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First assessment of GPS-based reduced dynamic orbit determination on TOPEX/PoseidonThe reduced dynamic Global Positioning System (GPS) tracking technique has been applied for the first time as part of the GPS experiment on TOPEX/Poseidon. This technique employs local geometric position corrections to reduce orbit errors caused by the mismodeling of satellite forces. Results for a 29-day interval in early 1993 are evaluated through postfit residuals and formal errors, comparison with GPS and laser/DORIS dynamic solutions, comparisons on 6-hr overlaps of adjacent 30-hr data arcs, altimetry closure and crossover analysis. Reduced dynamic orbits yield slightly better crossover agreement than other techniques and appear to be accurate in altitude to about 3 cm RMS.
Document ID
19950035440
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Yunck, T. P.
(Jet Propulsion Lab. Cal. Inst. of Tech., Pasadena, CA, United States)
Bertiger, W. I.
(Jet Propulsion Lab. Cal. Inst. of Tech., Pasadena, CA, United States)
Wu, S. C.
(Jet Propulsion Lab. Cal. Inst. of Tech., Pasadena, CA, United States)
Bar-Sever, Y. E.
(Jet Propulsion Lab. Cal. Inst. of Tech., Pasadena, CA, United States)
Christensen, E. J.
(Jet Propulsion Lab. Cal. Inst. of Tech., Pasadena, CA, United States)
Haines, B. J.
(Jet Propulsion Lab. Cal. Inst. of Tech., Pasadena, CA, United States)
Lichten, S. M.
(Jet Propulsion Lab. Cal. Inst. of Tech., Pasadena, CA, United States)
Muellerschoen, R. J.
(Jet Propulsion Lab. Cal. Inst. of Tech., Pasadena, CA, United States)
Vigue, Y.
(Jet Propulsion Lab. Cal. Inst. of Tech., Pasadena, CA, United States)
Willis, P.
(Jet Propulsion Lab. Cal. Inst. of Tech., Pasadena, CA, United States)
Date Acquired
August 16, 2013
Publication Date
April 1, 1994
Publication Information
Publication: Geophysical Research Letters
Volume: 21
Issue: 7
ISSN: 0094-8276
Subject Category
Astrodynamics
Accession Number
95A67039
Distribution Limits
Public
Copyright
Other

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