Looking Ahead for GPS - Stanford University

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10/19/2008 SCPNT Talk © Bradford W. Parkinson 1 Looking Ahead for GPS --- Bradford Parkinson Emeritus Professor Stanford University Department of Aeronautics and Astronautics

Transcript of Looking Ahead for GPS - Stanford University

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Looking Aheadfor GPS ---

Bradford ParkinsonEmeritus Professor

Stanford UniversityDepartment of Aeronautics and Astronautics

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"You've got to be very careful if you don't knowwhere you are going, because you might not get

there." -

GPtS – the Stealth Utility

• The Future• Challenges

Note: t = TIME

-- Yogi Berra

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Today, GPS Serves over 300 Million Users(from the FAA & C. Moon, AMTI)

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GPS Applications have Proliferated

• Civil– Transportation

• Aviation• Automobile• Maritime• Rail Control

– Public Services– Timing &

Frequency– Surveying– Surveillance– Other

• Military

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A Fundamental Change in Warfare

Improved BattlefieldSituational Awareness

Enable Precision,All-Weather Operations

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What’s Next?

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GLONASS –(Russia)

PNT to Explode withOpportunities

Galileo(European)GPS

(USA)

Compass(Beidou China)

QZSS(Japan)

The Five Design Keys (& Barriers to Entry)1. The CDMA signal (PRN or Spread spectrum)2. Van-Allen qualified atomic clocks3. Orbit prediction to a few meters (URE) in 20,000 miles of travel4. Spacecraft that lasted about ten years (cost of ownership)5. User Equipment that could (eventually) be miniaturized (<$)

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New Signals are On the Way

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Summary - Spectrum of Modernized GPSSignals

L5ARNS/RNSS Band

L1ARNS/RNSS Band

L2RNSS Band

P(Y)C/A

L2CM

L5

L1C

Earlier GPSDual Frequency w/Semi-codeless P(Y)

Block IIR-MLaunch 2005Dual FrequencyL1 C/A & L2C

Block IIF/IIR-M+Launch 2008Three FrequencyL1 C/A, L2C, & L5

Block IIILaunch 2013

L1C, L2C, L5,& L1 C/A Code

L5

New!

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GPS L2 GPS L1

1164MHz

Galileo E1 L1 E2Galileo E6Galileo E5A Galileo E5B

GPS L5 GLONASSG2

GLONASSG1

1188MHz

1214MHz

1217MHz

1239MHz

1260MHz

1261MHz

1300MHz

1559MHz

1563MHz

1587MHz

1591MHz

1593MHz

1610MHz

RNSS Band

Upper L-Band

RNSS Band

1151MHz

1237MHz

ARNS Band ARNS Band

RNSS BandRNSS Band

GLONASSG3 ?

Compass B6 B1Compass

B5BB2

Coming: a Plethora of Signals

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So what are the major new (orexpanded) applications going to be?

• Expanded Crustal Tracking

• Precision Tracking and Reporting (AirTraffic ADS-B)

• Cell/GPS explosion – where will this go?

"Predicting the future is easy. It's trying to figureout what's going on now that's hard.“ - Fritz R. S.

Dressler

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Robotic or “Assisted” Control already a Major Application of GPS

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New Systems: Robotic Use Of GPS at Stanford

Typical Accuracy-Four Inches

Blind Landing Tests – 110 straight successes with one go around

Stanford Robot Tractor

Note fourantennas toprovide 0.1o

Attitude

Tracking Test @ 5 m/s – worst error~ 3 inches!

Autonomous Model Helicopter

GPS Position, Velocity and Attitude

“Stanley” Vehicle the WinnerStanford-Berkeley

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A Future System: Auto-guided Automobilesand Freeway Automatic Traffic Control

• Use all InternationalPosition Signals

• Vector Kinematic Receivers (10 cm or better)

• MEMS/IMU/CSAC• Radars• Cooperative Tracking of

other vehiclesADS-B for Highways?

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A Caution:Three Critical

Issuesfor GPtS

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We are Victims of our success:

GPS Enormous Capability

Worldwide DependencyWhat must we do to insure that the

Trust in GPtSis not misplaced?

Preamble to the Issues

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The Three Issues

• Sustainment• Robustness• Interchangeability

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GPS Issue #1 – (Availability)Constellation Sustainment

• Average on-orbit life 8.9 years• First IIF currently available for launch:

January 2009• First GPS III currently available for

Operations - April 2014

Needed: Sustained, high-level supportfor earlier GPS III delivery and availability

It is imperative the we avoid “GPS Brownouts”

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GPS Issue #2 –GPS Robustness (Deterrence)

• Constellation size of 30+X for users inimpaired environments (the GDOP imperative)

• Affordable GPS Receiver InterferenceRejection Technology (inertial integration anddigital beam steering technology)

• GPS Backup – eLoran?

Need: Full, urgent Commitment by US

Needs full development

Needs decisions

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GPS Issue #3 –GPS and Galileo-True, Total Interoperability

• Real Measure: Interchangeability “Mix and

Match” with the same ranging accuracy

– L1C defined, implemented, and operable

– Seamless WAAS/EGNOS/+ ?

– True clock Synchronization (Common Clock) and common grid

• Payoff – Availability, Accuracy and

Robustness for Worldwide Users

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As providers of GPtS

we must insure the Service

is Always Available - To meet:

the Safety, Economic, and Convenience

Needs of the World

And the Defense of Freedom

The Burden for the GPS Community

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Thanks for your Attention -

Questions?

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Backups

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Illustrating why current numberof Satellites is Minimal (Courtesy GPS

World and John Lavrakas)• Accuracy is strongly driven by Masking Angle and

number of satellites (the impaired user’s problem)

• Above 10o, less than 30 satellites destroys accuracyand availability

Monthly Availability of24 sats 92 to 100%

Accuracy vs. Mask Angle(degrees)

The Knee

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THE “Big Five” Civil Goals for GPS1. Assured Availability of GPS signals-Including impaired situations

(mountains, urban areas, foliage, etc.)– Number of GPS Satellites/Geometry– Interoperability and Standardization with Galileo et al

2. Resistance to Interference (RFI)– Additional Satellite RF power and Frequency Diversity– More jam resistant GPS receivers

3. Accuracy– Require Prediction Accuracy (Satellite Clocks and Age of

Update)– Improved Satellite Geometry is essential– Augmentations: WAAS, LAAS,EGNOS, MSAS, NDGPS, PLs

4. Bounded inaccuracy to limit wild points– Concerned with the 1% or less “wild data points”– Good Satellite Geometry Coverage is Imperative

5. Integrity - eliminating HMI, meeting required time to alarm– WAAS– RAIM

Three of top four Goals are driven by the number of satellites –

hence DSB & IRT30+X satellite recommendation