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 88-4211Report Number: AIAA PAPER 88-4211