley, 2012).
13
Erika Meniconi was born in Perugia, Italy on
July 13, 1983. In 2007 she received her bachelor
degree in Information Engineering, in 2010 her
M.Sc. degree (with distinction) in Electronic
Engineering and in 2015 her PhD title from the
University of Studies of Perugia, Italy. For her
bachelor thesis research, she worked on phase
shifters for reconfigurable antennas at the
Department of Electronic and Information
Engineering (DIEI) of the University of Perugia,
Italy. Her Master thesis was focused on RFMEMS based switching modules for Ka-band
applications and was carried out at the research department of Airbus Defence
and Space GmbH, Ottobrunn, Germany.
From 2010 till 2014, she successfully worked on her Ph.D. at Airbus Defence
and Space GmbH, Ottobrunn, Germany, in cooperation with the University of
Studies of Perugia (DIEI Department). Her main research activity included
design, integration, and characterization of RF-MEMS based subsystems and
highly integrated RF-frontends for electronically steerable antennas. Since end
of 2014 she is working as Senior Design Engineer at TriQuint Semiconductor
GmbH, a company of Qorvo, in Munich, Germany.
Volker Ziegler received his Dipl.-Ing. degree in
electrical engineering and his Dr.-Ing. degree (with
honors) both from the University of Ulm,
Germany, in 1997 and 2001, respectively. From
2002 to 2003, he was member of the "Knowledge
Exchange Group for Research and Technology" at
the DaimlerChrysler AG in Stuttgart, Germany.
During this trainee period, he was working at the
University of Michigan, Ann Arbor, USA on the
design of GaN high-power MMICs and at United
Monolithic Semiconductors, Orsay, France on the
modeling and characterisation of III-V
semiconductor devices. Afterwards, he joined
EADS Innovation Works, Ottobrunn, Germany, where he became an EADS
Expert for "Microwave Technologies and Systems" in 2007. From 2013 to
2015, he was the Head of Team “RF and Waveforms” within AIRBUS Group
Innovations. Since 2016, he is the Head of Team “Automatic Flight Systems” ,
responsible for the research performed in the field of automated systems
including integrated perception, trajectory optimization, image processing and
virtual reality for human-machine-interfaces.
Volker Ziegler is senior member of the IEEE, member of the IEEE MTT-S
Technical Coordinating Committee 21 on RF-MEMS and member of the IEEE
MTT Antennas & Propagation German Chapter Executive Board. He served
twice as Associated Editor for the „International Journal of Microwave and
Wireless Technologies” and was for several years a member of the Technical
Program Committee for the European Microwave Week. He authored or coauthored more than 70 papers, holds eleven patents and is an industrial advisor
of the "Component Technical Board on Microwaves" for the European Space
Agency.
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