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VLBI determination of synchronous equatorial satellite orbits.A first-order theory of satellite orbit determination using time-difference data is developed for the case of a synchronous, equatorial spacecraft. Also, a first order error analysis is presented that permits one to estimate how errors in assumed or measured quantities affect the values of the derived orbital parameters. The theory is applied to observational data obtained during a series of VLBI (Very-Long-Baseline Interferometry) experiments conducted between stations at Rosman, North Carolina, and Mojave, California, using the ATS-3 satellite as a radio source. Orbit parameters derived from the VLBI data show good agreement with those determined by the ATS project office using more conventional tracking techniques.
Document ID
19720057902
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ross, S.
(S. Ross and Co. Boston, Mass., United States)
Date Acquired
August 6, 2013
Publication Date
September 1, 1972
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 72-924
Report Number: AIAA PAPER 72-924
Accession Number
72A41568
Funding Number(s)
CONTRACT_GRANT: NAS5-20360
Distribution Limits
Public
Copyright
Other

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