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High precision GPS orbit determination using March 1985 demonstration dataPreliminary orbit determination for satellites in the U.S. Department of Defense's Global Positioning System has been performed using GPS carrier phase data collected in March-April 1985 at 10 sites in the continental United States. The data were analyzed using a new data processing software package called GIPSY (GPS Inferred Positioning SYstem) and with existing covariance analysis software. Data from one day have been processed with average formal position errors of 1.4 to 3.6 meters. The true errors are probably somewhat larger. Covariance results are presented which suggest that the orbits can be obtained with formal errors under 2 meters after certain software issues are resolved.
Document ID
19860034946
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bertiger, W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wu, S.-C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Border, J. S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lichten, S. M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Williams, B. G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wu, J.-T.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Astrodynamics
Report/Patent Number
AIAA PAPER 86-0089
Report Number: AIAA PAPER 86-0089
Accession Number
86A19684
Distribution Limits
Public
Copyright
Other

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