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Phased Array Radars - Past, Present, And Future

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  • 8/9/2019 Phased Array Radars - Past, Present, And Future

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    104

    PHASED

    ARRAY RADARS -PAST, PRESENT AND

    FUTURE

    E.

    BROOKNER

    Raythe on Compan y, U.S.A.,

    ABSTRACT

    This i s a s w e y paper summariz ing the recent

    . developments and h tu re trends in passive, active

    bipolar and Monolithic Microwave Integrated Circuitry

    (MMIC) phased array radars for ground, ship, air, and

    space applications. Covered is the DD(X ) ship radar

    suite; THAAD (formerly GBR); European COBRA;

    Israel BMD radar antennas; Dutch shipboard M A R ;

    airborne US F-22, JSF and F-18 radars, European

    AMSAR, Swedish AESA, Japan

    FSX

    and Israel

    Phalcon; Iridium (66 satellites in orbit for total of 198

    antennas) and Globalstar MM IC spac ebom e active array

    systems (these last two are communications hut the

    technolog y is the same as used by radar systems, in fact

    the IRIDIUM T/R module technology derives from

    .technology developed for a space based radar); Thales

    (formerly Thomson-CSF) 4 inch MMIC wafer 94 GHz

    seeker antenna; digital beamforming; ferroelectric row-

    column scanning; optical electronic scanning for

    communications and radar; the MMIC C-band to Ku-

    band Advadced Shared Aperture Program (ASAP) and

    AMRFS antenna systems

    for

    shared 'use for

    .

    comm unications,~ radar, electronics counterm easures

    (ECM) and ESM; and continuous transverse stub (CTS)

    voltage-variable dielectric (WD) antenna.

    1.0

    h

    DECADES

    Phased arrays have com e a long way in the last three

    decades. This is illustrated by the many tube passive

    arrays and solid-state active arrays, which u se dlscrete

    and MM IC technology, that have been deployed or are

    under development [l-24,

    821;

    see Figures

    1

    through 4

    and Table 1. Figures 1 and 2 are for passive phased

    arrays-the fust generation of phased arrays;Fig. 3

    is

    for active solid state arrays using discrete compo nents;

    Fig. 4is for phased arrays using microwave analog

    integrated circuits, the thud generation. The numb ers in

    parentheses in the figures represent the numbers

    manufactured. Note that in some cases very large

    numbers have been produced, even for MM IC active

    phased arrays. Also one sees that phased arrays are

    being developed around the world. The People's

    Republic of China has come a long way in a very short

    time in the development of phase arrays passive,

    active, over-the-horizon, du al band, wide-ha nd, nltra-

    low-sidelobe, synthetic aperture, adaptive, digital-beam-

    forming, super-resolution and pha se only null steering

    [76].

    The question addressed now is what doe s the

    future hold

    ACCOMPLISHMENTS OVER THE LAST

    2

    Figure I -Ex am ple U.S.A. Passive Phased Arrays Having

    arge

    Production

    " P h a s e d A r ra y s F o r T h e New Millenium" by Eli Brookner which App ear ed in 2000

    IEEE International

    C o n f e r e n c e

    on

    P h a s e d A r r ay S y s t e m s & T e c h n o l o g y P ro c e d d i n g s , M a y 21-25,2000.0 2000

    IEEE

  • 8/9/2019 Phased Array Radars - Past, Present, And Future

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    ..

    \

    105

    Figure 2 -Exam ple Passive Phased Arrays From Around the World

    Figure

    3

    -Exam ple Discrete Active Arrays

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    106

    Figure 4 -Exam ple MMICActive Arrays Deployed and Under Development

    TABLE

    I

    -EXAMPLE RADAR PHASED ARRAYS HAVING LARGE PRODUCTIONS

    Raytheon

    NITPN-25

    X

    824

    14 850

    ANIGPN-22

    X 60 443

    ~

    COBRA DANE

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    2.0 DEVELOPMENT O F MMIC ACTIVE

    PHASED

    ARRAYS

    With the recent prdduction awards for three THAAD

    EDM (Engineering Development Model) radars,

    COBRA radars, SAM PSON radars, F-22 and JSF

    airborne radars, the planned development contracts for

    t he new U S A . D D ( X ) shi p radar suite, and the on going

    development of the Dutch X-band 4-faced APAR radar

    the future looks very good for MMIC phased-array

    radars; seeFigure 4[79,80].

    3.1 Clutter Rejection for

    an

    Airborne System

    (STAP and DPCA)

    To cope with ground clutter and sidelobe jamming for

    an airborne radar, extensive work is ongo ing toward the

    develop men t of airborne phased array using Space-

    Time Adap tive Processing (STAP) 125,261. STAP is a

    general form of Displaced Phase Center Antenna

    (DPCA) processing. STAP had been demonstrated

    several years ago on a modified E2-C system by

    NRL

    [27,

    281. More recently a flight demonstration STAP

    provided

    52

    to

    69 dB

    of sidelobe clutter cancellation

    relative to the mainbeam clutter

    [29].

    This system used

    an

    array m ounted

    on

    the side of an a,ucrafi. The antenna

    had

    11

    degrees

    of

    freedom in azimuth and 2 in elevation

    for a total of 22. Before STAP, the antenna r s

    sidelobe level was -30 dBi, with STAP it was -45 dBi.

    3.2 C- to Ku-band Multi-User Advanced Shared

    Aperture Program (ASAP) MMIC array and

    Dual-Band AMR FS and RECA P Arrays

    The COBR A DA NE radar system of Figure 1 and Table

    1

    has a 16% bandwidth and Rotmari lens mult i-beam

    array systems have a 2.5 to frequen cy bandwidth.

    Technology bad been carried out to develop an active

    MM IC phase-phase steered array that has over a 2 to 1

    frequency bandwidth and at the same time is shared by

    multiple users. Specifically the Nava l Air Weapo ns

    Center (NAWC ) and Texas Instruments (TI, now part of

    Raytheon) were developing a broadban d array having

    continuous

    coverage from C-band through K u-band that

    would share the functions of radar, passive ESM

    (Electronic

    Support

    Measures), active ECM (Electronic

    Counter

    Measures)

    and communications [3 0 ] . To

    achieve this wide bandwidth, a flared notch-radiating

    elemen t was used. Cross notches were used so that

    horizontal, vertical or circular polarization can be

    obtained. They had built a solid state TIR module that

    provides coverage

    over

    this wide band from C-band to

    Ku-band continuously. The module bad a power output

    of

    2

    to 4 W per element over the ban d;.a noise figure

    betwee n .6.5 and 9 dB over the band and power

    efficiency between 5.5 and 10%over the band. A

    IO

    x

    IO-element array having eight active TIR modules was

    built for test purposes. A typical full up array would be

    approximately

    29"

    wide by 13 high. With this type of

    array it. would ultimately be possible to use

    simultaneous part of the array as radar, part of

    he

    array

    for ESM, part of the array for ECM and part of the array

    for communications. The parts used for each function

    would change dynamically depending on the need.

    Also, these parts c ould .be non-o verlappin g or

    overlapping, depending

    on

    the needs. Although

    the

    ASAP funding has ended, the shared aperture

    technology is' being pushed-forward now by the USA

    Office of Naval Research

    (ONR)

    Advanced

    Multifunction Radar Frequency System (AMRFS)

    program [71, 781 and the DARF'A Reco nfigura ble

    Aperture

    Program

    [RECAP] program.

    DERA o f the UK had been developing a dual frequency

    array which would enable a single radar to use L-band

    for search at and X-band fo rtra ck

    so

    as to avoid the use

    of a single comp romise frequ ency for search and track

    [ 52 ] . Consideration

    is

    being given to the use of

    waveguide L-band radiating elements and dipole X

    band elements.

    3.3

    Table

    2

    lists where digital beam forming (DBF) has bee n

    operationally used, some developmental systems that

    have been built, and its significant advantages. The first

    operational radars to use digital beamforming are the

    over-the-horizon (OTH) radars. Specifically the GE

    OTH-B and Raytheon ROTHR (Relocatable OTH

    Radar). The ROTHR receive antenna is ahout

    8,500

    feet

    long.

    More ,recently Signaal used. digital

    beamforming for their deployed 3-D stacked heam

    SMA RT-L and SMA RT-S shipboard radars. The digital

    beamforming is done only on receive. FoFthe SMART-

    L system the antenna consists of 24 rows. The signal

    from each row is down converted and pulse compressed

    with SAW lines and then AiD'd with 12-bit 20 MH z

    Analog Devices AID S. The signal is then modulated

    onto an optical signal and passed down through a fiber

    optic rotary joint to a digital beamformer where 14

    beams are formed [3I].

    Digital Beamforming and

    Its

    Potential

    Table

    2 Digital eamforming

    (DBF)

    .

    OTHRMYTHEON); I -D

    . MART-LAND SMART-S (SIGNAAL);

    I-D STACKED BEAM SYSTEMS

    D W B L O P M N T A L S Y ST E MS

    ROME LAB: 32 COLUMNS,

    32

    INDEPENDENT BEAMS

    MICOM: ARRAY FEED OF6

    ELEMENTS

    BRITISH MESAR: SUBARRAY DBF

    BRLTISX: DBF ON TRANS. AND RTC..

    .

    I ? Er

    ADVANTAGES:

    FLEXLBILTTY:

    -ANTENNA WEIGHTING

    -GROWTH W T H

    TECHNOLOGY .

    .

    ADAPTNE PROCESSEO

    IMPROVED PERFORMANCE

    ULTRA-LOW SIDELOBES

    -DYNAMIC W G E

    J A M M E R A N D C L U I T E R

    SUPPRESSION

    -REDUCED EM1

    MULTIBEAMS

    .__

    LINCOLN LAB. ALLDIGITALUNF

    RECEIV

    R:8BIT3GSPSAC

    . MSAR:

    S m A R R A Y

    DBF

    A

    number of experimental DBF systems have been

    developed; see Table

    2.

    One is the Rome Laboratory

    (Hanscom AFB, MA) 32 column linear array at C-band

    that can form

    32

    independent beams and which uses

    a

    novel self-calibration system

    [32].

    Rome Lab. also bas

    developed a fast digital heamformer that utilizes a

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    108

    systolic processor architecture [77] based on the

    Quadratic Residue Number System (QRNS) [32].

    MICOM (U.

    S.

    Army) built a 64 element feed that used

    DB F for a space fed lens [33].

    The experimental Brit ish MESAR S-band system does

    digital beam formin g at the subarray level [34]. This

    experimental system h as 16 subarrays and a total

    of

    918

    waveguide-radiat ing elements and 156 T R solid state

    modules. Roke Manor Research Ltd. of Britain has

    built an experimental 13 element array using digital

    beamforming on transmit

    as

    well as on receive [35].

    This experimental system uses the Plessey SP2002 chip

    running at a 400 MHz rate as a digital waveform

    generator at every element. Doing digital beamforming

    on m nsm i t a l lows one to put nulls in the direction of an

    ARM

    hreat

    or

    where there is high clutter.

    National Defense Research Establishment of Sweden

    bas buil t an experimental S-band antenna operating

    between 2.8 and 3.3 GHz which does digital

    beamforming using a sampling rate

    of

    25.8

    MHz

    on a

    19.35 MHz IF signal [23]. The advantage of using IF

    frequency sampling rather than baseband sampling is

    that one doesn't have to wony about the imbalance

    between the two channels, that is, the I and Q channels,

    or

    the DC offset. They demonstrated that , by using

    digital beamforming, they could compensate for

    amplitude and phase variat ions that occur from element-

    to-element across angle and across the frequency band.

    Via a calibration, they were able to reduce an element-

    to-element gain variat ion over angle due to mutual

    coupling from

    I dB

    to about

    O.l

    dB. Using

    equalization, they were also able to reduce a i0.5 dB

    variation in the gain over the 5 MHz bandwidth to a less

    than *0.05 d variation. With this calibration and

    'equalization, they were able to demonstrate peak

    sidelobes 47 dB down ov er a

    5 MHz

    bandwidth.

    A

    50

    dB Chebyshev weighting was used. The

    RMS

    of the

    error sidelobes was down

    65dB

    from the peak near

    boresight [63]. They de mon strated that the calibration

    was maintained fairly well over a period of two weeks.

    This work demonstrates the potential advantage offered

    by digital beamforming with respect to obtaining ultra-

    low antenna sidelobes. These results were not achieved

    in real time in the field. The goal for the future is to

    obtain these results in real time in th e field.

    MIT Lincoln Laboratory developed the technology

    for

    an all-digital radar receiver for an airborne surveillance

    array radar like that of the UHF E-2C [43]. They are

    AID

    sampling directly at

    UHF

    ( -430 MHz) us ing a

    Rockwell 8 bit 3 Gigabit per sec

    AID

    running at room

    temperature. Three stages of down conversion are done

    digitally and because the

    AID

    quantization noise is

    filtered the effective number of bits of the

    AID

    is

    increased. For example if the signal bandwidth was

    only, 5

    MHz

    the increase in signal-to-noise ratio is 3

    .GHz/2 (5 MHz) = 25 dB

    so

    the increase in the number

    of effective bits is 25 dB divided by 6 @/bit

    or

    4.2 bits

    to yield 12 bits total. The w hole digital receiver is on an

    8 inch x 8 inch card that uses three 0.6 )m hips. In the

    future these three chips could be replaced by a single

    0.35 Fm CMOS chip.

    The Naval Research Laboratory

    (NU),

    MIT Lincoln

    Laboratory and NSWC are jointly developing an L-band

    active array which has an ID converter at every

    element [64.

    65 , 811.

    Using digital beamforming

    NRL

    demonstrated the ability to obtain a constrained

    beamwidth with frequency while at the same t ime

    achieving low sidelobes over specified angles and

    frequen cy band s [66].

    MIT Lincoln Laboratory had been developing a high-

    performance, low-pow er signal processor to do digital

    beamforming and signal processing for a notional X-

    band Discoverer I1 space-based radar [67,6:3]. This

    notional version of the system did ground moving target

    indication (GMTI) and synthetic aperture radar (SAR)

    mapping. I ts antenna consisted of 12 subarrays and 4

    SLCs. The signal bandwidth was assumed to he 180

    M H z For this system it is necessary to do the signal

    processing on-board

    in

    real time because telemetering

    the

    signal down would require too

    high

    a data rate -35

    Gbps if a 12 bit A D is assumed, well beyond the

    present state-of-the-&.The on-board signal processor

    must do digital beamforming, pulse compression,

    doppler processing, STAF' and SLC. To do this on-

    board in real time requires a signal processor capable

    of

    1100 G O P S (1.1 TERAOP). Lincoln Laboratory has

    shown that it is feasible to do the processing on board

    using a systolic array type architecture having volume