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Sensitivity of high-accuracy Tracking and Data Relay Satellite System (TDRSS) user spacecraft orbit determination to tracking schedulesThe results of a study to analyze the dependence of TDRSS user spacecraft orbit determination consistencies on varying tracking schedules are presented. In this study, the TDRS-East orbit determination results obtained utilizing Bilateration Ranging Transponder System data were evaluated. Six state parameters, three position and three velocity components and the solar radiation pressure coefficient, are estimated for TDRS-East. It is concluded that, in order to achieve high-precision orbit determination, the tracking coverage should not fall below 10 minutes every two orbits as decreasing it to every four orbits will significantly degrade the accuracy; present state-of-the-art consistency in orbit determination using TDRSS tracking is approximately 15 to 20 meters.
Document ID
19910027693
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Doll, C. E.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Gramling, C. J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Oza, D. H.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Radomski, M. S.
(Computer Sciences Corp. Lanham, MD, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Accession Number
91A12316
Funding Number(s)
CONTRACT_GRANT: NAS5-31500
Distribution Limits
Public
Copyright
Other

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