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Cours sur les principes de radar

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  • Bullock Engineering Research Copyright 2014

    1

    Introduction to RADAR

    Webinar By

    Scott R. Bullock of

    Besser Associates, Inc.

    Sponsored by:

  • Eastern OptX Background

    Test Solutions for:

    Radar Systems

    Transponders

    Altimeters

    FMCW

    LPI

    Digital Radios

  • Propagation Path Replicators

  • Phase Noise Test Systems

  • Service and Calibration

  • Bullock Engineering Research Copyright 2014

    6

    Introduction to RADAR

    Webinar By Scott R. Bullock of Besser Associates, Inc.

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

    7

    Scott R. Bullock [email protected]

    BSEE BYU, MSEE U of U, PE, 18 US Patents, 22 Trade Secrets

    Books & Publications

    Transceiver and System Design for Digital Communications, 4th edition

    http://iet.styluspub.com/Books/BookDetail.aspx?productID=395134

    http://www.theiet.org/resources/books/telecom/tsddcfe.cfm

    Broadband Communications and Home Networking

    http://sci.styluspub.com/Books/BookDetail.aspx?productID=369239

    http://digital-library.theiet.org/content/books/te/sbte002e

    Multiple Articles in Microwaves & RF, MSN

    Seminars - Raytheon, L-3, Thales, MKS/ENI, CIA, Titan, Phonex, NGC, Others

    Courses for Besser Associates

    Introduction to RADAR - http://www.besserassociates.com/outlinesOnly.asp?CTID=253

    Introduction to Wireless Communications Systems - http://www.bessercourse.com/outlinesOnly.asp?CTID=235

    Transceiver and Systems Design for Digital Communications - http://www.bessercourse.com/outlinesOnly.asp?CTID=208

    Cognitive Radios, Networks, and Systems for Digital Communications - http://www.bessercourse.com/outlinesOnly.asp?CTID=251

    College Instructor

    Graduate Presentation on Multiple Access to Polytechnic, Farmingdale//Brooklyn, NY

    Advanced Communications, ITT

    Engineering 201E, PIMA

    Key Designs

    Radar Simulator for NWS China Lake Acquisition, Target Tracking, Missile Tracking, MTI

    Navys IntegratedTopside INTOP Integrate Radar with EW, EA, Comms

    Radar Comms using CP-PSK Modulated Pulses for the SPY-3 Radar and PCM/PPM

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    RAdio Detecting And Ranging

    RADAR

    RADAR is a method of using electromagnetic waves to

    determine the position (range and direction), velocity

    and identifying characteristics of targets.

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Radar Applications

    Military Search and Detection

    Targeting and Target Tracking

    Missile Guidance

    Fire Control Acquisition, Track

    Airborne Intercept

    Ground and Battle field Surveillance

    Air Mapping Systems

    Submarine and Sub-Chasers

    Commercial Weather, Navigation, Air Traffic Control

    Space and Range

    Road and Speeding

    Biological Research Bird and Insect Surveillance and Tracking

    Medical diagnosis, organ movements, water condensation in the lungs, monitor heart rate and pulmonary motion, range(distance), remote sensor of heart and respiration

    rates without electrodes, patient movement and falls in the home

    Miniature Seeing aids, early warning collision detection and situational awareness

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Two Basic Radar Types

    Pulse Radar

    Transmits a pulse stream with a low duty cycle

    Receives pulse returns from targets during the time off or dead time between pulses

    Continuous Wave Radar

    Sends out a continuous wave signal and receives a Doppler frequency for moving targets

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    Pulse Vs. Continuous Wave

    Pulse Radar

    Single Antenna

    Determines Range & Altitude

    Susceptible To Jamming

    Physical Range Determined

    By Pulse Width PW and Pulse

    Repetition Frequency PRF

    Low average power

    Time synchronization

    Continuous Wave Radar

    Based on Doppler

    Requires 2 Antennas

    No Range or Altitude Information

    High SNR

    More Difficult to Jam But Easily

    Deceived

    Simpler to operate, timing not

    required

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Pulsed Radar

    Most radar systems are pulsed

    Transmit a pulse and then listen for received signals, or echoes

    Avoids problem of a sensitive receiver simultaneously operating

    with a high power transmitter.

    Transmits low duty cycle, short duration high-power RF- pulses

    Time synchronization between the transmitter and receiver of a

    radar set is required for range measurement.

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Pulse Radar Modulation

    100% Amplitude Modulation AM

    ON/OFF keying

    Turn on/off a Carrier Oscillator

    Pulse width is how long the carrier is on

    Pulse Repetition Frequency is how fast the

    carrier is turned on

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    Radar Turns on/off the

    Carrier Frequency

    Pulse Width = 1us

    Time between pulses = PRI = 7us = 1/PRF = 143 kHz

    V

    t

    Burst of Carrier Frequency Radar burst Low duty cycle, high power Duty cycle = time on/time off * 100 a percentage Above example approx. 1/6 * 100 = 16%

    carrier wave = 4MHz

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    Radar Burst of Frequency

    Pulse Modulated On/Off Keying t

    V

    Oscillator

    Modulator

    On/Off Switch

    Continuous Waveform - CW

    Pulse Train: PRF

    Radar Pulses

    V

    t PW

    PRI = PRT

    PRF = 1/PRI

    t

    V

    PW

    PRI = PRT

    PRF = 1/PRI

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Pulse Characteristics

    Pulses are repeated at the Pulse Repetition Frequency or PRF

    PRF is the number of pulses per second

    Pulse Repetition Indicator PRI is the time between pulses

    Pulse Repetition Time PRT is the same as PRI

    PRT = PRI = 1/PRF

    PRF determines the radars maximum detection range

    Pulse Width PW - amount of time that the radar is transmitting

    Pulse Width (PW) determines the minimum range resolution

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Pulse Distortion

    P1

    PRI = 1/PRF Long P1 returns cause

    distortion to P2 returns

    t

    V

    Long returns from P1 causes distortion to the returns of P2

    P2

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Basic RADAR

    Transmit Radar Pulse

    Radar Directional Antenna

    Target

    Reflection

    off a Target

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    Basic Radar Diagram

    Transmitter Reflective

    Radar

    Surface

    Transmit

    Channel

    Low Noise

    Receiver

    Receive

    Channel

    RADAR

    TARGET

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Radar Path Budget

    Tracks Signal & Noise Levels from Radar to Target back to Radar Power Out (PA), Tx Losses, Channel Losses, Target Reflectivity,

    Channel Losses, Rx Losses, Rx Detect S/N

    Required S/N

    Radar Budget - Allocation of Power and Noise

    Radar Tx PA to Radar Rx Detector (LNA)

    Used in Solving Tradeoffs

    Size, cost, range

    Radar pulses are reflected off targets that are in the transmission path Targets scatter electromagnetic energy

    Some of the energy is scattered back toward the radar.

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    Effective Isotropic Radiated

    Power EIRP

    EIRP = Effective Isotropic Radiated

    Power = RF Power * Antenna Gain

    RF

    Power

    Gain

    RF

    Power

    Target

    Target

    ERP = Effective Radiated Power

    EIRP = ERP + Gdipole (2.14dB)

    ERP = EIRP - Gdipole (2.14dB)

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    Sun

    Focusing

    Sun Rays

    To Increase

    Power

    Focusing Radio Waves

    To Increase

    Power

    Magnifying

    Glass

    Directional Antenna

    Receiver

    Focusing Increases Power To

    Provide Gain

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Radar Cross Section RCS

    RCS () - size and ability of a target to reflect radar energy m s = Projected cross section * Reflectivity * Directivity

    The target radar cross sectional area depends on:

    Airplanes physical geometry and exterior features

    Direction of the illuminating radar

    Transmitted frequency,

    Material types of the reflecting surface.

    Difficult to estimate

    Equals the targets cross-sectional area theoretically

    Not all reflected energy is distributed in all directions

    Some energy is absorbed

    Usually measured for accurate results

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Radar RCS Patterns

    Sphere s = pr2

    Flat Plate s = 4pw2h2/l2

    Corner Reflector s = 8pw2h2/l2

    Similar to

    Antenna

    Gains

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    Radar Transmitter

    Power to Target

    Freespace

    Attenuation

    Water

    Vapor

    Rain

    Loss

    Oxygen

    Absorption

    Multipath

    Loss

    EIRP

    Afs = l2/(4pR)2 LAtmos Lmulti

    Transmitter

    Reflector

    Target Pt

    Gt

    Power at Target = Ptarg(i) = PtGtAfs= PtGt l2

    (4pR)2

    Power at Target = Ptarg = PtGtAfs = PtGt l2

    Includes other losses Lt (4pR)2 Lt

    Lt = LAtmos * Lmulti

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    Radar Received

    Power from Target

    Afs = l2/(4pR)2

    LAtmos Lmulti

    Freespace

    Attenuation Water

    Vapor

    Rain

    Loss

    Oxygen

    Absorption

    Multipath

    Loss

    Receiver

    Reflector

    Target

    Gtarg= 4ps/l2

    s = RCS

    Gr

    Pr

    Ptarg

    Lt = LAtmos * Lmulti

    Ptarg(i) 4ps l2 Gr

    l2 (4pR)2 Power received at Radar (ideal) = Pr(i) = Ptarg(i)Gtarg AfsGr =

    Ptarg 4ps l2 Gr

    l2 (4pR)2 Lt

    Power at Radar = Pr= PtargGtarg AfsGr =

    (Includes losses) Lt

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    Radar Antenna Gain and

    Channel Losses

    Freespace

    Attenuation

    Water

    Vapor

    Rain

    Loss

    Oxygen

    Absorption

    Multipath

    Loss

    EIRP

    Afs = l2/(4pR)2 LAtmos Lmulti

    Transmitter

    Receiver

    Reflector

    Target

    Duplexer

    Gtarg= 4ps/l2

    s = RCS

    Pt Gt l2 4ps l2 Gr =

    (4pR)2 l2 (4pR)2

    Pt

    Pr

    Power at Target (Ideal) = Ptarg(i) = PtGtAfs= PtGt (l2/(4pR)2)

    Power at Radar (Ideal) = Pr(i) = Ptarg(i)Gtarg AfsGr =

    Pr =

    One-way Loss: Lt = LAtmos * Lmulti Two-way Losses = Lt * Lt = Lt

    2 = Ls

    Including other losses in the path

    Assume Antenna Gain Gt = Gr

    PtGtGrl2s

    (4p)3R4

    PtG2l2s

    (4p)3R4Ls

    PtGtGrsc02

    (4p)3f2R4 =

    PtG2sc0

    2

    (4p)3f2R4Ls

    =

    Lt = LAtmos * Lmulti

    Afs = l2/(4pR)2

    LAtmos Lmulti

    Freespace

    Attenuation Water

    Vapor

    Rain

    Loss

    Oxygen

    Absorption

    Multipath

    Loss

    Lt = LAtmos * Lmulti Gr

    Gt

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    Radar Example

    Power at Target = Ptarg = PtGtAfs= PtGt (l2/(4pR)2)

    Pr =

    PtG2l2s

    (4p)3R4Ls

    PtG2sc0

    2

    (4p)3f2R4Ls

    = Given: What is Pr in dBm?

    f = 2.4 GHz, , l = .125

    Pt = 100W

    R = 1000m

    Gt = Gr = 1000

    Total 2-way loss Ls = 10

    s= 140 m2

    100(1000)2(.125)2(140)

    (4p)3 (1000)4(10) Pr =

    =1.10235*10-8W = 1.10235*10-5mW

    Prdbm = 10log(1.10235*10-5) = -49.6 dBm

    Freespace

    Attenuation

    Water

    Vapor

    Rain

    Loss

    Oxygen

    Absorption

    Multipath

    Loss

    EIRP

    Afs = l2/(4pR)2 LAtmos Lmulti

    Transmitter

    Receiver

    Reflector

    Target

    Duplexer

    Gtarg= 4ps/l2

    s = RCS

    Gr

    Pt

    Pr

    Gt

    Lt = LAtmos * Lmulti

    Afs = l2/(4pR)2

    LAtmos Lmulti

    Freespace

    Attenuation Water

    Vapor

    Rain

    Loss

    Oxygen

    Absorption

    Multipath

    Loss

    Lt = LAtmos * Lmulti

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Free Space Attenuation

    Forms of free-space attenuation depends on how it is used

    Afs = (l/(4pR))2 will be less than 1 and multiplied

    Afs = ((4pR)/l)2 will be greated than 1 and divided

    Afs = 20log l/(4pR) = will be a negative number and added

    Afs = 20log (4pR)/l = will be a positive number and subtracted

    Important to determine if it is added or subtracted to avoid mistakes

    Given:

    Pt = 100W = 50dBm, l = .125, R = 1000m

    Afs = (l/(4pR))2 = 98.9 x 10-12 need to multiply: Pr = 100W * 98.9 x 10-12 = 9.89 x 10-9

    Afs = ((4pR)/l)2 = 1.01065 x 1010 need to divide: Pr = 100W/(1.01065 x 1010)= 9.89 x 10-9

    Afs = 20log l/(4pR) = -100 dB need to sum: Pr = 50dBm + (-100dB) = -50dBm

    Afs = 20log (4pR)/l = 100 dB need to subtract: Pr = 50dBm - 100dB) = -50dBm

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Two-Way Radar Losses

    Two-way free space loss used twice Once for the radar transmitter to target path

    Once for the target to radar receiver path

    Free Space Loss 2*Afs = 2* 20log l/(4pR)

    Two-way Losses in Radar in dB Atmospheric loss 2* Latmos

    Multipath loss 2* Lmult T/R switch or Circulator loss 2* Ltr

    Antenna loss, Polarization, Mis-pointing, Radome 2* Lant

    Implementation loss 2*Li

    Losses in dB:

    Ltotal = 2* Latmos + 2* Lmult + 2* Ltr + 2* Lant + 2* Li

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    RADAR Equation

    to Assess Radar Performance

    P r = Radar received power

    P t = Radar transmitted power

    G t = Transmitter antenna gain

    G r = Receiver antenna gain

    G2 = Gr Gt assumes the same antenna at the radar l = wavelength

    R = slant range

    Ls = total two-way additional losses

    s = radar cross section of the target RCS

    Log Form

    Pr = PtG tG r Afs AfsGtarg1/Ls

    10logPr = 10logPt + 10logG + 10logG + 10logAfs + 10logAfs + 10logGtarget - 10log(Ls)

    Pr dBm = Pt dBm + 2GdB + 2Afs dB + Gtarget dB Ls dB

    Pr = PtG2l2s

    (4p)3R4Ls

    P(mW) = dBm or P(W) = dBw

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    Radar Example dB

    Power at Target = Ptarg = PtGtAfs= PtGt (l2/(4pR)2)

    AfsdB = 10log(l2/(4pR)2) = 20log(l/(4pR) = 20log[(.125)/(4p1000)] = -100.05dB

    Gtarg = 10log(4ps/l2) = 10log(4p*140/.1252) = 50.5dB

    PtG2l2s

    (4p)3R4Ls

    PtG2sc0

    2

    (4p)3f2R4Ls

    =

    Given: What is Pr?

    f = 2.4 GHz, , l = .125

    Pt = 100W = 50dBm

    R = 1000m

    Gt = Gr = 1000 = 30dB

    Total 2-way loss Ls = 10 = 10dB

    s= 140 m2 Pr dBm = Pt dBm + 2GdB + 2Afs dB + Gtarget dB Ls dB

    Pr dBm = 50dBm + 2*30dB + 2*-100.05 dB + 50.5 dB 10dB = -49.6dBm

    Freespace

    Attenuation

    Water

    Vapor

    Rain

    Loss

    Oxygen

    Absorption

    Multipath

    Loss

    EIRP

    Afs = l2/(4pR)2 LAtmos Lmulti

    Transmitter

    Receiver

    Reflector

    Target

    Duplexer

    Gtarg= 4ps/l2

    s = RCS

    Gr

    Pt

    Pr

    Gt

    Lt = LAtmos * Lmulti

    Afs = l2/(4pR)2

    LAtmos Lmulti

    Freespace

    Attenuation Water

    Vapor

    Rain

    Loss

    Oxygen

    Absorption

    Multipath

    Loss

    Lt = LAtmos * Lmulti

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Range Determination

    Range calculation uses time delay between objects Time delay is measured from source to reflector and back

    Time delay divided by two to calculate one way range

    Sound-wave reflection Shout in direction of a sound-reflecting object and hear the echo

    Calculate two-way distance using speed of sound 1125 ft/sec in air

    Measure two way delay of 5 seconds

    Range = 1125ft/sec x 5/2 = 2812ft

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    Sound Wave Reflection

    Hi

    Hi

    Determine the distance using range formula

    Listen to multiple echoes off difference distances

    Best echo effects when the yell is short short pulse width

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    Sound Wave Reflection

    Hi

    Hi

    Determine the distance using range formula

    Listen to multiple echoes off difference distances

    Best echo effects when the yell is short short pulse width

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Radar Range Calculation

    Radar uses electromagnetic energy pulses

    Pulse travel at the speed of light C0

    Reflects off of a surface and returns an echo back to the radar

    Calculates the two-way distance or slant range

    Slant range = line-of-sight distance from radar to target

    Takes in account the angle from the earth

    Ground range = horizontal distance from radar to target

    Slant range calculated using ground range and elevation

    Radar energy to the target drops proportional to range squared.

    Reflected energy to the radar drops by a factor of range squared

    Received power drops with the fourth power of the range Need very large dynamic ranges in the receive signal processing

    Need to detect very small signals in the presence of large interfering

    signals

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    Slant Range

    Slant Range = Rslant

    Radar

    Directional

    Antenna

    Target

    Ground Range = Rgnd

    Elevation = EL

    Rslant2 = Rgnd

    2 + EL2: Rslant = (Rgnd2 + EL2)1/2

    Sinf = El/Rslant: Rslant = El/sinf

    Cosf = Rgnd/Rslant: Rgnd = Rslant*cosf

    f Given:

    Elevation = 5000 ft

    Angle = 300

    Calculate Slant Range =

    Rslant = El/sinf = 5000/sin(30) = 10,000 ft

    What is the Ground Range =

    Rgnd = Rslant*cosf = 10,000*cos(30) = 8660.25 ft

    Rslant2 = Rgnd

    2 + EL2: Rgnd = (Rslant

    2 - EL2) 1/2 = (10,0002 - 50002) 1/2 = 8660.25ft

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    Range Calculation

    Electromagnetic energy pulse travels at the speed of light C0

    R = (tdelay * C0)/2

    R = slant range

    tdelay = two way time delay Radar-Target-Radar C0 = speed of light = 3*10

    8 m/s

    Given:

    tdelay = 1ms

    C0 = 3x108 m/sec

    Calculate Slant Range =

    R = (1ms * 3*108 m/s)/2 = 150km

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    Radar Range Equation

    Rmax = PtGtGrl2s 1/4 = PtGtGrsc0

    2 1/4

    (4p)3SminLs (4p)3f2SminLs

    Double the range requires 16 times

    more transmit power Pt

    Radar detection range = the maximum range at which a

    Target has a high probability of being detected by the radar

    Pr = S = PtGtGrl2s

    (4p)3R4Ls

    Basic Radar Equation

    R4 = PtGtGrl2s

    (4p)3SLs

    Radar Range Equation (solving for Rmax range for minimum signal Smin):

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    Range Ambiguity

    Caused by strong targets at a range in excess of the pulse repetition

    indicator or time

    Pulse return from the first pulse comes after the second pulse is sent

    This causes the range to be close instead of far away

    Radar does not know which pulse is being returned

    Large pulse amplitude and higher PRF amplifies the problem

    The maximum unambiguous range for given radar system can be

    determined by using the formula:

    Rmax = (PRI T) * C0/2 PRI = pulse repetition indicator

    T = pulse width time

    C0 = speed of light

    Example: PRI = 1msec, T = 1us

    Calculate Max unambiguous Range = (1ms 1us)*3*108/2 = 149.9km

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    Range Ambiguity

    P1 P2

    PRI Range Ambiguities

    t

    V

    Rmax = (PRI PW) * C0/2

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    Range Ambiguity Mitigation

    Decreasing the PRF reduces the range ambiguity

    Longer the time delay, higher free-space loss, smaller the return

    Transmit different pulses at each PRF interval

    Higher receiver complexity

    Requires multiple matched filters at each range bin and at each azimuth and elevation

    Increases rate of the DSP required for each separate transmit pulse and matched filter pair

    Vary the PRF, depending radars operational mode

    Requires changing the system parameters

    Used most often to mitigate range ambiguity

    Desired returns from the second pulse move with the PRF

    Undesired returns do not move since they are reference to the first pulse

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    Minimum Detectable Range

    Example

    P1

    t

    V R1 R2

    R3

    Minimum Detectable

    Range Pulse

    Does not interfere with

    the Radar pulse

    Tmin for Rmin = Pulsewidth

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    Minimum Detectable Range

    Radar minimum detectable range return cannot come back during the pulse width

    Rmin = (T + Trecovery)*C0/2

    T = Pulse width, Trecovery = time for pulse to recover

    Very close range targets equivalent to the pulse width not be detected

    Typical value of 1 s for the pulse width of short range radar corresponds to a minimum range of about 150 m

    Longer pulse widths have a bigger problem

    Typical pulse width T assuming recovery time of zero:

    Air-defense radar: up to 800 s (Rmin = 120 km)

    ATC air surveillance radar: 1.5 s (Rmin = 225 m)

    Surface movement radar: 100 ns (Rmin = 15 m)

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    Plan Position Indicator (PPI)

    The return is displayed on a Plan Position Indicator

    (PPI)

    Rotating Search Radars illuminates the targets on the PPI according to the angle received

    Range is displayed according to the distance from the center of the PPI

    Uses a range gate to lock on the range of the PPI

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    PPI and A-Scope Displays

    N

    S

    00

    900

    1800

    2700

    AoA = 770

    Range

    Gate

    PPI A-Scope

    Range

    Gate

    V

    t

  • www.BesserAssociates.com

    Besser Associates Besser Associates, Inc. 2014 All rights reserved

    Thank you for Attending !

    For more information on this subject please consider attending

    the live Besser course, Introduction to Radar, March 2 to 4,

    2015, in Costa Mesa, California.

    Contact Besser Associates at [email protected] or

    visit us at www.BesserAssociates.com

    Sponsored by:

    online at www.eastern-optx.com

  • Bullock Engineering Research www.BesserAssociates.com Copyright 2014

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    Additional Slides If Needed

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    Range Resolution

    Range resolution - separate two equal targets at the same

    bearing but different ranges

    Depends on the width of the transmitted pulse

    Types and sizes of targets

    Efficiency of the receiver and indicator

    Pulse width is the primary factor in range resolution

    Able to distinguish targets separated by one-half the pulse width

    Basically the same as minimum detectable range

    Theoretical range resolution is:

    Sr = (c0*t)/2

    Sr = range resolution as a distance between the

    two targets

    c0 = speed of light

    t = transmitters pulse width

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    Pulse Compression Range

    Resolution

    In pulse compression the range-resolution is given by the

    bandwidth of the transmitted pulse (Btx), not by its pulse width

    Sr = > c0/2Btx

    Sr = range resolution as a distance between the two targets

    c0 = speed of light

    Btx = band width of the transmitted pulse

    Allows very high resolution with long pulses with a higher

    average power

    Given: Btx = 20 MHz

    Calculate Range resolution Sr =

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    51

    Basic Radar Range Resolution

    CW without Compression

    CW without Compression

    Poor Resolution

    Good Resolution

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    52

    Pulse Compression

    Improves Range Resolution

    Using Spreading Techiques

    Chirped FM Compression

    Phase Shift Keying PSK Compression

    Good Resolution

    Good Resolution