MS_3장 CW and Pulse Radar

34
Prof. Y Kwag@ RSP Lab Korea Aerospace Univ. Chapter 3 Continuous Wave and Pulsed Radars

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cw and pulse radr

Transcript of MS_3장 CW and Pulse Radar

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    Chapter 3

    Continuous Wave and Pulsed Radars

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.1. Functional Block Diagram

    < CW radar block diagram >

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    Narrow Band Filters (NBF)

    : bandwidth Doppler measurement accuracy , noise power

    In practical, operating bandwidth of CW Radar is finite bandwidth

    NBF bank (Doppler filter bank) is implemented using an FFT of size NFFT

    - individual NBF bandwidth (FFT bin)

    effective radar Doppler bandwidth

    Single frequency CW radar cannot measure target range

    - in order to measure target range

    transmit and receive waveforms must have some sort of timing marks

    - timing mark : implemented by modulating the transmit waveform

    commonly technique Linear Frequency Modulation (LFM)

    3.1. Functional Block Diagram

    f

    2/fNFFT

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    : loss term associated with the type of window (weighting)

    3.2. CW Radar Equation

    - Dwell interval : determine frequency resolution or bandwidth of the individual NBFs

    DwellTf /1

    fBNFFT /2

    BNT FFTDwell 2/

    FLkTRGTP

    SNRe

    iav

    43

    22

    4

    avP

    winertDwellcw

    FLLkTR

    GGTPSNR

    43

    2

    4

    CWP iT DwellT

    winL

    (3.1)

    (3.2)

    (3.3)

    (3.4)

    (3.5)

    - NBF bank size

    - for (1), (2)

    - CW radar equation : derived from high PRF Radar equation high PRF Radar equation

    - (CW average transmitted power over the dwell interval),

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.3 Frequency Modulation

    General formula for an FM waveform

    t

    mf duufktfAts0

    0 2cos2cos)(

    : carrier frequency, : modulating signal

    A : constant, : peak freq. deviation

    0f tfm2cos

    peakf fk 2 peakf

    (3.6)

    tftfduufftft m

    t

    mpeak 2sin22cos22)( 00

    0 (3.7)

    m

    peak

    f

    f (3.8)

    - FM modulation index

    - Phase

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.3 Frequency Modulation

    Received radar signal

    )(2sin)(2cos)( 0 ttfttfAts mrr (3.9)

    - Time Delay

    c

    Rt

    2 (3.10)

    Phase detector : extract target range from the instantaneous frequency

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.3 Frequency Modulation

    FM waveform

    tftfAts m 2sin2cos)( 0 (3.11)

    tfsin2jtfj2 m0 eeReAs(t) (3.12)

    - Using the complex exponential Fourier series (F.S)

    n

    tfjn

    n

    tfj mm eCe22sin (3.13)

    (3.14)

    - F.S coefficient

    dtee

    Ctfjntfj

    nmm

    22sin

    2

    1

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.3 Frequency Modulation

    - Bessel function of the first kind of order n,

    due

    J nuujn

    )sin(2

    1)(

    tfu m2

    (3.15)

    (3.16)),(nn JC

    n

    tfjn

    n

    tfj mm eJe22sin

    )(

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.3 Frequency Modulation

    - Total power in the signal s(t)

    (3.17)

    (3.18)

    2

    2

    2

    2

    1)(

    2

    1AJAP

    n

    n

    - Substituting Eq.(3.16) into Eq.(3.12)

    tfjn2

    n

    n

    tfj2 m0 eJeReAs(t) )(

    (3.19)

    - Expanding Eq.(3.18)

    n

    mn tfnfJAts )22cos()()( 0

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.3 Frequency Modulation

    - Since for n Odd & for n Even)()( nn JJ )()( nn JJ

    }..........

    ])cos()[cos()(

    ])cos()[cos()(

    ])cos()[cos()(

    ])cos()[cos()(

    )({

    4

    3

    2

    1

    0

    tf8f2tf8f2J

    tf6f2tf6f2J

    tf4f2tf4f2J

    tf2f2tf2f2J

    eJAs(t)

    m0m0

    m0m0

    m0m0

    m0m0

    tfjn2 0

    (3.20)

    - The spectrum of s(t)

    Amplitude of the central spectral line

    -

    Amplitude of the nth spectral line

    -

    ),(0 AJ

    ),(nAJ

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.3 Frequency Modulation

    For small , the Bessel functions can be approximated by

    mfB )1(2 (3.21)

    (3.22)

    - When is small, and : significant value)(0 J )(1 J

    ]})cos()[cos()(

    2cos)({

    1

    00

    tf2f2tf2f2J

    tfJAs(t)

    m0m0

    1)(0 J 21

    )(1 J

    - Bandwidth can be approximated using Carsons rule

    (3.23), (3.24)

    ]})cos()[cos(2

    1

    2{cos 0

    tf2f2tf2f2

    tfAs(t)

    m0m0

    (3.25)

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    Example 3.1 & 3.2

    If the modulation index is = 0.5, give an expression for the signal s(t).

    - Solution: 9385.0)5.0(0 J 2423.0)5.0(1 J

    ]})cos()[cos()2423.0(

    2cos)9385.0{( 0

    tf2f2tf2f2

    tfAs(t)

    m0m0

    Prob.3.2 ))(2000cos(100 tts(t) Output signal:Frequency deviation : 4Hz

    Modulating waveform : tx(t) 6cos10

    How many spectral lines will pass through a band pass filter whose

    bandwidth is 58Hz centered at 1000Hz?

    - Solution: Hzf peak 40104

    58

    40

    m

    peak

    f

    f

    HzfB m 968)15(2)1(2

    Prob.3.1

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.4 Linear FM (LFM) CW Radar

    LFM CW radar range & Doppler information

    Fig 3.5. Transmitted and received triangular LFM signals and beat frequency for stationary

    target

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.4 Linear FM (LFM) CW Radar

    (3.26)- Modulating frequency

    021tm

    f

    - Rate of frequency change(3.27)

    - Beat frequency

    fff mff

    t

    f

    m 2

    )0 2/1(

    fftfcR

    b 2

    (3.28)

    Eq.(3.28) rewritebR

    c ff2

    (3.29)

    (3.30)c

    fRff mb

    4

    When Doppler is present.

    dtransmittereceivedb fff (3.31)

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.4 Linear FM (LFM) CW Radar

    Fig 3.6. Transmitted and received LFM signals and beat frequency, for a moving

    target.

    Positive slope Doppler shift term subtracts from the beat frequency

    Negative slope the two terms add up

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.4 Linear FM (LFM) CW Radar

    -Beat frequency during positive slope fbu

    -Beat frequency during negative slope fbd

    Rf

    c

    Rfbu

    22

    Rf

    c

    Rfbd

    22

    (3.32)

    (3.33)

    Range )(4

    bdbu fff

    cR

    (3.34)

    (3.35)

    Range rate )(4

    bubd ffR

    -Maximum time delay 0max 1.0 tt (3.36)

    (3.37)-Maximum range

    mfctcR

    41.0

    2

    1.0

    max0

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.5 Multiple Frequency CW Radar

    Multiple frequency scheme (CW radar)

    - very adequate range measurement, without using frequency modulation

    -Waveform : tfAs(t) 02sin

    )2sin( 0 tfA(t)s rr-Received signal :

    (3.38)

    (3.39)

    -phase : cRf 202 (3.40)

    -Solving for R

    44 0

    f

    cR (3.41)

    Maximum unambiguous range occurs when is maximum.

    R is limited to impractical small values.

    2

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.5 Multiple Frequency CW Radar

    Two CW signals

    tfA(t)s 111 2sin

    tfA(t)s 222 2sin

    (3.42)

    (3.43)

    Received signals from moving target

    )2sin( 1111 tfA(t)s rr

    )2sin( 2222 tfA(t)s rr

    (3.44)

    (3.45)

    Phase difference between the two received signals

    fc

    Rff

    c

    R

    4)(

    41212

    (3.46)

    f

    cR

    2(3.47)

    Maximum unambiguous range 2

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.6 Pulsed Radar

    Pulsed Radar

    - Transmit & receive a train of modulated pulsed.

    - Two way time delay between a Transmitted and Received pulse

    extract range information.

    - If accurate range measurements are available between consecutive pulses

    Doppler frequency extracted from the range rate

    Defined the pulsed radar waveform

    carrier frequency : depend on the design requirements and radar mission.

    pulse width : related to the BW and defines the range resolution.

    modulation : difference modulation techniques are usually utilized to

    enhance the radar performance.

    PRF : must be chosen to avoid Doppler and range ambiguities.

    tRR

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    PRF Classification & Agility

    Radar system employ low, medium, and high PRF schemes.

    Low PRF : accurate, long, unambiguous range measurements,

    but, severe Doppler ambiguities.

    Medium PRF : must resolve both range and Doppler ambiguities. but, provide

    adequate average transmitted power as compare to low PRFs.

    High PRF : superior average transmitted power and excellent clutter rejection

    capability. but, extremely ambiguous range

    - Radar system utilizing high PRFs are often called Pulsed Doppler Radar (PDR)

    - Moving Target Indicator (MTI) radar use the PRF agility known as PRF staggering

    PRF agility use to avoid blind speed

    use to avoid range and Doppler ambiguities

    use to prevent jammers from locking onto the radars PRF PRF jitter

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    Pulsed Radar Block Diagram

    range gate : implemented as filters that open and

    close at time intervals

    that correspond to the

    detection range.

    NBF bank : implemented using an FFT, individual filter

    BW = FFT freq.

    resolution

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.7 Range and Doppler Ambiguities

    Range and Doppler Ambiguities

    Fig 3.8. Spectra of transmitted and received wavwforms and Doppler bank.

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.7 Range and Doppler Ambiguities

    Range and Doppler Ambiguities

    - Range ambiguous : Second pulse is transmitted prior to the return of the first pulse.

    - Radars operational requirements radar PRF chose.

    ex. long-range search(surveillance) low-PRF

    - Line spectrum of a train of pulses has sinx/x envelope Line spectra are separated by the PRF(fr).

    - The Doppler filter bank is capable or resolving target Doppler as long as the anticipated Doppler

    shift is less than one half the bandwidth of the individual filters

    )48.3(2

    2 maxmaxr

    dr

    vff

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    Multiple PRF

    Doppler ambiguous;

    If the target Doppler freq. is high enough to make an adjacent spectral line

    move inside the Doppler band of interest.

    Detecting high speed target Require high PRF

    Detecting the high speed target by using long range radar

    range and Doppler ambiguous.

    resolving by using multiple PRFs.

    Multiple PRF schemes;

    incorporated sequentially within each dwell interval (scan or integration frame)

    use a single PRF in one scan and resolve ambiguity in the next.

    may have problems due to changing target dynamics from

    one scan to the next.

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    Resolving Range Ambiguity

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.8 Resolving Range Ambiguity

    Resolving Range Ambiguity

    - Radar uses two PRFs and , to resolve range ambiguity

    - Desired PRF that corresponds to as

    - One choice is to select and for some integer

    - Within one period of the desired PRI( ) the two PRFs and coincide

    only at one location true unambiguous range.

    - M1(M2) : number of PRF1(PRF2) intervals between transmit of a pulse and receipt

    of the true target return.

    - Over the interval 0 to , the only possible result are M1=M2=M or M1+1=M2.

    - Time delay t1 and t2 correspond to the time between the transmit of a pulse on

    each PRF and receipt of a target return due to the same pulse.

    )( 11 ur Rf )( 22 ur Rf

    )(, 21 rangesunambiguouradardesiredRRR uuu

    uR rdf

    rdr Nff 1 rdr fNf )1(2 N

    rdd fT 1 1rf 2rf

    dT

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    Resolving Range Ambiguity

    )52.3(2

    israngetargettrue

    )51.3(

    islocationtargettruethetotimetripround

    1,1

    )50.3(

    )49.3(

    :Icase.1

    22

    11

    22

    11

    21

    12

    2

    2

    1

    1

    21

    r

    r

    r

    rr

    rr

    ctR

    tMTt

    tMTt

    fT

    fTwhere

    TT

    ttM

    f

    Mt

    f

    Mt

    tt

    )56.3(2

    israngetargettrue

    )55.3(

    islocationtargettruethetotimetripround

    1,1

    )54.3()(

    )53.3(1

    :IIcase.2

    1

    111

    22

    11

    21

    212

    2

    2

    1

    1

    21

    r

    r

    rr

    rr

    ctR

    tMTt

    fT

    fTwhere

    TT

    TttM

    f

    Mt

    f

    Mt

    tt

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    Resolving Range Ambiguity

    )58.3(2

    israngetargettrue

    )57.3(

    ambiguityfirsttheinistargetThe

    :IIIcase.3

    2

    212

    21

    r

    r

    ctR

    ttt

    tt

    - Blind range : pulse cannot be received while the following pulse is being

    transmitted, these time correspond to blind range.

    resolved by using a thired PRF

    rdr

    rdr

    rdr

    fNNf

    fNNf

    fNNf

    )2)(1(

    )2(

    )1(

    3

    2

    1

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    3.9 Resolving Doppler Resolution

    Resolving Doppler Ambiguity

    -The Doppler ambiguity problem is analogous to that of range ambiguity.

    same methodology can be used to resolve Doppler ambiguity.

    - Measure the Doppler frequency and instead of and .1df 2df 1t 2t

    )62.3(

    :.3

    )61.3(

    )60.3(

    :.2

    )59.3()(

    :.1

    21

    21

    2211

    21

    12

    21

    21

    212

    21

    ddd

    dd

    drddrd

    rr

    dd

    dd

    rr

    rdd

    dd

    fff

    ffIIIcase

    fMfforfMff

    isDopplertrueand

    ff

    ffM

    ffIIcase

    ff

    fffM

    ffIcase

    - Blind Doppler can occur can be resolved using a third PRF.

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    Example 3.3

    kmf

    cR

    kmf

    cR

    kHzfNf

    kHzNff

    kHzR

    cf

    fPRF

    r

    u

    r

    u

    rdr

    rdr

    u

    rd

    rd

    667.110902

    103

    2

    695.1105.882

    103

    2

    90)1500)(159()1(

    5.88)1500)(59(

    thatfollowsIt

    5.110200

    103

    2

    ,desired,first:solution*

    3

    8

    2

    2

    3

    8

    1

    1

    2

    1

    3

    8

    .,,,f compute .59 Choose . 100 is range sunambiguou

    desired The s.ambiguitie range resolve to PRFs two usesradar certain A

    212r1 uuru RandRf NkmR

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    Example 3.4 (1)

    PRF.eachfor17and2

    8atappearingtargetanotherforfreq.)(Doppler Calculate . 550m/s isvelocity

    whose target afor PRFeach ofposition frequency theCalculate .9 Assume

    21 and 1815 PRFs; h threeradar wit aConsider

    0

    321

    kHz,kHz

    ,kHzf

    GHzf

    kHz.fkHz,kHz, ff

    d

    rrr

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    Example 3.4 (1)

    3321

    3318

    3315

    321where Eq.(3.61) using

    33103

    10955022f

    is frequency Doppler : *

    33333

    22222

    11111

    8

    9

    0d

    ddr

    ddr

    ddr

    ddirii

    fnffn

    fnffn

    fnffn

    ,,ifffn

    kHzc

    vf

    solution

    .12and152 are freq.Doppler apparentThus,

    .11way samevalue.acceptable:32Choose

    .sincevalueacceptablenot:18and331and0 Choose

    321

    3211

    1111

    kHzf,khzfkHz,f

    n,nkHzfn

    ffkHzkHz,f,n

    ddd

    d

    rdd

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    Example 3.4 (2)

    1721

    218

    815

    Eq.(3.61) using.problemtheofpartSecond

    3333

    2222

    1111

    nfffn

    nfffn

    nfffn

    ddr

    ddr

    ddr

    0 1 2 3 4

    8 23 38 53 68

    2 20 38 56

    17 38 39

    n

    1from rd ff

    2from rd ff

    3from rd ff

    smv

    kHzfnnn

    r

    d

    /7.6232

    0333.038000

    38isDopplertargettruetheand1and,2,Thus 321

    isrelationsthreeabovethesatisfythatintegersSmallest 321 n,n,n

  • Prof. Y Kwag@ RSP LabKorea Aerospace Univ.

    range_calc.m

    3.10. MATLAB program range_calc.m

    - The program range_calc.m solves the radar range equation of the form

    )63.3()()4(

    4

    1

    0

    3

    2

    SNRLFTk

    GGTfPR

    e

    rtirt

    Peak transmitted power Boltzmans constant

    Pulse width Effective noise figure

    PRF System noise figure

    Transmitting antenna gain Total system losses

    Receiving antenna gain Dwell interval (time on target)

    Wavelength Minimum SNR required for detection

    Target cross section

    tP

    rf

    tG

    rG

    k

    eT

    F

    L

    iT

    0)(SNR

    - This equation applies for both CW and pulsed radar.

    - In the case of CW radars, the terms must be replaced by the average CW

    power .

    rt fP

    CWP