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GDGPS (Internet-based Global Differential GPS)
Global Differential GPS system with unparalleled
accuracy,
coverage,
and economy
GDGPS (Internet-based Global Differential GPS) is a uniquely powerful and flexible C-language software package
that provides a complete end-to-end system capability for GPS-based real-time positioning and orbit determination.
Features:
-
10 cm horizontal and 20 cm vertical real time positioing accuracy with dual frequency GPS receivers.
- 5 cm - level real time orbit determination for low Earth satellites carrying dual frequency GPS receivers.
- The most precise and complete set of geodetic, satellite dynamics, and GPS measurement models for uncompromising accuracy.
- Dual mode application: same software used to compute GPS orbit and clock corrections and, embedded, for user positioning/orbit determination.
- Uniformly valid corrections anywhere in the world or in space
- Internet-based correction dissemination
- Software proven operationally in a number of critical real time systems.
Complete end-to-end automation
Accomplishments:
- Extensively implemented for real-time and near-real-time user positioning and orbit determination:
- NASA Shuttle SRTM mission (rapid receiver validation)
- SNOE (Student Nitric Oxide Experiment) spacecraft
- NASA X33/RLV mission (onboard navigation demonstration package; payload integration and testing)
- NASA AirSAR mission (precise positioning and calibration for science data and control)
- Scheduled to fly on SAC-C GPS receiver, 2000
- Scheduled to fly on ST-5 Communications and Navigation Transceiver (CCNT), 2003
- Successful implementation for continuous operational control and conversion of
NASA Global GPS Network (GGN) data,
provided to the International GPS Service (IGS) on an operational basis (since 1/2000)
- Successful implementation in commercial wide-area differential service (SATLOC, 1995-2000)
- Successful implementation in Federal Aviation Administration (FAA)
Wide Area Augmentation System (WAAS) proof of concept demonstrations;
selected by FAA for implementation by Raytheon in operational system
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JPL clearance
number:
CL
01-1764
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