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1
Update on NASA Uses of GPS
11th GNSS WorkshopSeoul, South Korea4-5 November 2004
Dr. Scott PaceOffice of Space Communications
NASA Headquarters
2
Vision for Space Exploration
3
NASA Vision and MissionNASA Vision and Mission
4
Topics for Discussion
Satellite Navigation ActivitiesNASA’s Contribution to IGS
Global Differential GPSTDRSS Augmentation Service
Launch Vehicle Tracking Search and Rescue
GPS Technologies & ApplicationsProbing the Earth
Geodesy and Oceanography Atmosphere and IonospherePrecision Orbit Determination
Formation FlyingFuture Developments
National Policy and Vision
5
Satellite Navigation Activities -International GPS Service (IGS)
NASA Key Contribution Areas
(60 out of 286 NASA’s)
JPL
JPL
JPL JPL
JPL
JPLGoddard
What is IGS?
• The International GPS Service (IGS) was formally recognized in 1993 by the International Association of Geodesy (IAG), and began routine operations on January 1, 1994
• Over 10 years it has expanded to a coordinated network of over 300 GPS monitoring stations from 200 contributing organizations in 75 countries
• Mission: “to provide a service to support, through GPS data products, geodetic and geophysical research activities” – IGS Terms of Reference
• Collects, archives, processes, and distributes GPS observation data with typical 1 hour latency (not in real-time).
IGS Network Products:
• High accuracy GPS orbits• Earth rotation parameters • IGS tracking station coordinates and velocities • GPS satellite and IGS tracking station clock
information • Zenith tropospheric path delay estimates • Global ionospheric maps• Available at:
http://igscb.jpl.nasa.gov/components/prods.html
6
Satellite Navigation Activities -NASA’s Contribution to IGS
• IGS Central Bureau at JPL responsible for day-to-day management and coordination
– Significant international outreach activity for GPS and NASA– Network coordination for international standardization across ~80 agencies
• JPL Analysis Center, Network Operations, and Operational Data Center• Global Data Center at GSFC+• JPL/GSFC members on IGS Governing Board
• NASA GPS Stationso NASA Cooperative Stations• Other Agency Stations
Tracking Network of the International GPS Service
Highlighting NASA’s Contributions
7
Satellite Navigation Activities –Global Differential GPS (GDGPS)
Uplink
Broadcast
TDRSS
Space users
Land lines
QuickTime™ and aPhoto - JPEG decompressor
are needed to see this picture.
Terrestrial usersIridium Inmarsat
Features:• Fully operational since 2000• 60 dual-frequency GPS
geodetic reference stations• 10 cm horizontal & 20 cm
vertical real-time positioning accuracy with dual frequency GPS receivers
• 10 cm level real–time orbit determination for LEO satellites with dual frequency GPS receivers
• Not certified for safety-of-life applications
For more information see:http://gipsy.jpl.nasa.gov/igdg
GDGPS Operations Center
Frame
Internet
NASA’s global real time network
8
Satellite Navigation Activities -Powerful GPS Performance Monitoring
The GDGPS System tracks each GPS satellite by at least 6 sites, and by 15 sites on average, enabling robust, real-time GPS performance monitoring with 4 sec to alarm
The GDGPS GPS Integrity Monitor
9
Satellite Navigation Activities -TDRSS Augmentation Service for Satellites (TASS)
Under Development• TASS provides NASA’s GDGPS
corrections via TDRSS satellites
• Integrating NASA’s Ground and Space Infrastructures
• Provides user navigational data needed to locate the orbit and position of user satellites
47o W171o W
85o E
~18-20o
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Satellite Navigation Activities -Launch Vehicle Tracking
• Space-based navigation and range safety technologies are key components of the next generation launch and test range architecture
– Developed by NASA in conjunction with the Defense Department and the Federal Aviation Administration
– Provides a more cost-effective launch and range safety infrastructure while augmenting range flexibility, safety, and operability
Typical EastCoast Launch
Area
Typical WestCoast Launch
Area
East Coast TDRSCoverage Footprint(s)
West Coast TDRSCoverage Footprint(s)
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Distress Alerting Satellite System (DASS)
Cospas-Sarsat System• International cooperative effort with
Search & Rescue (SAR) payloads on numerous satellites and a worldwide network of 45 ground terminals
• Relay distress signals from maritime, aviation, and land-based beacons
• 1997 Canadian Follow-On SAR System (FOSS) study showed MEO constellation would provide an optimal follow-on space platform
DASS• SAR Payloads to fly on the GPS satellite
constellation• Under Development by the NASA SAR Mission
Office in partnership with the DoD & Sandia National Labs (SNL) in support of the National SAR Committee (NSARC)
• Reduces search area from square km to square meters, reduce location time from hours to minutes.
DASS Proof-of-Concept (POC)
406 MHz Uplink
S-Band downlink for POC
1544 MHz for OPS
SAR POC Ground Station(s)
SAR Aircraft
Beacons
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GPS Technologies and Applications -Probing the Earth with GPS
IONOSPHEREIONOSPHEREOCEANSOCEANS SOLID EARTHSOLID EARTH
ATMOSPHEREATMOSPHERE
Significantwave heightSignificant
wave height
Ocean geoid andglobal circulationOcean geoid andglobal circulation
Surface windsand sea state
Surface windsand sea state
Short-term eddyscale circulationShort-term eddyscale circulation
OCEANSOCEANS
High resolution 3Dionospheric imagingHigh resolution 3D
ionospheric imaging
Ionospheric struc-ture & dynamics
Ionospheric struc-ture & dynamics
Iono/thermo/atmo-spheric interactionsIono/thermo/atmo-
spheric interactions
Onset, evolution& prediction ofSpace storms
Onset, evolution& prediction ofSpace storms
TIDs and globalenergy transportTIDs and globalenergy transport
Precise ion cal forOD, SAR, altimetryPrecise ion cal forOD, SAR, altimetry
IONOSPHEREIONOSPHERE
Climate change &weather modelingClimate change &weather modeling
Global profiles of atmosdensity, pressure, temp,and geopotential height
Global profiles of atmosdensity, pressure, temp,and geopotential height
Structure, evolutionof the tropopause
Structure, evolutionof the tropopause
Atmospheric winds,waves & turbulenceAtmospheric winds,waves & turbulence
Tropospheric watervapor distribution
Tropospheric watervapor distribution
Structure & evolutionof surface/atmosphere
boundary layer
Structure & evolutionof surface/atmosphere
boundary layer
ATMOSPHEREATMOSPHERE
Earth rotationPolar motion
Earth rotationPolar motion
Deformation of thecrust & lithosphereDeformation of thecrust & lithosphere
Location & motionof the geocenter
Location & motionof the geocenter
Gross massdistributionGross massdistribution
Structure, evolution of the deep interior
Structure, evolution of the deep interior
Shape of the earthShape of the earth
SOLID EARTHSOLID EARTH
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Science – Geodesy and Oceanography
GPS 1
GPS 2
LEO
GPS 4GPS 3
Ocean surface • Height • Roughness (winds)
Reference ellipsoid
h2h1
Troposphere: vertically integrated precipitable water vapor
Bi-Static Ocean Reflectrometry• Operational ocean altimeter calibrations for Navy
and NASA
Gravity Field Measurements• GRACE dual-satellite mission • JPL GPS Receiver with integrated camera
and K-band spacecraft to spacecraft tracking
• 1-micron accuracy measurement• Improve knowledge of the Earth’s gravity
field by several orders of magnitude
14
Science – Atmosphere and Ionosphere
GPS Global Network occultation techniques• Global snapshots of ionospheric structure for
scientific research and space weather applications
GPS Receivers in Low-Earth Orbit• High-resolution soundings of atmospheric
properties (e.g. temperature) and ionospheric structure and irregularities
Occulting LEO
Occulting GPS
Calibrating GPS
Ground receiver
Ionosphere
Neutral atmosphere
EarthOcculted Signal
Technology Transfer to WAAS• Real-time software for GPS orbits, clocks, and
ionosphere maps• Enhanced ionosphere capability improved
safety/availability algorithms
Ionospheric Remote Sensing• Input to Navy/AF advanced space weather models• Improved navigation• Mitigate effects on communications• Improved geo-location and surveillance• Improved understanding of ionospheric response to
storms• Improve understanding of ionosphere-
magnetosphere coupling• Improve understanding of ionosphere-lower
atmosphere coupling
GPS Satellite Occultation Techniques
15
GPS Technologies and Applications - Sample Precision Orbit Determination Activities
5 cm (20-cm real-time)operational automated processing
20000 km altitude
GPS
• 2-cm radial orbits (Topex GPS flight receiver, Motorola built to JPL specs)
• 1-cm radial orbits (Jason-1 GPS flight receiver, JPL Blackjack design)
operational automated processing
1336 km altitude
Geostationary36000 km altitude(TDRSS, QZSS)
1 m, ground-based trackingWith GPS < 10 cm
MicroLab/GPSMET730 km altitude
Shuttle Radar Topography Mission (SRTM): 230-km alt45-cm orbit accuracy
CHAMP: 470-km alt< 5-cm orbit accuracy
Recent Results with JPL-Built Blackjack Flight GPS Receivers
SAC-C: 705-km alt< 5-cm orbit accuracy
GRACE: 500-km alt (2 s/c)2-cm orbit accuracy10-psec relative timing1-micron K-band ranging
• Other JPL Blackjack GPS flight receivers in development: COSMIC (6 orbiters), PARCS (Space Station), and OSTM (Jason-2).
16
GPS Technologies and Applications -Formation Flying
Summary• Technology will enable a large number of
spacecraft to be managed with minimum ground support.
• The result will be a group of spacecraft with the ability to detect errors and cooperatively agree on the appropriate maneuver to maintain their desired positions and orientations.
• Applicable to any mission class, low-Earth or Deep Space, that desires to fly multiple satellites autonomously.
Technology• Innovative use of fuzzy logic decision making
capabilities and natural language to resolve multiple conflicting constraints .
• Scripting environment to enable algorithm updates without software changes.
• Flight wrapper that interfaces directly with command & data handling subsystem for input & output.
• Multiple operating modes to allow execution control.
• Generic closed-loop formation flying control algorithms applicable to many missions.
• Modular architecture design.
Missions• Earth Observing (EO-1) &
Landsat 7• Aqua, CALIPSO, CloudSat,
Parasol, & Aura.
... and many others
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GPS-Based Technologies and Applications -The final frontier in navigation...
Another ‘GPS’ - Mars Network
• Integrated Navigation and Telecommunications• Develop a communications capability to provide a
substantial increase in data rates and connectivity from Mars to Earth
• Develop an in situ navigation capability to enable more precise targeting and location information on approach and at Mars.
http://marsnet.jpl.nasa.gov/
Terrestrial Planet Finder
• Objective: find Earth-like planets up to 45 light years away • Potential technologies include precision formation flying
• Several small telescopes acting as a very large one• ~1cm accuracy levels
http://planetquest.jpl.nasa.gov/TPF/tpf_index.html
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Backup Slides (Background Material)
19
Contributors to this Presentation
• Dr. Lawrence Young – Jet Propulsion Laboratory– 818-354-5018 [email protected]
• Allen Farrington – Jet Propulsion Laboratory – 818-393-5260 [email protected]
• Dr. Yoaz Bar-Sever – Jet Propulsion Laboratory– 818-354-2665 [email protected]
• Dr. Frank Bauer – Goddard Space Flight Center – 301-286-3102 [email protected]
• Dr. Dave Affens - Goddard Space Flight Center – 301-286-9839 [email protected]
• Dr. Michael Moreau – Goddard Space Flight Center– 301-286-8382 [email protected]
• Roger J. Flaherty – Goddard Space Flight Center– 301-286-7028 [email protected]
• Scott Murray – Johnson Space Center– 281-483-8242 [email protected]
• Dr. Scott Pace – NASA Headquarters– 202-358-1811 [email protected]
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Satellite Navigation Activities -Tracking and Data Relay Satellite System (TDRSS)
• The Tracking and Data Relay Satellite Project (TDRS) system consists of in-orbit telecommunications satellites stationed at geosynchronous altitude and associated ground stations located at White Sands, New Mexico, and Guam.
• Functions:– Space Network tracking.– Provide data, voice and video services to NASA scientific satellites, the Shuttle,
International Space Station, and to other NASA customers. – Provide user navigational data needed to locate the orbit and position of NASA user
satellites.
F-5174°WTDW
F-7171°WStored
F-1049°W
F-6047°WTDS
F-4041°WTDE
F-3275°WTDZ
WHITE SANDS COMPLEX
GODDARD SPACE FLIGHT
CENTER
GUAM REMOTE GROUND TERMINAL
F-8171.5°W
F-9150°WTest
F-10150.7°WTest
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Satellite Navigation Activities -GPS Integrity Monitoring with GDGPS
GDGPS is ideally suited for GPS integrity/performance monitoring:• State space approach (as in the OCS) enables separation of orbit and clock errors• Large global network allows estimation of clocks independent of models (unlike
OCS), enabling prediction of integrity failures• Large global network enables implementation of majority voting schemes• High operational reliability• High performance monitoring: high accuracy, multiple metrics, absolute metrics• Independent of any other system employed in support of GPS operations
Leverage the NASA tens of million dollar investment in the GDGPS infrastructure
A prototype GPS integrity monitor was developed by JPL funded by IGEB and NASA • Operational since May 2003• 100% availability to-date, with no known failures• No false alarms• All GPS anomalies monitored• Extremely positive feedback from 2SOPS
3000
4000
5000
6000
7000
8000
9000
15
20
25
30
35
40
5 6 7 8 9 10 11 12 13
# of Hits
# of Distinct IP
s
Month, 2003
Non-JPL/Aerospace Usage Statistics
22
Distress Alerting Satellite System (DASS)
DASS Provides• 406 MHz ‘bent pipe’ repeaters on future GPS
satellites• Full compatibility with existing and future 406 MHz
beacons• Global detection and location
• Beacons without embedded GPS – greater than Cospas-Sarsat accuracy with 3 bursts or less
• Self-locating beacons – GPS accuracy after single beacon burst
• Support USAF/military SAR responsibilities• Alert data downlink freely available internationally• Low technical risk and low cost (uses modified
existing GPS hardware)
Optionally Could Provide• Short digital message return confirmation
message • Aids in false alarm mitigation • Direct communications with survivors • Support rescue force coordination• Reduced interference susceptibility via
confirmation
Development Status
On-Orbit Testing• Four DASS capable satellites, Block IIRs, in-orbit
as of 2004• Preliminary results support feasibility analysis
DASS POC Ground Equipment• Antenna system installation completed 3rd quarter
2004• Ground station equipment acquisition underway• The DASS Local User Terminal being developed
at GSFC
Ground Station Site Selection• Antennas on GSFC Building 28 roof, ground
station equipment in Building 25• GSFC physical space construction begin