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GPS tracking of TOPEX/POSEIDON: Results and implicationsA reduced dynamic filtering strategy that exploits the unique geometric strength of the Global Positioning System (GPS) to minimize the effects of force model errors has yielded orbit solutions for TOPEX/POSEIDON which appear accurate to better than 3 cm (1 sigma) in the radial component. Reduction of model error also reduces the geographic correlation of the orbit error. With a traditional dynamic approach, GPS yields radial orbit accuracies of 4-5 cm, comparable to the accuracy delivered by satellite laser ranging and the Doppler orbitography and radio positioning integrated by satellite (DORIS) tracking system. A portion of the dynamic orbit error is in the Joint Gravity Model-2 (JGM-2); GPS data from TOPEX/POSEIDON can readily reveal that error and have been used to improve the gravity model.
Document ID
19950049099
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Bertiger, W. I.
(NASA Jet Propulsion Lab. Pasadena, CA, United States)
Bar-Sever, Y. E.
(NASA Jet Propulsion Lab. Pasadena, CA, United States)
Christensen, E. J.
(NASA Jet Propulsion Lab. Pasadena, CA, United States)
Davis, E. S.
(NASA Jet Propulsion Lab. Pasadena, CA, United States)
Guinn, J. R.
(NASA Jet Propulsion Lab. Pasadena, CA, United States)
Haines, B. J.
(NASA Jet Propulsion Lab. Pasadena, CA, United States)
Ibanez-Meier, R. W.
(NASA Jet Propulsion Lab. Pasadena, CA, United States)
Jee, J. R.
(NASA Jet Propulsion Lab. Pasadena, CA, United States)
Lichten, S. M.
(NASA Jet Propulsion Lab. Pasadena, CA, United States)
Melbourne, W. G.
(NASA Jet Propulsion Lab. Pasadena, CA, United States)
Date Acquired
August 16, 2013
Publication Date
December 15, 1994
Publication Information
Publication: Journal of Geophysical Research
Volume: 99
Issue: C12
ISSN: 0148-0227
Subject Category
Spacecraft Instrumentation
Report/Patent Number
ISSN: 0148-0227
Accession Number
95A80698
Distribution Limits
Public
Copyright
Other

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