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Multifunction Phased Array R d (MPAR)Radar (MPAR)
John Cho
18 November 2014
Sponsors: Michael Emanuel, FAA Advanced Concepts and Technology Development (ANG-C63)
Distribution Statement A. Approved for public release; distribution is unlimited.
This work is sponsored by the Federal Aviation Administration under Air Force Contract #FA8721-05-C-0002. Opinions, interpretations, recommendations and conclusions are those of the author and are not necessarily endorsed by the United States Government.
gy ( )Kurt Hondl, NOAA National Severe Storms Laboratory
MPAR Concept
ASR-8 ASR-9 ASR-11
Terminal AreaWeather
Current Aircraft and Weather Radars
Weather
Aircraft
Ground Based UAS S d A id
Multifunction Phased Array Radar (MPAR)
TDWRAircraft
ASR 8 ASR 9 ASR 11
Long Range Aircraft
Sense and Avoid
Non Cooperative
TDWR
ARSR-3 ARSR-4ARSR-1/2FPSMultifunction
Radar
Non-Cooperative Target
NEXRADLong Range Weather • Has potential to lower cost by
– Reducing number of radar units– Lowering O&M (no moving parts)– Streamlining support
infrastructure
CARSR
• Multiple stove-piped radars• Rotating dish technology
M i d f lif
infrastructure– Simplifying training and logistics– Open systems procurement and
maintenance• Increased performance benefits
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 2JYNC 18 November 2014
• Many nearing end-of-life p
Potential Reductionin Number of Radars
500
600
-34%R
equi
red
300
400
TMPARMPARLegacy
(4-m antenna)(8-m antenna)
-28%
-16%
of R
adar
s R
0
100
200 Legacy
Num
ber
01 2 3 4 5 6FAA Only FAA + NOAA FAA + NOAA
+ Air Force
ASRs + ASRs + ASRs +ASRs + TDWR
ASRs + TDWR + NEXRAD
ASRs + TDWR + NEXRAD + LRRs
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 3JYNC 18 November 2014
Greater potential cost savings if more stakeholders join
TMPAR = Terminal MPARLRR = Long Range Radar
Potential Federal Enterprise Capability Enhancements
Weather Observation andAir Surveillance New User EntrantsWind Farm
Improvements to Current Missions Emerging Needs
Observation and Prediction
Air Surveillance New User EntrantsMitigation
Miti t i P idE t d hi h lit B d t• Mitigates equipage failures to cooperative / dependent aircraft
• Enhanced target
• Provides non-cooperative target positions
• Offers support to avoidance and
• Extends high-quality observation to small and medium airports
• Icing risk identification
• Broad-spectrum clutter suppression
• Improved low altitude target g
acquisition and tracking
– Smaller RCS detection
– Improved clutter
well-clear policies and applications
• Hail identification• Improved forecasts• Longer lead times
for severe weather
gdetection and tracking
• Eliminate weather false-alarms on ATC displays
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 4JYNC 18 November 2014
pperformance warnings
ATC displays
RCS = radar cross section
NextGen Surveillance and Weather Radar Capability (NSWRC)
MPARSingle Function Radar Multifunction High Density
Some Candidate NSWRC Solutions
MPARS band
Single Function Radar(One-to-one legacy
replacement)L, S, and C bands
Multifunction High Density Short Range Radar Network
X band
• Low technical risk• Limited capability to
address operational shortfalls and emerging
• High technical risk– Risk reduction for
weather surveillance by NSF’s CASA program
• High technical risk• High capability
enhancement potentialP t ti l lif l t
Risk reduction required to validate MPAR as viable solution
shortfalls and emerging needs • Near-surface coverage
benefit• Potential life cycle cost
reduction
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 5JYNC 18 November 2014
Risk reduction required to validate MPAR as viable solution
CASA = Collaborative Adaptive Sensing of the Atmosphere
Outline
• IntroductionIntroduction
• Notional requirements and design
• Risk reduction activities
• SummarySummary
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 6JYNC 18 November 2014
MPAR Requirements
• “Notional Functional Requirements” jointly being developed by FAA and NOAA mainly based on requirements for current radars
• Requirements added to anticipate emerging needs– Terminal aircraft RCSTerminal aircraft RCS
• Reduced from 1 m2 to 0.25 m2
– Aircraft height estimation accuracy introduced• 500 ft rms (0.25–30 nmi), 1000 ft rms (30–60 nmi), ( ), ( ),
2000 ft rms (60–150 nmi), 3000 ft rms (150–250 nmi)– Wind turbine clutter mitigation
• RCS = 1m2, Pd = 80%, 1000 ft above wind farm– Precipitation volume scan update period
reduced to 60 sec
Requirements still evolving will adapt to stakeholder composition
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 7JYNC 18 November 2014
Requirements still evolving, will adapt to stakeholder composition
Legacy Requirements That Drive MPAR Performance
FunctionMaximum Range for Detection of
1m2 Target
Required Coverage Angular Resolution
Waveform Scan Period
Range Altitude Az El1m Target Range Altitude Az El
Terminal Area Aircraft
Surveillance(ASR-9/11)
55 nmi 60 nmi 25,000' 1.4 5o ~18 pulsesPRI ~ 1 ms 5 sec
En Route Aircraft
Surveillance(ARSR-4)
210 nmi 250 nmi 100,000' 1.4 2.0 ~10 pulsesPRI ~ 3 ms 12 sec
Airport Weather ~70 pulsesAirport Weather(TDWR) 250 nmi 48 nmi 70,000' 1 0.5 ~70 pulses
PRI ~ 0.6 ms >180 sec
Nationwide Weather
(NEXRAD)260 nmi 250 nmi 70,000' 1 1 ~50 pulses
PRI ~ 1 ms >240 sec
• Weather surveillance drives requirements for radar power and aperture size
Ai ft ill d i i t f b t d i it ti
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 8JYNC 18 November 2014
• Aircraft surveillance drives requirements for beam management and revisit time
MIT LL MPAR Concept Design
Two 6 x 2 beam clusters
Aircraft Aircraft SurveillanceSurveillance
Aircraft(up to 24 linear pol beams)
SurveillanceSurveillance
Weather(up to 12 linear pol beams)
Weather Weather SurveillanceSurveillance
Frequency: 2.7 - 2.9 GHzDiameter: 4m & 8mT/R per face: 5,000 / 20,000Beamwidth: 2 / 1° (broadside)A t/ 2 $50k
• Four radiating aperture faces• Antenna beam diversity
- Optimize energy-on-target vs. volume coverage Array cost/m2: $50kPolarization: Dual linear/circularBeam count: > 10 beamsBandwidth: ~3 MHzDuty cycle: 8%
ChallengingChallenging
- High sensitivity vs. rapid scanning
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 9JYNC 18 November 2014
Duty cycle: 8%Peak power: 8W/elementStraightforwardStraightforward
MPAR Adaptive BeamScanning Example
Aircraft SurveillanceAircraft Surveillance
Weather SensingWeather Sensing
Dual Pol Horizon Weather Scan
Single Pol Aircraft and Weather Volume Scan
Single Pol Aircraft Tracking
Dual Pol Weather Tracking
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 10JYNC 18 November 2014
Repeat
Outline
• IntroductionIntroduction
• Notional requirements and design
• Risk reduction activities
• SummarySummary
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 11JYNC 18 November 2014
Key Risk Reduction Activities
• Antenna– Cost– Dual polarization performance for weather– Manufacturability– Calibration and reliability– Asynchronous operation and self-interference
• Back end– Receiver cost– Adaptive multifunctional resource management– Open modular architecture
• Operational• Operational– RF spectrum resource usage– Wind-shear detection performance
Radar mission prioritization
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 12JYNC 18 November 2014
– Radar mission prioritization
MPAR Risk Reduction Timeline
Subarray Ten-Panel Demonstrator
Advanced Technology Demonstrator (ATD)Panel
Portable PlatformFull Scale RadarGen 2 PanelGen 1 PanelFull Scale Radar
Testing
Performance Aircraft and Weather 2 Panel Subarray
-60 -40 -20 0 20 40 60-50
-40
-30
-20
-10
0
Angle (deg)
Ampl
itude
(dB
)
Test and Eval
FY15-17
Performance Assessment
• Quantify polarization • Demonstrate full scale radar
FY 13-15
Mode Development
• Component and board development
2 Panel Subarray
FY 07-11
• Component re-spin
FY 12
Test and Eval
• Digital beam clusters• Verify thermal mgmt• Initial radar testing• Support IARD
• Real time radar backend• Multiple mode processing• Adaptive resource mgmt• Flexible test asset
S t IID
board development• Range testing• Initial cost /
performance data
• Tileable panels• Backplane design• Thermal Design• Range testing
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 13JYNC 18 November 2014
• Support IID
IARD = Investment Analysis Readiness DecisionIID = Initial Investment Decision
MIT LL Government Proof of Concept (GPC) MPAR Antenna Panel
RadiatorT/R ModuleRF Chip Set Beamformer0.180.18”
1.251.25”RF Receive RF Receive ChipChip
RF Transmit RF Transmit ChipChip
High Power High Power AmplifierAmplifier
MPAR panel attributes• 2.7-2.9 GHz operating band• 900 W peak RF transmit power
MPAR Panel
p p• Dual simultaneous receive polarization• Low production cost ($8k per panel)
Low cost and high performance met by
16”16”
g p y• Design for manufacturability• Low cost transmit/receive modules• Scalable aperture design
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 14JYNC 18 November 2014
• Digital subarray architecture
2-Panel Subarray Testing
Test Chamber Measurements Hanscom Field Measurements
Far-field amplitude of Mpar Testing5.nsi
40.00
50.00
40 00
-30.00
-20.00
-10.00
0.00
10.00
20.00
30.00
Elev
atio
n (d
eg)
-60-58-56-54-52-50-48-46-44-42-40-38-36-34-32-30-28-26-24-22-20-18-16-14-12-10-8-6-4-20
-50.00 -40.00 -30.00 -20.00 -10.00 0.00 10.00 20.00 30.00 40.00 50.00
Azimuth (deg)
-50.00
-40.00
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 15JYNC 18 November 2014
Panels are achieving objective performance
10-Panel Portable Demonstrator Array
Operational Parameters
Parameter ValueOperating Band 2.7-2.9 GHzPeak Transmit Power 3.5 kWWeather Sensitivity at 40 km 11 dBZPulse Width 80 µsRx Bandwidth 1.0 MHzReceiver Noise Figure 4.7 dBReceive Noise Floor -109 dBmAntenna Gain (Transmit) 33 dBAntenna Gain (Receive) 31 dB
Azimuth Beamwidth Tx = 2.5°Rx = 3.0
• Provides critical risk reduction data – Digital beam clusters
Polarization propertiesElevation Beamwidth Tx = 6.3°
Rx = 7.4°Array Elements, Total 640 (40 x 16)Array Size (w, h) 2.0 m x 0.8 m
– Polarization properties– Thermal management effectiveness– Initial radar testing
• Fabrication in progress
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 16JYNC 18 November 2014
• Field testing in CY15
Risk Reduction: Path Forward
Advanced Technology Demonstrator (ATD)
T h i l Ri k
User Community Outreach
Technical Risk Reduction
• Dual-pol weatherB lib ti
CONOPS Refinement
• Beam calibration• Adaptive
multifunctionality• Resource
sched ling
To replace NWRT SPY-1A antenna76 panels (4 m x 4 m)Performance
scheduling• Range and
angular sidelobes• Spectrum usage
• Front end: MIT LL GPC panels• Back end: Leverage Navy’s
ACRA program (tentative)
Requirements Development
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 17JYNC 18 November 2014
ACRA = Affordable Common Radar ArchitectureNWRT = National Weather Radar Testbed (Norman, OK)
Joint funding by NOAA and FAA
Summary
• MPAR is a potentially cost-effective and enhanced-performance solution for NextGen Surveillance and Weather Radar Capability (NSWRC)
• MIT LL has developed a conceptual MPAR system based on legacy and emerging observation needslegacy and emerging observation needs
• Next steps: Build and test Advanced Technology DemonstratorNext steps: Build and test Advanced Technology Demonstrator to further mitigate technical risk and refine system requirements
Lincoln Laboratory Air Traffic Control Workshop 2014MPAR - 18JYNC 18 November 2014