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Differential correction capability of the GTDS using TDRSS dataA differential correction (DC) capability was implemented in the Goddard Trajectory Determination System (GTDS) to process satellite tracking data acquired via the Tracking and Data Relay Satellite System (TRDRSS). Configuration of the TDRSS is reviewed, observation modeling is presented, and major features of the capability are discussed. The following types of TDRSS data can be processed by GTDS: two way relay range and Doppler measurements, hybrid relay range and Doppler measurements, one way relay Doppler measurements, and differenced one way relay Doppler measurements. These data may be combined with conventional ground based direct tracking data. By using Bayesian weighted least squares techniques, the software allows the simultaneous determination of the trajectories of up to four different satellites - one user satellite and three relay satellites. In addition to satellite trajectories, the following parameters can be optionally solved: for drag coefficient, reflectivity of a satellite for solar radiation pressure, transponder delay, station position, and biases.
Document ID
19800019889
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Liu, S. Y.
(Computer Sciences Corp. Greenbelt, MD, United States)
Soskey, D. G.
(Computer Sciences Corp.)
Jacintho, J.
(NASA Goddard Space Flight Center)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Publication Information
Publication: Flight Mech.(Estimation Theory Symp.
Subject Category
Astrodynamics
Accession Number
80N28390
Funding Number(s)
CONTRACT_GRANT: NAS5-24300
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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