Overview of ultra-precise time transfer formation flying, and spacecraft-spacecraft tracking systems
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Engineering topics
Publications and source records attributed to Lichten, S..
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Presentation in three parts. Part 1: GPS capabilites in JPL's tracking systems and applications section: Introduction. Part 2: JPL's GPS Receiver Technology. Part 3: JPL's relevant expertise in GPS performance analysis and software.
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Radar altimeter missions require precise estimates of the satellite radial orbit position in order to support measurement of surface heights.
Two key NASA OES research objectives are the Seasonal to Interannual Climate Variability and Prediction and Long-Term Climate/Natural Variability and Change investigations.
In February 1998 Student Nitric Oxide Explorer (SNOE) was successfully launched and began scientific observations.
Technology is currently available to support real-time on-board knowledge of the position of a low earth orbitor at the 5-15 meter level using the civilian broadcast GPS signal with sophisticated models and filtering techniques onboard the spacecraft.
In this paper, we describe some recent advances in GPS-based precise orbit determination for low-Earth orbiting satellites.
This paper proposes an implementation of AFF that borrows technology from the Global Positioning System (GPS), using measurements of both r-f carrier phase and a ranging code.
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We describe results from an experiment in which TDRS and GPS satellites were tracked simultaneously from a small (3 station) ground network in the western United States. We refer to this technique as 'GPS-like tracking' (GLT) since the user satellite - in this case TDRS - is essentially treated as a participant in the GPS constellation. In the experiment, the TDRS K(sub space-to-ground link (SGL) was tracked together with GPS L-band signals in enhanced geodetic-quality GPS receivers (TurboRogue). The enhanced receivers simultaneously measured and recorded both the TDRS SGL and the GPS carrier phases with sub-mm precision, enabling subsequent precise TDRS orbit determination with differential GPS techniques. A small number of calibrated ranging points from routine operations at the TDRS ground station (White Sands, NM) were used to supplement the GLT measurements in order to improve determination of the TDRS longitude. Various tests performed on TDRS ephemerides derived from data collected during this demonstration - including comparisons with the operational precise orbit generated by NASA Goddard Space Flight Center - provide evidence that the TDRS orbits have been determined to better than 25 m with the GLT technique.
An experimental system, called GPS-like tracking, was used to track TDRS and GPS satellites simultaneously from a small (3 station) ground network. Comparison with the operational precise orbit indicates that GLT determined the TDRS orbit to within 25 m.
The flight data have been combined at JPL with ground GPS data from a global network to routinely produce precise TOPEX/Poseidon orbits.
GPS-based tracking is increasingly becoming the tracking system of choice for low-Earth orbiters
Geocentric Tracking Station coordinates can be measured with global positioning system.
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Beginning June 1992 and continuing indefinitely as part of our contribution to FLINN (Fiducial Laboratories for an International Natural Science Network), DOSE (NASA's Dynamics of the Solid Earth Program), and the IGS (International GPS Geodynamics Service), analysts at the Jet Propulsion Laboratory (JPL) have routinely been reducing data from a globally-distributed network of Rogue Global Positioning System (GPS) receivers.