NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Sub-meter GPS orbit determination and high precision user positioning - A demonstrationHigh-accuracy orbit solutions have been obtained for GPS satellites, and submeter orbit accuracy is demonstrated for two well-tracked satellites. Orbit accuracy was tested based upon orbit repeatability from independent data sets, orbit prediction, ground baseline determination, and formal errors. Baselines of up to 2000 km in North America found with the GPS orbits show a daily repeatability of 0.3-1.5 parts in 10 to the 8th, and are found to agree well with VLBI solutions at the level of 0.3-3 parts in 10 to the 8th. Baselines were also determined between Florida and sites in the Caribbean region over 1000 km away, with a daily repeatability of 1-4 parts in 10 to the 8th.
Document ID
19880063127
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lichten, Stephen M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bertiger, Willy I.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Katsigris, Eugenia C.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Astrodynamics
Report/Patent Number
AIAA PAPER 88-4211
Meeting Information
Meeting: AIAA/AAS Astrodynamics Conference
Location: Minneapolis, MN
Country: United States
Start Date: August 15, 1988
End Date: August 17, 1988
Accession Number
88A50354
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available