Precise interferometric tracking of the DSCS II geosynchronous orbiterA demonstration of the precise tracking of a geosynchronous orbiter by radio metric techniques based on very-long-baseline interferometry (VLBI) has been jointly conducted by the Jet Propulsion Laboratory and Japan's Radio Research Laboratory. Simultaneous observations of a U.S. Air Force communications satellite from tracking stations in California, Australia, and Japan have determined the satellite's position with an accuracy of a few meters. Accuracy claims are based on formal statistics, which include the effects of errors in non-estimated parameters and which are supported by a chi-squared of less than one, and on the consistency of orbit solutions from disjoint data sets. A study made to assess the impact of shorter baselines and reduced data noise concludes that with a properly designed system, similar accuracy could be obtained for either a satellite viewed from stations located within the continental U.S. or for a satellite viewed from stations within Japanese territory.
Document ID
19860035120
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Border, J. S. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Donivan, F. F., Jr. (California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Shiomi, T. (Ministry of Posts and Telecommunications Radio Research Laboratories, Kashima, Japan)
Kawano, N. (Ministry of Posts and Telecommunications Radio Research Laboratories, Tokyo, Japan)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AIAA PAPER 86-0402Report Number: AIAA PAPER 86-0402