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    A Dual-Polarized Planar-Array Antenna for

    S-Band and X-Band

    Airborne

    Applications

    S

    H

    Y R

    2

    , a K C

    1

     Department of Electrical and Computer Engineering, Texas A M University

    College Station, TX 77843-3128, USA

    Tel: +1 (979) 845-5285; E-mail: [email protected]

    21ntelligent Automation, Inc.

    Rockville, MD 20855, USA

    Abstract

    A new dual-frequency dual-polarized array antenna for airborne applications is presented in this paper. Two planar arrays

    with thin substrates (RIT Ouroid 5880 substrate, with

    e;

    = 2.2 and a thickness of 0.13 mm) are integrated to provide

    simultaneous operation at S band (3 GHz) and X band (10 GHz). Each 3 GHz antenna element is a large rectangular ring

    resonator antenna, and has a 9.5 dBi gain that is about 3 dB higher than the gain of an ordinary ring antenna. The 10 GHz

    antenna elements are circular patches. They are combined to form the array with a gain of 18.3 dBi, using a series-fed

    structure to save the space of the feeding line network. The ultra-thin array can be easily placed on an aircraft's fuselage, due

    to its lightweight and conformal structure. It will be useful for wireless communication, radar, remote sensing, and surveillance

    applications.

    Keywords: Antenna arrays; microstrip arrays; microwave antenna arrays; aircraft antennas; planar arrays; polarization

    1. Introduction

    M

    odern wireless communication systems demand low-profile,

    lightweight, and relatively inexpensive antennas [1]. There

    has been increasing interest in the development of dual-polarized

    antennas/arrays, due to many advantages in performance improve

    ment for wireless communication and radar systems. Dual

    polarization avoids the requirement

    of

    precise alignment needed in

    single-polarized systems. Dual-polarized operation can also pro

    vide more information for radar systems, can increase the isolation

    between the transmitting and receiving signals

    of

    transceivers and

    transponders, and can double the capacity of communication sys

    tems by means of frequency reuse [2, 3]. In simultaneous transmit

    ting-receiving applications, dual-polarized antennas with two-port

    connections offer an alternative to the commonly used bulky

    circulator, or separate transmitting and receiving antennas. Further

    more, dual-polarized antennas can provide polarization diversity,

    which prevents the system's performance degradation due to multi

    path fading in complex propagation environments [4]. Compared

    with space diversity, the polarization-diversity technique has the

    advantage of reducing the number and size of the antenna elements

    in the system.

    To create dual polarization, the antenna element has to be fed

    at two orthogonal points or edges, such that two degenerate reso

    nant modes can be excited for the orthogonal polarizations, i.e.,

    vertical and horizontal polarizations. Design techniques of dual

    polarized antennas can be classified into three main categories. The

    first is to make an orthogonal arrangement

    of

    the radiation ele-

    ments for two polarizations [5, 6]. The second is to properly

    choose stacked structures of the radiating elements [7, 8]. The third

    is to use special feeding techniques [9, 10]. In general, symmetric

    structures tend to give better dual-polarization performance. At

    higher frequencies, a dielectric-resonator antenna can be used to

    reduce the metallic loss of the patch [11].

    The dual-polarized antenna elements can be assembled to

    construct a high-gain array. Although many dual-polarized anten

    nas have been proposed, not all of them are good candidates for

    array design, due to their complex structures and feeding-line net

    works. Many of them are bulky and heavy, and not suitable for air

    borne applications. On the other hand, isolation is one

    of

    the

    important parameters to be considered in dual-polarized array

    design. Most reported dual-polarized arrays achieve at least 20 dB

    isolation [12-15]. To minimize the coupling between the feed-line

    networks, a proximity/aperture-coupling structure can be applied to

    prevent radiation due to the microstrip line and radiator from

    degrading the polarization performance. The multilayer structure

    can also be used to enhance the isolation, in which isolations of

    better than 20-30 dB can be obtained with more-complicated struc

    tures. However, most dual-polarized antenna designs will result in

    a bulky array that is not suitable for use in aircraft, airships, or

    unmanned aerial vehicles (DAVs).

    In many airborne applications, an array antenna should have

    good isolation, high efficiency, and ease of integration with the

    aerial vehicle. A simple feeding-line network with lower loss and

    high isolation is generally desired. Microstrip series-fed arrays

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    have been shown to have a structure that enhances the antenna's

    efficiency [1]. This is because the array feeding-line length is

    significantly reduced, compared to the conventional corporate feed

    ing-line network. Such arrays can be either traveling-wave or reso

    nant arrays. A planar structure with a thin and flexible substrate is

    a good choice, because it will not disturb the appearance

    of

    the air

    craft, and can be easily integrated with electronic devices for signal

    processing.

    In this paper, a dual-frequency dual-polarized array antenna is

    presented for airborne antenna applications. A multilayer structure

    is adopted for dual-band operation. The antenna arrays for the two

    frequencies are separated on different layers. To reduce the array's

    volume and weight, a series-fed network is used. An ultra-thin sub

    strate is chosen in order to make the array conformal, and the array

    can be easily placed on an aircraft's fuselage, or inside the aircraft.

    The parameters affecting the array's characteristics are discussed,

    and the measured return losses, radiation gains, and array patterns

    are presented.

    Two RTlDuroid 5880 substrates (61 =63 =2.2 and a foam

    layer  6 2 = 1.06)

    form

    the multilayer structure. The thicknesses

    of

    the substrates   and h

    2

    ) are both only 0.13 rom (5 mil). These

    ultra-thin and flexible substrates make it possible for the array to

    be easily attached onto the aircraf t' s fuselage, or installed inside

    the a ircraft . The foam layer has a th ickness of

    h

    2

    =1.6mm. The

    dimensions of the array were opt imized by using the full-wave

    electromagnetic simulator, I [.

    2 1 X Band Antenna and Subarray

    The X-band array uses the circular patch as its unit antenna

    element. The patch radius, R, for the dominan t TM)) mode at the

    resonant frequency (Ir in GHz) can be calculated from [17]

    2 Array Design

    (1)

    Unlike most other elements, the electrical parameters

    of

    the

    substrate will be affected by the temperature and moisture varia

    tions occurring in airborne applications, and these affect the

    performance

    of the antennas. The magnitude of the transmitting

    power may also generate a large amount of heat, which results in a

    significantly increased temperature. The choice of the substrate is

    therefore an important factor in airborne-antenna design . The

    configuration

    of

    the antenna element determines the complexity

    of

    the array feeding-line network, which controls the size and mass of

    the array. The configuration of the feeding-line networks may also

    incur different levels of port isolation and pattern polarization.

    Important design considerations of a dual-polarized airborne array

    antenna are summarized in Table

    I.

    Our goal is to design a low

    mass conformal array antenna for airborne applications. An ultra

    thin substrate is used to achieve the

    conformal

    antenna.

    D

    The multi layer array structure for dual-band (S band and X

    band) operation is shown in Figure

    I.

    The S-band antenna elements

    sit on the top layer , and the X-band antennas are on the bottom

    layer. A foam layer  

    2

    ) serves as the spacer, and is sandwiched

    between the two subst rate layers . One of the important design

    considerations for this multilayer dual-band array is that the S-band

    antenna element should be nearly transparent to the X-band

    antenna elements. Otherwise, the S-band element may degrade the

    performance of

    the X-band antenna.

    y.

    x

    Figure 1. The multilayer structure of th e dual- band dual

    polarized array

    antenna.

    Table 1. Design considerations

    for

    the airborne array antenna.

    Factor

    Impact

    Temperature

    This is determined by the aerial conditions and delivered power, which will affect the electrical

    parameters

    ofthe

    substrate.

    Moisture

    The effects due to moisture are similar to the temperature effects.

    Electrical parameters

    This controls the antenna's nerformance and is mainly changed by large temperature variations.

    Feeding-line network

    This determines the complexityof the array. Unsuitable antenna elements could result in a bulky

    and heavy array.

    Isolation

    Port-to-port isolation and cross-polarization level can be enhanced by using well-designed

    feeing-line networks, such as proximity/aperture coupling and multilayer configurations.

    Coupling

    For dual-frequency operation, the interference between antennas operating at different

    frequencies may affect radiation patterns and gain.

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    where O and h (in em) are the relative dielectric constant and

    thickness of

    the substrate, respectively. At the operating frequency,

    fr

    =10GHz, an initial value of R of 5.82 mm, calculated from

    Equation

     I ,

    was used. The optimized value

    of

    5.95

    mm

    was

    obtainedwith the aid

    of

    IE3D.

    The circular patches are fed with microstrip lines at the

    circumferential edge, as shown in Figure2a. For a single circular

    patch, two microstrip feeding lines are used to feed the circular

    patch to generate two orthogonally radiating TM

    t

    1

    modes for dual

    polarized operation. Two feed points are located at the edge

    of

    the

    patch, 90

    0

    away from each other, so that the coupling between

    these two ports can be minimized. The port isolation also depends

    on the quality factor of the patch. Increasing the substrate's thick

    ness decreases the isolation [18]. Therefore, using thin substrates

    could improve the quality

    of

    isolation.

    with

    F =8.79I

    F

    ,

    (2)

    , 2R , L H-port

    <

    l

    L-  --   --- ::::_ :t------------------- -------------------

    Figure 2a. The layout of the X-band antenna, where

    L =

    106,

    W =183, R =

    5

    .82,

    LxI =

    22,

    and W

    xt

    =

    0.17 (all dimensions

    are in mm),

    ..-.._.  _._.._.

    L,5

    ----------------------------------------------------

     1

    ,

    ,

    .

    H-port :

     

    Figure 2b.

    The

    layout of the S-band antenna, where

    L

    =

    106,

    W=183

    , L

    st

    =53.89 , L

    s2

    =44.6 , L

    s3

    =0.94 , L

    s4

    =19.31 ,

    L

    ss

    =

    34

    .17,

    W

    st

    =

    4

    .9 , and W

    s2

    =

    7.8 (all dimensions

    are

    in

    mm).

    Figure2a shows a 4 x 8 dual-polarized X-band array. The V

    port and the H port are the input ports for the two orthogonal

    polarizations (vertical and horizontal). The array is composed

    of

    two 4

    x

    4 subarrays. The corporate-fed power-divider lines split the

    input power at eachport to the subarrays.Within each subarray, the

    circular patches are configured into four 4

    x

    1 series-fed resonant

    type arrays, which make the total array compact and have less

    microstrip line losses than would a purely corporate-fed type of

    array [19]. An open circuit is placed after the last patch

    of

    each

    4 x 1 array.The spacing between adjacent circular-patch centers is

    about one guided wavelength

     

    g

    =

    21.5mm at 10 GHz). This is

    equivalent to a 360

    0

    phase shift between patches, such that the

    main beam points to the broadside. The power coupled to each

    patch can also be controlled by adjusting the size

    of

    the individual

    patch to achieve a tapered amplitude distribution for a lower

    sidelobe design. Another advantage of using the series-fed array

    configuration is that the array can be easily converted into a travel

    ing-wave array, with a matched termination at the end

    of

    the last

    elements, if a steered-beamarray is needed.

    2 2 S Band Antenna and Subarray

    Figure 3. The geometry of the dual-band dual-polarized array

    antenna.

    As shown in Figure 2b, the S-band antenna elements are

    printed on the top substrate, and are separated from the X-band ele

    ments by the foam layer. To reduce the blocking of the radiation

    from the X-band elements at the bottom layer, the shape of the S

    band elements has to be carefully selected. A ring configuration

    was a good candidate, since it uses less metallization than an

    equivalent patch element. Here, a square-ringmicrostrip antenna is

    used as the unit element

    of

    the S-band array. Because antenna ele

    ments at both frequency bands share the same aperture, it is also

    preferred that the number of elements on the top layer be as small

    as possible, to minimize the blocking effects.

    The stacked X-band and S-band array antennas are shown in

    Figure 3. As can be seen in the figure, the four sides of the square

    ring element are laid out in such a way that they only cover part of

    the feeding lines on the bottom layer, but none

    of

    the radiating ele

    ments. Unlike an ordinary microstrip-ring antenna that has a mean

    circumference equal to a guided wavelength, the antenna proposed

    here has a mean circumference

    of

    about 2

    g

     

    g

    =

    82.44mm at

    V-port .

    (S-band) •

    H-port

    (X-band)

    H-port

    (S-band)

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    • Mean radius of the ring - 2

      9

    GHz

    • Select two operating frequencies I r I I

    • Use very thin substrates

    10 GHz

    • Use Eq. (1)

    to

    calculate R

    • Select I

    X1

    - 1  '9' w

    x1

    = 0.17 mm

    • Based on (l

    s2

    - Is1)< (lx1 - 2R)

    and (l

    s2

    + I

    s1)

     2 - 2 '9

     select

    I

    s1

    and I

    s2

    • Select I

    s3

    and W

    s3

    (50 ohm)

    No

    • Design the power divider

    • Interconnect the patch elements

    No

    Yes

    Yes

    Overlay the 3 GHz elements on the 10 GHz elements with

    minimum blockage of the circular patches

    Figure 4. The design flowchart of the proposed

    antenna array.

    3 GHz). Although the size of the proposed unit element is larger

    than an ordinary ring antenna, its gain is about twice as high,

    because

    of

    its larger radiation-aperture area. The ring is loaded by

    two gaps at two of its parallel sides, and these make it possible to

    achieve a 50 n input match at the edge

    of

    the third side without

    using a small value

    of

    Ls

     

    LsI

    as mentioned in [20]. For an edge-

    fed microstrip ring, if a second feed line is added to the orthogonal

    edge, the coupling between the two feeding ports will be high. The

    V-port and H-port feeds are therefore placed at two individual ele

    ments, so that the coupling between the two ports can be signifi

    cantly reduced. Using separate elements seems to increase the

    number of antenna elements within a given aperture. However, this

    harmful effect could be minimized by reducing the number

    of

    ele

    ments with the use of larger-sized microstrip rings. A design flow

    chart of the proposed antenna array is provided in Figure 4.

    3. Measurement and Discussion

    A dual-band array prototype was fabricated and tested in the

    anechoic chamber of the Texas A&M University. The array was

    tested for one polarization at one frequency at a time, while the

    other three ports were terminated with 50n loads. Detailed simu

    lated and measured results are given and discussed in the follow

    ing.

    3 X-band Array

    top of it. The center frequency of both polarizations was at around

    9.95 GHz, and the return losses  8

    11

    and 8

    22

    ) were better than

    22 dB. 8

    11

    was the return loss for the V port, and 8

    22

    was for the

    H port. The isolation  

    21

    or 8

    12

    )

    between the V and the H

    polarizations was better than 30 dB at the resonant frequency, and

    better than 25 dB over a wide frequency band. These results were

    considered excellent for a dual-polarized array for which the feed

    ing lines for both polarizations were present at the same layer.

    These results were similar to those reported in [4], and the physical

    size of the array was reduced, due to the hybrid use

    of

    the corpo

    rate-fed and series-fed configurations.

    Normalized measured radiation patterns are shown in Fig

    ure 6. Well-defined patterns were observed. Cross-polarization lev

    els in the E plane and H plane were 17dB below the co-polarized

    beam peaks. It was noted that the dimensions

    of

    the ground plane

    used for the array were about 18.3 em x 10.6 em, which were close

    to those of the array's aperture. This could create strong edge

    diffraction, and might account for the relatively higher cross

    polarization levels. The peak sidelobe levels (SLL) were

    -10

    to

    -13dB, which were normal for the arrays with a uniform ampli

    tude distribution. The asymmetric sidelobes of the H port were

    caused by its feeding-line network asymmetry with respect to the

    array's center. The maximum measured gain was

    18.3

    dBi, and the

    averaged radiation efficiency was 31%. The half-power beamwidth

    (HPBW)

    of

    the x-z plane was 9°, and that

    of

    the y-z plane was 17°.

    This difference was due to the asymmetry of the 4

    x

    8 array

    arrangement.

    Figure 5 shows the return loss and the isolation

    of

    the X-band

    array. The measurements were carried out with the S-band layer on

    Theoretically, a microstrip antenna has a very good front-to

    back ratio (FBR), due to its infinite - or relatively large - ground

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    plane . This is similar to the case when an airborne antenna is

    mounted on an airframe. Here, with a finite ground plane , the

    front-to-back radiation ratios of both the E and H planes were bet

    ter than 30 dB. The back radiation was very small , and hence not

    shown. A ground plane with a larger dimension can provide a

    higher front-to-back radiation ratio, since the coupling and diffrac

    tion

    of

    electromagnetic waves are reduced. Detailed specifications

    of the X-band array are summarized in Table 2.

    3 2 S Band Array

    - - Mea sured E-planeco-pol

    --- -- Measured E-plane x-pol

    _

     

    _

    <

    _ Simulated E-plane co-pol

      Measured H-plane co-pol

    -----

    Measured H-plane x-pol

    Simulated H-plane co-pol

    Figure 6a. The radiation patterns of the X-band array: V-pert

    feed, E plane.

    he return loss of the S-band array is shown in Figure 7. The

    measurements were carried out with the X-band layer under the

    S-band layer. About 19 dB return loss was obtained at the resonant

    frequency of 2.96 GHz, for both polarizations. Since two separate

    elements were used for two polarizations, the results show that the

    port isolation was close to 30 dB. Normalized measured radiation

    patterns for both polarizations are shown in Figure 8. A typical sin

    gle main beam with a wide 3 dB beamwidth was observed . The

    cross-polarization levels were better than 20 dB. The maximum

    gain of the antenna was measured to be 9.5 dBi, and the averaged

    radiation efficiency was 81%. The HPBW of the S-band array was

    about 56° on each plane. The front-to-back radiation ratios on both

    planes were better than 34 dB for the V port and 25 dB for the H

    port, which indicated that the dimensions of the ground plane were

    acceptable for the S-band antenna.

    (dB) -30 -20 -10

     

    Measured E-plane co-pol

    Measured E-plane x-pol

    Simulated E-plane co-pol

    Figure 6b. The radiation patterns of the X-band array: V-port

    feed, H plane.

    -20

    - Measured S11

    ........Simulated S11

     > < Measured S12

    -10 ...

    o

    ·30 .

    -20 -10

      Measured H-plane co-pol

    0° - - - - - Measured H-plane x-pol

    Simulated H-plane co-pol

    Figure 6c. The radiation patterns of the X-band array: H-port

    feed, E plane.

    -30 .

    -20 .

    -40

    9.5 9.6 9.7 9.8 9.9 10 10.1 10.2 10.3 10.4 10.5

    Frequency (GHz)

    Figure Sa. The S parameters of the X-band array, where

    port

    1

    is the V-port feed for vertical polarization.

    o

    Figure Sb. The S parameters ofthe X-band array, where port 2

    is the H-port feed for horizontal polarization.

    Figure 6d. The radiation patterns of the X-band array: H-port

    feed, H plane.

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    Table

    2. A

    summary of the measured and simulated results for the X-band

    and

    S-band array antennas.

    X

    -Band S-Band

    Polarization

    V

    Port

    H

    Port

    V

    Port

    HPort

    Frequency (GHz)

    Measurement 9.8-9.98 9.81-10.0 2.94-2.96 2.94-2.96

    Simulation 9.91-9.99 9.9-10.0 2.94-2.96

    2.94-2.96

    Bandwidth (%)

    Measurement

    1.8

    2.3

    1.03 1.03

    Simulation

    1.0 1.0 1.03 1.03

    Gain (dBi)

    Measurement

    18.3

    17.3 9.5

    7.9

    Simulation 17.6 17.6 8.72

    8.73

    Efficiency (%) Measurement 32.4 28.8 96.8 66.8

    Simulation 27.5 27.5 80.9

    80.9

    HPBW (degrees)

    E plane

    17°

    8.9° 58° 59°

    Hplane

    9.5°

      7 4°

    53° 52°

    Peak SLL (dB)

    Measurement

    -12

    .3 -1 0.0

    None

    None

    Simulation -13 .0 -13 .0

    FBR (dB) -30

    -30 -34 .8

    -25.5

    Isolation (dB)

    > 3I.l > 25.3 >36.4

    >33 .8

    X to S band X to S band S to X band S to X band

    3.3 Mutual Coupling Effects of Two Layers

    Figure

    7.

    The

    S parameters

    of the S-band

    array, where port 1

    is the V-port feed for vertical polarization, and port 2 is the H

    port

    feed for horizontal polarization.

    - - Measured [- plane co-pol

     

    Measured [- planes -pot

      Measured If-plane co-pol

     

    Measur ed ..plane x..pol

    • SimulatedE-plane co-pol

    Simulated H-plane co-pol

    - - Measured E-plane co-pol

      Measured [ -plane r-pel

      Measured H-plane co-pol

    - Measu red H-plan e s-pot

    • S imulat ed [ - planeco-pol

    Simulated If-planeco-pol

    -90

    Figure

    8a. Radiation

    patterns

    ofthe

    S-band array

    :

    V-port

    feed.

    Figure 8b. Radiation patterns of the S-band array: H-port feed.

    ments for the S-band array, with or without the presence of the X

    band array, including the S parameters and the radiation patterns.

    When the X band was presented, the isolation of S-to-X (from the

    ports

    of

    the S-band antenna to the ports

    of

    the X-band) was

    between 33 dB and 42 dB; the isolation of X-to-S was better than

    25 dB.

    It

    was observed that increasing the spacing between the S

    band and the X-band antennas did not significantly improve the

    isolation. Instead, it raised the center frequency

    of

    the S-band

    antenna, and vice versa. Consider the case where the foam-layer

    thickness  

    z

    )

    is changed within

    ±O.5 mm

    , If h

    z

    is increased by

    3.2.15.1

    - - - - Measured511

     

    Measured 522

    - Measreud 521

    -e-o-e-Simulated S

     

    - Simulated S22

    2.95 3 3.05

    Frequency (GHz)

    2.9

    .85

    -20 - - - - - -- - - - -- - - - - - -- - - - -- - - - - - - -- -- - - - - - - - - - -

    -30

    ·10

    -40

    -50

    2.8

    CD

     

    Simulated results

    of

    the return losses and radiation patterns

    from IE3D are also shown for comparison. Good agreement was

    observed for both frequency bands. Small discrepancies in the

    resonant frequencies may be attributed to the accuracy of the

    permittivity and the thickness dimension ofthe foam layer given by

    the manufacturer. The former value played a more important role.

    The resonant frequency shifts from 3 GHz to 2.95 GHz when the

    dielectric constant of the foam layer

      6Z)

    changes from 1.06 to

    I.l2 , a 5.7% change within the inaccuracy

    of

    the fabrication proc

    ess. The effects due to the thickness ofthe foam layer are described

    in the following section. The specifications of the S-band array are

    summarized in Table 2.

    The results presented here for both the X and S bands were

    measured with the concurrent presence of

    both antenna layers

    (dual-band operation). However, measurements of the single layer

    without the presence of the other layer,

    i.e.,

    single-band operation,

    were also conducted, to investigate the mutual-coupling effects

    between the elements of different frequency bands.

    It

    was found

    that there were no distinct variations between the two measure-

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      Dual layer

    - - - X-ba nd la yer only

    -90

    Figure

    9a.

    Comparisons

    of

    the X-band

    radiation patterns of

    the If-port feed for the E plane.

    5 Acknowledgment

    The authors would like to thank the Rogers Corporation for

    donating the high-frequency laminates, and Mr. Ming-Yi

    Li of

    Texas A&M University for his technical assistance and helpful

    suggestions.

    6 References

    1. A. Vallecchi and G. Gentili, Design of Dual-Polarized Series

    Fed Microstrip Arrays with Low Losses and High Polarization

    Purity, IEEE Transactions on Antennas and Propagation, AP-S3,

    5, May 2005, pp. 1791-1798.

    3. X. Qu, S. Zhong, Y. Zhang, and W. Wang, Design of an SIX

    Dual-Band Dual-Polarised Microstrip Antenna Array for SAR

    Applications,

    lET

    Microwave, Antennas, and Propagation, 1, 2,

    April 2007, pp. 513-517.

    5. G. Chattopadhyay and J. Zmuidzinas, A Dual-Polarized Slot

    Antenna for Millimeter Waves, IEEE Transactions on Antennas

    and Propagation, AP-46, 5, May 1998, pp. 736-737.

    2. S. Gao and A. Sambell, Dual-Polarized Broad-Band Microstrip

    Antennas Fed by Proximity Coupling, IEEE Transactions on

    Antennas and Propagation, AP-S3, 1, January 2005, pp. 526-530.

    4. S. Zhong, X. Yang, S. Gao, and J. Cui, Comer-Fed Microstrip

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    of

    Dual-Polarization Operation,

    IEEE Transactions on Antennas and Propagation, AP SO 10,

    October 2002, pp. 1473-1480.

    -30dB)

     

    Dual layer

    - - - X-band layer only

    Figure

    9b. Comparisons of the X-band radiation patterns of

    the

    H-port feed for

    the

    H plane.

    0.1 mm, the frequency is raised by 40 MHz; while if

    h

    2

    is

    decreased by 0.1 mm, the frequency is reduced by about 60 MHz.

    6. K. Mak, H. Wong, and M. Luk, A Shorted Bowtie Patch

    Antenna with a Cross Dipole for Dual Polarization, IEEE Anten

    nas and WirelessPropagation Letters, 6, 2007, pp. 126-129.

    For the X-band array, only small variations in the sidelobe

    levels were observed, and the measured peak gain dropped about

    0.5 dB with the presence of the top S-band layer. Comparisons of

    the radiation patterns

    of

    the H port are shown in Figure 9. The S

    band layer presented little effect on the performance of the X-band

    layer. The statement that one antenna layer was transparent to the

    other one was therefore confirmed.

    7. S. Gao and A. Sambell, Dual-Polarized Broad-Band Microstrip

    Antennas Fed by Proximity Coupling, IEEE Transactions on

    Antennas and Propagation, AP-S3, 1, January 2005, pp. 526-530.

    8. K. Ghorbani and R. Waterhouse, Dual Polarized Wide-Band

    Aperture Stacked Patch Antennas, IEEE Transactions on Anten

    nas and Propagation, AP-S2, 8, August 2004, pp. 2171-2174.

    4 Conclusions

    A dual-frequency (S-band and X-band) dual-polarization

    array antenna has been developed. An ultra-thin structure was

    adopted for the purpose of use with aircraft. The conformal array

    can be installed on the airframe or inside the aircraft, due to its

    small size and light weight. The X-band array used a series-fed

    configuration to save the space

    of

    the feeding-line network. The S

    band array adopted a larger radiation aperture to decrease the num

    ber of elements, to reduce the blockage, and to enhance the radia

    tion gain. The V and H ports were put on two separate elements to

    achieve high isolation. More subarrays could be assembled to

    obtain higher gain with a narrower beamwidth. The newly devel

    oped dual-frequency dual-polarization array antenna should be use

    ful for future wireless communications, remote sensing, surveil

    lance, radar systems, and UAV applications.

    9. D. Krishna, M. Gopikrishna, C. Aanandan, P. Mohanan, and K.

    Vasudevan, Compact Dual-Polarized Square Microstrip Antenna

    with Triangular Slots for Wireless Communication, lEE Electron

    ics Letters, 42,16, August 2006, pp. 894-895.

    10. K. Wong and T. Chiou, Design

    of

    Dual Polarized Patch

    Antennas Fed by Hybrid Feeds, Proceedings of the IEEE Fifth

    International Symposium on Antennas, Propagation, and EM The

    ory, Beijing, China, August 2000, pp. 22-25.

    11. Y. Guo and K. Luk, Dual-Polarized Dielectric Resonator,

    IEEE Transactions on Antennas and Propagation, AP-51, 5, May

    2003,pp.1120-1123.

    12. B. Lindmark, S. Lundgren, J. Sanford, and C. Beckman, Dual

    Polarized Array for Signal-Processing Applications in Wireless

    Communications,

    IEEE Transactions on Antennas and Propaga

    tion, AP-46, 6, June 1998, pp. 758-763.

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    13. A Parfitt and N. Nikolic, A Dual-Polarised Wideband Planar

    Array for X-Band Synthetic Aperture Radar, IEEE International

    Symposium on Antennas and Propagation Digest, 2, Boston, MA,

    July 2001, pp. 464-467.

    14. H. Wong, K. Lau, K. Luk, Design

    of

    Dual-Polarized L-Probe

    Patch Antenna Arrays with High Isolation, IEEE Transactions on

    Antennas and Propagation, AP-52, 1, January 2004, pp. 45-52.

    17. C. Balanis, Antenna Theory, Second Edition, New York, John

    Wiley & Sons, Inc., 2002.

    18. J. R. James and P. S. Hall (eds.), Handbook of Microstrip

    Antennas, Volume 1, London, Peter Peregrinus, 1989.

    19. R. Garg, P . Bhartia,

    1.

    Bahl, and A. Itt ipiboon, Microstrip

    Antenna Design Handbook, Norwood, MA, Artech House, Inc.,

    2001.

    15. J . Skora, A. Sanz, and R. Fabbra, Dual Polarized Phased

    Array Antenna for Airborne L-Band SAR, IEEE MTT-S Interna

    tional Conference, Long Beach, CA, July 2005, pp. 192-196.

    16. IE3D, Version 10.2, Zeland Software Inc., Fremont, CA, 2004.

    20 . P. M. Bafrooei and L. Shafai, Characteristics of Single- and

    Double-Layer Microstrip Square-Ring Antennas,

    IEEE Transac

    tions on Antennas and Propagation, AP-47, 10, October 1999, pp.

    1633-1639.

    Introducing the Feature Article Authors

    Texas -A&M University, he conducted research on wireless power

    transmission, power combining, ultra-wideband antennas, and

    phased arrays. In 2007, he joined Intelligent Automation Inc.,

    Rockville, MD, where he is involved in research and development

    of

    advanced antennas and RP/microwave systems, including

    conformal antennas, metamaterial antennas, VAV collision avoid

    ance radar, airborne weather radar, through-the-wall noise radar,

    and RPID sensors for biological-warfare agent detection and struc

    ture health monitoring.

    Kai

    Chang

    received the BSEE degree from the National Tai

    wan University, Taipei, Taiwan; the MS degree from the State

    University

    of

    New York at Stony Brook; and the PhD degree from

    the University of Michigan, Ann Arbor; in 1970, 1972, and 1976,

    respectively.

    From 1972 to 1976, he worked for the Microwave Solid-State

    Circuits Group, Cooley Electronics Laboratory

    of

    the University

    of

    Michigan as a Research Assistant. From 1976 to 1978, he was

    employed by Shared Applicat ions , Inc., Ann Arbor, where he

    worked in computer simulation

    of microwave circuits and micro

    wave tubes . From 1978 to 1981, he worked for the Electron

    Dynamics Division, Hughes Aircraft Company, Torrance, CA,

    Yu-Jiun

    Ren

    received the BSEE from Nat ional Chung

    Hsing University, Taiwan; the MS degree in Communication Engi

    neering from National Chiao-Tung University, Taiwan; and the

    PhD degree from Texas A&M Univers ity at Col lege Stat ion; in

    2000,2002,

    and 2007, respectively. From 2002 to 2003, he was a

    research assistant with the Radio Wave Propagation and Scattering

    Laboratory, National Chiao-Tung University, and involved in

    mobile-radio propagation, channel modeling, and cell planning. At

    Shih-Hsu

    Hsu received the BSEE degree from National

    Cheng-Kung University, Taiwan; the MS degree in Electrical Engi

    neering from the University of Wisconsin-Madison; and the PhD

    degree from Texas A&M University at College Station; in 2000,

    2004, and 2008 , respectively. At Texas A&M University, his

    research activities involved microstrip reflectarrays, reconfigurable

    antennas, and wideband antennas. In October 2008, he joined

    Applied Optoelectronics, Inc., where he is involve in high-speed

    laser design.

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    where he was involved in the research and development of

    millimeter-wave solid-state devices and circuits, power combiners,

    oscillators and transmitters. From 1981 to 1985, he worked for the

    TRW Electronics and Defense, Redondo Beach, CA, as a Section

    Head, developing state-of-the-art millimeter-wave integrated cir

    cuits and subsystems including mixers, VCOs, transmitters,

    amplifiers, modulators, up-converters, switches, multipliers,

    receivers, and transceivers. He joined the Electrical Engineering

    Department

    of

    Texas A&M University in August 1985 as an

    Associate Professor, and was promoted to a Professor in 1988. In

    January 1990, he was appointed Raytheon E-Systems Endowed

    Professor

    of

    Electrical Engineering. His current interests are in

    microwave and millimeter-wave devices and circuits, microwave

    integrated circuits, integrated antennas, wideband and active anten

    nas, phased arrays, microwavepower transmission, andmicrowave

    optical interactions.

    Dr. Chang has authored and coauthored several books. He

    served as the editor of the four-volume Handbook ofMicrowave

    and Optical Components, published by John Wiley in 1989 and

    1990 (second edition 2003), and the editor for the Wiley

    Encyclopedia

    of

    RF and Microwave Engineering (six volumes,

    2005). He is the editor of Microwave and Optical Technology Let

    ters, and the Wiley book series in Microwave and Optical

    Engineering (over 70 books published). He has published over 450

    papers, and many book chapters in the areas of microwave and

    millimeter-wave devices, circuits, and antennas. He has graduated

    over 25 PhD students and over 35MS students.

    Dr. Chang has served as technical committee member and

    session chair for IEEE MTT-S, AP-S, and many international

    conferences. He was the Vice General Chair for the 2002 IEEE

    International Symposium on Antennas and Propagation. He

    received the Special Achievement Award from TRW in 1984, the

    Halliburton Professor Award in 1988, the Distinguished Teaching

    Award in 1989, the Distinguished Research Award in 1992, and

    the TEES Fellow Award in 1996 from the Texas A&M University.

    Dr. Chang is a Fellow of the IEEE.

    78

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