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Orbit determination accuracies using satellite-to-satellite trackingThe results are reported of the ATS-6/GEOS-3 and the ATS-6 Nimbus-6 satellite-to-satellite orbit determination experiments. NASA intends to use the tracking data relay satellite system for operational orbit determination of NASA satellites. Hence, in the near future, satellite-to-satellite tracking data will be routinely processed to obtain orbits. The satellite-to-satellite tracking system used in the ATS-6/Nimbus-6 and ATS-6/GEOS-3 experiments performed with a resolution of 1 to 2 m in range and less than 1 mm/s in range rate for a 10-s averaging. A Bayesian least squares estimation technique utilizing independent ranging to the synchronous relay satellite was determined to be the most effective procedure for estimating orbits from satellite-to-satellite tracking data. The use of this technique yields estimates of user satellite orbits which are comparable in accuracy to what is usually obtained from ground based systems.
Document ID
19790036215
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Vonbun, F. O.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Argentiero, P. D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Schmid, P. E.
(NASA Goddard Space Flight Center Greenbelt, Md., United States)
Date Acquired
August 9, 2013
Publication Date
November 1, 1978
Publication Information
Publication: IEEE Transactions on Aerospace and Electronic Systems
Volume: AES-14
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Accession Number
79A20228
Distribution Limits
Public
Copyright
Other

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