Introduction To Radar Systems 2004

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Radar Systems EngineeringLecture 14Airborne Pulse Doppler RadarDr. Robert M. O’DonnellIEEE New Hampshire SectionGuest LecturerIEEE New Hampshire SectionRadar Systems Course 1Airborne PD 1/1/2010IEEE AES Society

Examples of Airborne RadarsCourtesy of US NavyF-16APG-66 , 68Courtesy of US Air ForceBoeing 737 AEW&CE-2CAPS-125Courtesy of milintelTRJOINT STARS E-8AAPY-3AWACSE-3AAPY-1Courtesy of US Air ForceCourtesy of US Air ForceRadar Systems CourseAirborne PD 1/1/20102IEEE New Hampshire SectionIEEE AES Society

Outline Introduction– The airborne radar mission and environmentClutter is the main issue Different airborne radar missions– Pulse Doppler radar in small fighter / interceptor aircraftF-14, F-15, F-16, F-35– Airborne, surveillance, early warning radarsE-2C (Hawkeye), E-3 (AWACS), E-8A (JOINT STARS)– Airborne synthetic aperture radarMilitary and civilian remote sensing missionsTo be covered in lecture 19, later in the course Radar Systems CourseAirborne PD 1/1/2010Summary3IEEE New Hampshire SectionIEEE AES Society

Block Diagram of Radar utter as seen from an airborne platform,Signal waveforms, and Doppler processingwill be the focus in this lectureAntennaSignal Processor r Rejection(Doppler Filtering)User Displays and Radar ControlGeneral Purpose ectionDataRecordingPhoto ImageCourtesy of US Air ForceRadar Systems CourseAirborne PD 1/1/20104IEEE New Hampshire SectionIEEE AES Society

First Use of Airborne RadarsUS APS-3 Radarwith Dish Antenna3 cm wavelengthGerman “Lichtenstein” RadarDipole array – 75 / 90 cm wavelengthCourtesy of Department of DefenseCourtesy of US Navy When they were introduced on airborne platforms duringWorld War II, they were used to detect hostile aircraft atnight in either a defensive or an offensive modeRadar Systems CourseAirborne PD 1/1/20105IEEE New Hampshire SectionIEEE AES Society

Role of Airborne Military Radars Missions and Functions– Surveillance, Tracking, Fire Control– Reconnaissance– Intelligence Examples– Air-to-air fighter combatAircraft interception (against air breathing targets)–––– Airborne Early warningAir to ground missionsClose air supportGround target detection and trackingRadar modes––––Radar Systems CourseAirborne PD 1/1/20106Pulse Doppler radarSynthetic Aperture radarDisplaced Phase Center Antenna (DPCA)Ground Moving Target IndicationIEEE New Hampshire SectionIEEE AES Society

Geometry of Airborne ClutterVP Key components of the ground clutter echo from radar’s onan airborne platform:– Main beam of antenna illuminates the ground– Antenna sidelobes illuminate clutter over a wide range ofviewing angles– Altitude return reflects from the ground directly below the radarThe Doppler frequency distributions of these effects and howthey affect radar performance differ with:1. radar platform velocity (speed and angle), and2. the geometry (aspect angle of aircraft relative to groundillumination point)Radar Systems CourseAirborne PD 1/1/20107IEEE New Hampshire SectionIEEE AES Society

Airborne Radar Clutter SpectrumNo Doppler AmbiguitiesVP and VT in same vertical planeVPAntennaMainlobeOutgoingTargetRelative Power (dB)Antenna SidelobesVTMainlobeClutterClutter FreeRadar Systems CourseAirborne PD 1/1/2010OutgoingTargetNoise 2VPλ8Clutter FreeSidelobe Clutter02VPλNoiseDoppler FrequencyIEEE New Hampshire SectionIEEE AES Society

Airborne Radar Clutter SpectrumNo Doppler AmbiguitiesVP and VT in same vertical planeVPAntennaMainlobeIncomingTargetRelative Power (dB)Antenna Sidelobes VTMainlobeClutterClutter FreeRadar Systems CourseAirborne PD 1/1/2010Clutter FreeSidelobe ClutterIncomingTargetNoiseNoise 2VPλ902VPλDoppler FrequencyIEEE New Hampshire SectionIEEE AES Society

Viewgraph Courtesy of MIT Lincoln Laboratory Used with permissionRadar Systems CourseAirborne PD 1/1/201010IEEE New HampshireMIT LincolnSectionLaboratoryIEEE AES Society

Constant Range Contours on theGroundRange to Ground ScenariohLines of Constant Range to GroundRSR S2 h 2 R G2 The projections on the ground of the lines of constantrange are a set circlesRadar Systems CourseAirborne PD 1/1/201011IEEE New Hampshire SectionIEEE AES Society

Constant Doppler Velocity Contours onthe GroundVC VP cos αα VP cos θ sin φVC Clutter velocityVP Platform velocity The projections on theground of the lines ofconstant Doppler velocityare a set hyperbolaeRadar Systems CourseAirborne PD 1/1/201012fD 2VC cos αλIEEE New Hampshire SectionIEEE AES Society

Constant Doppler Contours on GroundVC 0 VC VPVC VPThe lines of constantDopplerfrequency/velocity arecalled “Isodops”The equation for thefamily of hyperbolaedepend on:– Airborne radar heightabove ground– Angle between airborneradar velocity and thepoint on the ground thatis illuminated– Wavelength of radarVC 0Radar Systems CourseAirborne PD 1/1/201013IEEE New Hampshire SectionIEEE AES Society

Range-Doppler Ground Clutter ContoursRange ContoursCirclesDownRangeVC 0VC VP UpRangeVC VPDoppler ContoursHyperbolaeRadar Systems CourseAirborne PD 1/1/2010CrossRange14VC 0IEEE New Hampshire SectionIEEE AES Society

Range-Doppler Ground Clutter ContoursRange ContoursCirclesCrossRangeRange – DopplerCell on GroundΔf DΔRxDownRangeUpRangexPowerDoppler ContoursHyperbolaeRadar Systems CourseAirborne PD 1/1/201015Doppler FrequencyIEEE New Hampshire SectionIEEE AES Society

Unambiguous Doppler Velocity and RangeUnambiguous Range (nmi)400First Blind Speed (knots)30001000221000M401041λ f PRFVB zdBGnS35BaXndaBaK300100andcRU 2 f PRFYields30100.1110100λcVB 4 RUPulse Repetition Rate (KHz)Radar Systems CourseAirborne PD 1/1/201016IEEE New Hampshire SectionIEEE AES Society

Classes of Pulse Doppler RadarsRangeMeasurementDopplerMeasurementLow PRFUnambiguousHighlyAmbiguousMedium h PRFRadar Systems CourseAirborne PD 1/1/201017IEEE New Hampshire SectionIEEE AES Society

Missions for Airborne Military Radars“The Big Picture” Fighter / Interceptor Radars–Antenna size constraints imply frequencies at X-Band or higherReasonable angle beamwidths– This implies Medium or High PRF pulse Doppler modes for lookdown capabilityWide Area Surveillance and Tracking–Pulse Doppler solutionsLow, Medium and/or High PRFs may be used depending on the specificmission––– E-2CUHFAWACS S-BandJoint Stars X-BandSynthetic Aperture Radars will be discussed in a later lectureRadar Systems CourseAirborne PD 1/1/201018IEEE New Hampshire SectionIEEE AES Society

Outline Introduction– The airborne radar environment Different airborne radar missions– Pulse Doppler radar in small fighter / interceptor aircraftF-14, F-15, F-16, F-35High PRF ModesMedium PRF Modes– Airborne, surveillance, early warning radarsE-2C (Hawkeye), E-3 (AWACS), E-8A (JOINT STARS)– Airborne synthetic aperture radarMilitary and civilian remote sensing missionsTo be covered in lecture 19, later in the course Radar Systems CourseAirborne PD 1/1/2010Summary19IEEE New Hampshire SectionIEEE AES Society

Photographs of Fighter RadarsCourtesy of Northrop GrummanUsed with PermissionAPG-65(F-18)APG-66(F-16)Courtesy of RaytheonUsed with permissionCourtesy of USAFActive Electronically Scanned Arrays (AESA)APG-63 V(2)(F-15C)APG-81 (F-35)Radar built byRaytheonRadar Systems CourseAirborne PD 1/1/2010Courtesy of BoeingUsed with permission20Courtesy of Northrop GrummanUsed with PermissionIEEE New Hampshire SectionIEEE AES Society

Outline Introduction– The airborne radar environment Different airborne radar missions– Pulse Doppler radar in small fighter / interceptor aircraftF-14, F-15, F-16, F-35High PRF ModesMedium PRF Modes– Airborne, surveillance, early warning radarsE-2C (Hawkeye), E-3 (AWACS), E-8A (JOINT STARS)– Airborne synthetic aperture radarMilitary and civilian remote sensing missionsTo be covered in lecture 19, later in the course Radar Systems CourseAirborne PD 1/1/2010Summary21IEEE New Hampshire SectionIEEE AES Society

Pulse Doppler PRFsFrequencyPRF TypePRF Range*Duty Cycle* X- BandHigh PRF100 - 300 KHz 50% X- BandMedium PRF10 - 30 KHz 5% X- BandLow PRF1 - 3 KHz .5% UHFLow PRF300 HzLow* Typical values only; specific radars may vary inside and outside these limitsRadar Systems CourseAirborne PD 1/1/201022IEEE New Hampshire SectionIEEE AES Society

High PRF Mode FrequencyPRF TypePRF Range*X- BandHigh PRF100 - 300 KHzExample:PRF 150 KHzPRI 6.67 μsecDuty Cycle* 50%Duty Cycle 35%Pulsewidth 2.33 μsecUnambiguous Range 1 kmUnambiguous Doppler Velocity 4,500 knots For high PRF mode :– Range – Highly ambiguousRange ambiguities resolved using techniques discussed in Lecture13– Doppler velocity – UnambiguousFor nose on encounters, detection is clutter free– High duty cycle implies significant “Eclipsing Loss”Multiple PRFs, or other techniques requiredRadar Systems CourseAirborne PD 1/1/201023IEEE New Hampshire SectionIEEE AES Society

High PRF Mode – Range Eclipsing High PRF airborne radars tend to have a High Duty cycle to gethigh energy on the target– Pulse compression usedPRITimeTransmit PulsewidthReceive TimeUneclipsedTargetEclipsedTarget Eclipsing loss is caused because the receiver cannot bereceiving target echoes when the radar is transmitting– Can be significant for high duty cycle radars– Loss can easily be 1-2 dB, if not mitigatedRadar Systems CourseAirborne PD 1/1/201024IEEE New Hampshire SectionIEEE AES Society

High PRF Pulse Doppler Radar No Doppler velocity ambiguities, many range ambiguities– Significant range eclipsing loss Range ambiguities can be resolved by transmitting 3redundant waveforms, each at a different PRF– Often only a single range gate is employed, but with a largeDoppler filter bank The antenna side lobes must be very low to minimizesidelobe clutter– Short range sidelobe clutter often masks low radial velocitytargets High closing speed aircraft are detected at long range inclutter free region Range accuracy and ability to resolve multiple targets canbe poorer than with other waveformsRadar Systems CourseAirborne PD 1/1/201025IEEE New Hampshire SectionIEEE AES Society

Outline Introduction– The airborne radar environment Different airborne radar missions– Pulse Doppler radar in small fighter / interceptor aircraftF-14, F-15, F-16, F-35High PRF ModesMedium PRF Modes– Airborne, surveillance, early warning radarsE-2C (Hawkeye), E-3 (AWACS), E-8A (JOINT STARS)– Airborne synthetic aperture radarMilitary and civilian remote sensing missionsTo be covered in lecture 19, later in the course Radar Systems CourseAirborne PD 1/1/2010Summary26IEEE New Hampshire SectionIEEE AES Society

Medium PRF Mode FrequencyPRF TypePRF Range*X- BandMedium PRF10 - 30 KHzDuty Cycle* 5%Example : 7 PRF 5.75, 6.5, 7.25, 8, 8.75, 9.5 & 10.25 KHz(From Figure 3.44 in text)Range Ambiguities 14 to 26 kmBlind Speeds 175 to 310 knots For the medium PRF mode :– Clutter and target ambiguities in range and velocity– Clutter from antenna sidelobes is an significant issueRadar Systems CourseAirborne PD 1/1/201027IEEE New Hampshire SectionIEEE AES Society

Clear Velocity Regions for a MediumPRF RadarPRF (Hz)Clear Radial Velocity Regions for Seven PRF Radar Waveform57506500725080008750950010250No. of PRFs in Clear0100200300400500600Number of PRFs in Clear vs. Target Radial Velocity864200100200300400500600Doppler velocity of target (meters/sec) The multiple PRFs (typically 7) and their associated higher radarpower are required to obtain sufficient detections to unravel rangeand velocity ambiguities in medium PRF radarsRadar Systems CourseAirborne PD 1/1/201028IEEE New Hampshire SectionIEEE AES Society

Medium PRF ModeHigh PRF ModePowerPowerMedium PRF ModeTrue Doppler FrequencyPRFTrue Doppler FrequencyPRF 1PRF 2PRF 5PRF 4True TargetDopplerPRF 1 In the Doppler domain, the target and clutter alias (fold down)into the range 0 to PRF1, PRF2, etc.– Because of the aliasing of sidelobe clutter, medium PRF radarsshould have very low sidelobes to mitigate this problem In the range domain similar aliasing occurs– Sensitivity Time Control (STC) cannot be used to reduce cluttereffects (noted in earlier lectures) Range and Doppler ambiguity resolution techniquesdescribed in previous lectureRadar Systems CourseAirborne PD 1/1/201029IEEE New Hampshire SectionIEEE AES Society

Medium PRF Pulse Doppler Radar Both range and Doppler ambiguities exist––– Seven or eight different PRFs must be usedInsures target seen at enough Doppler frequencies to resolve rangeambiguitiesTransmitter larger because of redundant waveforms used to resolveambiguitiesThere is no clutter free region––Fewer range ambiguities implies less of a problem with sidelobeclutterAntenna must have low sidelobes to reduce sidelobe clutter Often best single waveform for airborne fighter / interceptor More range gates than high PRF, but fewer Doppler filters for eachrange gate Better range accuracy and Doppler resolution than high PRFsystemsRadar Systems CourseAirborne PD 1/1/201030IEEE New Hampshire SectionIEEE AES Society

Outline Introduction– The airborne radar environment Different airborne radar missions– Pulse Doppler radar in small fighter / interceptor aircraftF-14, F-15, F-16, F-35– Airborne, surveillance, early warning radarsE-2C (Hawkeye), E-3 (AWACS), E-8A (JOINT STARS)– Airborne synthetic aperture radarMilitary and civilian remote sensing missionsTo be covered in lecture 19, later in the course Radar Systems CourseAirborne PD 1/1/2010Summary31IEEE New Hampshire SectionIEEE AES Society

Airborne Surveillance & TrackingRadars Missions and Functions– Surveillance, Tracking, Fire Control– Reconnaissance– Intelligence Examples– Airborne early warning– Ground target detection and tracking Radar modes––––Pulse Doppler radarSynthetic Aperture radarDisplaced Phase Center Antenna (DPCA)Other modes/techniquesElevated radar platforms provide long range andover the horizon coverage of airborne and ground based targetsRadar Systems CourseAirborne PD 1/1/201032IEEE New Hampshire SectionIEEE AES Society

Examples of Airborne RadarsCourtesy of US NavyBoeing 737 AEW&CCourtesy of milintelTRGlobal HawkE-2CAPS-125Courtesy of US Air ForceJOINT STARS E-8AAPY-3AWACSE-3AAPY-1Courtesy of US Air ForceCourtesy of US Air ForceRadar Systems CourseAirborne PD 1/1/201033IEEE New Hampshire SectionIEEE AES Society

AEW Radar CoverageGround Based Surveillance Radar CoverageAirborne Surveillance Radar Coverage Elevating the radar can extend radar coverage well out over thehorizon Range Coverage -400 km to 800 kmGround based radars 400 kmAirborne radar 800 km–– IssuesHigh acquisition and operating costsLimited Antenna sizeRadar Weight and prime powerMore challenging clutter environment––––Radar Systems CourseAirborne PD 1/1/201034IEEE New Hampshire SectionIEEE AES Society

Characteristics of Ground Clutter(from Airborne Platform)vPGround Clutter Doppler Frequency2 vP2 vPfC cos α cos θ sin φλλMainBeamClutterΔf SL MLDoppler Frequency Width(Sidelobe Main Beam Clutter)Δf SL MLSidelobeClutterΔf ML4 vP λDoppler Frequency Width of MainBeam Clutter (Null to Null)2 vP λRadar Systems CourseAirborne PD 1/1/2010DopplerFrequency (Hz)352 vPλΔf MB 4 vP λ 4 vP λ LLIEEE New Hampshire SectionIEEE AES Society

Spread of Main Beam ClutterBeamCenterAircraft Velocity and TrajectoryIndividualClutterScattererα Doppler frequency ofclutter return depends onangle of clutter withvelocity vector of aircraft Doppler frequency ofclutter return at center ofbeam2 VPfC cos θλ Doppler spread of mainbeam clutter can be foundby differentiating thisequationθθBVPRadarSpread of Main Beam ClutterMaximum at θ 90 Adapted fromSkolnik Reference 1Radar Systems CourseAirborne PD 1/1/201036Depression angle of beam neglected2 VPΔf C θ B sin θλIEEE New Hampshire SectionIEEE AES Society

Clutter Spread with a UHF Airborne RadarClutter PowerSpeed of aircraft 400 knotsAntenna beamwidth 7 degreesθ 90 θ Angle between radar beamand the platform velocity vectorθ 60 60Hz35Hz0100200300θ 0 θ 30 30Hz400500600Doppler Frequency (Hz) Both the width of the clutter spectra and its center frequencydepend on the angle θ When the antenna points in the direction of the platform velocityvector, the Doppler shift of the clutter echo is maximum, but thewidth of the spectrum is theoretically zero When the antenna is directed in the direction perpendicular to thedirection of the platform velocity, the clutter center frequency iszero, but the spread is maximumAdapted from Skolnik Reference 1Radar Systems CourseAirborne PD 1/1/201037IEEE New Hampshire SectionIEEE AES Society

Aliasing of Clutter in Low PRF UHFAirborne RadarClutter PowerPRF 360 Hzθ 90 0θ 90 100200300360400Doppler Frequency (Hz) PRF 360 Hz corresponds to a maximum unambiguousrange of 225 nmiA relatively large portion of the frequency domain (Dopplerspace) is occupied by the clutter spectrum because ofplatform motionThe widening of the clutter needs to be reduced in order forstandard clutter suppression techniques to be effectiveRadar Systems CourseAirborne PD 1/1/201038IEEE New Hampshire SectionIEEE AES Society

AEW Airborne Radar Clutter Rejection There are 2 effects that can seriously degrade theperformance of a radar on a moving platform– A non-zero Doppler clutter shift– A widening of the clutter spectrum These may be compensated for by two different techniques– TACCAR (Time Averaged Clutter Coherent Airborne Radar)The change in center frequency of the clutter spectrum– DPCA (Displaced Phase Center Antenna)The widening of the clutter spectrum Radars which have used these techniques, over the years,to compensate for platform motion are Airborne EarlyWarning radarsRadar Systems CourseAirborne PD 1/1/201039IEEE New Hampshire SectionIEEE AES Society

Compensation for Clutter Doppler Shift TACCAR (Time Averaged Clutter Coherent Airborne Radar)– Also called “Clutter Lock MTI” The Doppler frequency shift from ground clutter can becompensated by using the clutter echo signal itself to setthe frequency of the reference oscillator (or coho)– This process centers the ground clutter to zero Dopplerfrequency– The standard MTI filter (notch at zero Doppler) attenuates theground clutter This technique has been used in ground based radars tomitigate the effect of moving clutter– Not used after the advent of Doppler filter processingRadar Systems CourseAirborne PD 1/1/201040IEEE New Hampshire SectionIEEE AES Society

AEW Advances - E-2D and MP-RTIPE-2D E-2D––Courtesy of US NavyMP-RTIP mounted on Proteus Aircraft Mechanically RotatingActive ElectronicallyScanned Antenna (AESA)Space Time AdaptiveProcessing (STAP)MP-RTIP––“Multi-Platform RadarTechnology InsertionProgram”Originally Joint StarsUpgrade ProgramGlobal Hawk and then awide area surveillanceaircraft–Advanced ground targetsurveillance capabilityCourtesy of US Air ForceRadar Systems CourseAirborne PD 1/1/201041IEEE New Hampshire SectionIEEE AES Society

E-3A Sentry - AWACSRadar APY-2E-3A Sentry AircraftS-Band (10 cm wavelength)Range 250 milesHigh PRF waveform to rejectclutter in look down modeLong range beyond thehorizon surveillance modeCourtesy of USAF AWACS Radar (S-Band)––Maritime surveillance modeMission –Long range Surveillance, Command and Control forair tactical environmentRadar System Improvement Program (RSIP)Advanced pulse Doppler waveformsPulse compression addedDetection range doubled (over original radar)Radar Systems CourseAirborne PD 1/1/201042See reference 1IEEE New Hampshire SectionIEEE AES Society

AWACS Radar AntennaRadomeRadar AntennaCourtesy of martin juliaCourtesy of Northrop GrummanUsed with Permission Radome Diameter 30 ftAWACS (APY-1/2) Antenna– Phased array – 26 ft by 4.5 ft ultralow sidelobe arrayElliptically shaped28 slotted waveguides with a total of over 4000 slotsAntenna is mechanically scanned 360 in azimuthUses 28 ferrite reciprocal phase shifters to scan in elevation10 sec rotation (data) rate––––See Skolnik reference 1Radar Systems CourseAirborne PD 1/1/201043IEEE New Hampshire SectionIEEE AES Society

Displaced Phase Center Antenna (DPCA)ConceptT1T2If the aircraft motion is exactly compensated by the movement of thephase center of the antenna beam, then there will be no clutterspread due to aircraft motion, and the clutter can be cancelled with atwo pulse canceller344334 2.pptRMO 9-01-00Viewgraph Courtesy of MIT Lincoln Laboratory Used with permissionRadar Systems CourseAirborne PD 1/1/201044IEEE New Hampshire SectionIEEE AES Society

DPCA for Mechanically Scanned AEW RadarIndividualClutterScattererAngle α offbeamcenterBeam 1Beam 2 A mechanically rotating antenna on a movingplatform that generates two overlapping(squinted) beams can act as a DCPA whenthe outputs of the two squinted beams areproperly combinedThe sum and difference of the two squinted beams aretaken––The sum is used for transmitThe sum and difference are used on receive A phase advance is added to the first pulse and a phase lag is added tothe second pulse beams are taken The added (or subtracted) phase shift depends on aircraft velocity, thePRF, and the scan angle of the radar relative to the aircraft direction The two signals are then subtracted, resulting in the cancellation of theDoppler spread of the clutterRadar Systems CourseAirborne PD 1/1/201045IEEE New Hampshire SectionIEEE AES Society

DPCA – The Math- AbbreviatedIndividualClutterScattererAngle α off Beam 1beamcenterΣ R Sum (2 pulses) of receive signalΔ R Difference (2 pulses) of receive signalBeam 2E22ηThe sum and difference of the two squinted beamsare takenThe sum is used for transmitThe sum and difference are used onreceiveAfter MUCH manipulation, the correctedreceived pulses become:Phasorrepresentation ofclutter echoes from2 successive pulsesE1E2Correctionsapplied to pulsesallowingcancellationηηRadar Systems CourseAirborne PD 1/1/2010e 2 j E 2 tan ηE146e1 j E1 tan ηPulse 1Σ R (α ) j k (v sin θ ) Δ R (α )Pulse 2Σ R (α ) j k (v sin θ ) Δ R (α )ΣConstant k accounts for differences inand Δ patterns, as well as a factor 4 TP/DFor more detail see Skolnik, Reference 1, pp 166-168IEEE New Hampshire SectionIEEE AES Society

Multiple Antenna Surveillance Radar(MASR)CP130-569DPCA OffDPCA OnViewgraph Courtesy of MIT Lincoln LaboratoryUsed with permissionRadar Systems CourseAirborne PD 1/1/201047IEEE New Hampshire SectionIEEE AES Society

Joint Surveillance Target Attack RadarSystem (Joint STARS)Courtesy of US Air Force Employs Interferometric SAR for airborne detection of groundvehicles and imaging of ground and surface targets– Employs APY-3, X Band radar Mission in wide area surveillance mode:– Coverage 50,000 km2– Detect, locate, identify, classify, and track trucks, tanks, and othervehiclesCan differentiate tracked and wheeled vehiclesCan see vehicles at ranges 200 km , moving at walking speedsRadar Systems CourseAirborne PD 1/1/201048IEEE New Hampshire SectionIEEE AES Society

Joint Stars RadarJSTARSAntennaCourtesy of Northrop GrummanUsed with Permission Radar employs a slotted array antenna 24 ft by 2 ft456 x 28 horizontally polarized elementsBeam scans 60 in azimuth; mechanically rotated in elevation–– Aperture can be used as a whole for SAR mappingWhen total aperture is divided into 3 independent apertures in theinterferometric mode, it is used for moving target detectionMoving targets are separated from clutter by different time of arrivals oftarget and clutter in the 3 aperturesDPCA techniques are used to cancel main beam clutter––Radar Systems CourseAirborne PD 1/1/201049IEEE New Hampshire SectionIEEE AES Society

Joint Stars Moving Target DetectionsOperation DesertStorm(Feb 1991)Courtesy of Northrop GrummanUsed with PermissionRadar Systems CourseAirborne PD 1/1/201050IEEE New Hampshire SectionIEEE AES Society

Outline Introduction– The airborne radar environment Different airborne radar missions– Pulse Doppler radar in small fighter / interceptor aircraftF-14, F-15, F-16, F-35– Airborne, surveillance, early warning radarsE-2C (Hawkeye), E-3 (AWACS), E-8A (JOINT STARS)– Airborne synthetic aperture radarSAR basics to be covered in lecture 19Military and civilian remote sensing missionsTo be covered in lecture 19, later in the course Radar Systems CourseAirborne PD 1/1/2010Summary51IEEE New Hampshire SectionIEEE AES Society

Detection of Ground Moving Targets Ground Moving Target Indication (GMTI)– Low or medium PRF pulse Doppler radar used– PRF chosen so that Doppler region of interest isunambiguous in range and Doppler– Ku (16 GHz) or Kα (35 GHz) Band often used, since fixedminimum detectable Doppler frequency will allow detection oflower velocities than X band– APG-67 (X-Band) in F-20 fighter has GMTI mode usingmedium PRF– AWACS has low PRF ship detection mode Side-Looking Airborne Radar (SLAR)– Standard airborne radar subtracts sequential conventionalimages of terrain ( Non-coherent MTI) to detect moving targetsRadar Systems CourseAirborne PD 1/1/201052IEEE New Hampshire SectionIEEE AES Society

Detection of Ground Moving Targets Synthetic Aperture Radar (SAR) with MTI– SARs (discussed in lecture 19) produce excellent images offixed targets on the groundGood cross range resolution obtain by processing sequentialtarget echoes as aircraft moves a significant distance LCross range resolution inversely proportional to L not antenna size D– Moving targets distorted and smeared in SAR image– Can be detected if target Doppler is greater than bandwidthof clutter echo– Requires high PRF to avoid aliasing issues Joint Stars– Uses interferometer for clutter suppression processingRadar Systems CourseAirborne PD 1/1/201053IEEE New Hampshire SectionIEEE AES Society

Summary Difficult ground clutter environment is chief radar design driver forairborne radarsElevated radar platform implies ground clutter at long rangeBoth Doppler frequency of clutter and its spread depend on radarplatform motion and scan angle–– Clutter challenges with Airborne radarsAntenna aperture size often limits frequencies, so that ambiguousrange and Doppler velocity issues arise–Low, Medium and High PRF Modes each have unique clutter issuesDoppler spreading of ground clutter, particularly at broadside, viewingcan degrade performance– Sophisticated clutter suppression techniques can alleviate some ofthese issuesDPCA techniquesMedium and High PRF modes often imply higher power–– Active Electronically Scanned arrays and advanced signalprocessing techniques (STAP) offer significant new capabilities forairborne radarsRadar Systems CourseAirborne PD 1/1/201054IEEE New Hampshire SectionIEEE AES Society

Homework Problems From Skolnik (Reference 1)Problems 3-19, 3-20, 3-21, 3-22, 3-23, and 3-24Show that the maximum Doppler frequency of ground clutter as seenby an airborne radar is––2V h2 1 2 fD λ R Where:V velocity of airborne radarλ radar wavelengthh height of radar above groundR slant rangeShow that, for an airborne radar flying at a constant height above theground, the lines of constant clutter velocity are a set of hyperbolae–The last problem is from Roger Sullivan’s previously referenced textRadar Systems CourseAirborne PD 1/1/201055IEEE New Hampshire SectionIEEE AES Society

References1. Skolnik, M., Introduction to Radar Systems, McGraw-Hill, NewYork, 3rd Ed., 20012. Barton, D. K., Modern Radar System Analysis, Norwood,Mass., Artech House, 19883. Skolnik, M., Editor in Chief, Radar Handbook, New York,McGraw-Hill, 3rd Ed., 20084. Skolnik, M., Editor in Chief, Radar Handbook, New York,McGraw-Hill, 2nd Ed., 19905. Nathanson, F. E., Radar Design Principles, New York,McGraw-Hill, 1st Ed., 19696. Richards, M., Fundamentals of Radar Signal Processing,McGraw-Hill, New York, 20057. Schleher, D. C., MTI and Pulsed Doppler Radar, Artech,Boston, 19918. Long, W. H., et. al, “Medium PRF for the AN/APG-66 Radar”,Proceedings of the IEEE, Vol. 73, No 2, pp 301-311, February1985Radar Systems CourseAirborne PD 1/1/201056IEEE New Hampshire SectionIEEE AES Society

Acknowledgements Niall J. DuffyDr. Allen HearnMark A. WeinerRadar Systems CourseAirborne PD 1/1/201057IEEE New Hampshire SectionIEEE AES Society

Radar Systems Course 3 Airborne PD 1/1/2010 IEEE New Hampshire Section IEEE AES Society Outline Introduction – The airborne radar mission and environment Clutter is the main issue Different airborne radar missions – Pulse Doppler radar in small fighter / interceptor aircraft F-14, F-15, F-16,

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