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High Precision and Real Time Tracking of Low Earth Orbiters With GPS: Case Studies With TOPEX/POSEIDON and EUVETOPEX/POSEIDON carries a dual-frequency 6 channel GPS receiver while EUVE has a 12 channel single frequency receiver. Flying at an altitude of 1334 km, TOPEX/POSEIDON performs precise ocean altimetry, which demands the highest possible accuracy in determining the radial orbit component in post-processing. Radial RMS accuracies of about 2 cm were realized using reduced dynamic tracking techniques. In this approach, orbit errors due to force are substantially reduced by exploiting the geometric strength of GPS to solve for a set of stochastic forces. On EUVE, the emphasis was on evaluating real time positioning techniques with a single frequency receiver. The capability for real time 3D accuracies of 15 m in the presence of Selective Availability was shown. This was validated by comparing to a post-processed differential GPS truth orbit believed accurate to about 1 m.!.
Document ID
20060041923
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Yunck, Thomas P.
Bertiger, Winy I.
Gold, Kenn
Guinn, Joseph
Reichert, Angie
Watkins, Michael
Date Acquired
August 23, 2013
Publication Date
April 1, 1995
Subject Category
Astrodynamics
Meeting Information
Meeting: International Workshop on High Precision Navigation, 3rd
Location: Stuttgart
Country: Germany
Start Date: April 1, 1995
Distribution Limits
Public
Copyright
Other
Keywords
Tracking low-Earth orbiters

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