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Improved solution accuracy for TDRSS-based TOPEX/Poseidon orbit determinationOrbit determination results are obtained by the Goddard Space Flight Center (GSFC) Flight Dynamics Division (FDD) using a batch-least-squares estimator available in the Goddard Trajectory Determination System (GTDS) and an extended Kalman filter estimation system to process Tracking and Data Relay Satellite (TDRS) System (TDRSS) measurements. GTDS is the operational orbit determination system used by the FDD in support of the Ocean Topography Experiment (TOPEX)/Poseidon spacecraft navigation and health and safety operations. The extended Kalman filter was implemented in an orbit determination analysis prototype system, closely related to the Real-Time Orbit Determination System/Enhanced (RTOD/E) system. In addition, the Precision Orbit Determination (POD) team within the GSFC Space Geodesy Branch generated an independent set of high-accuracy trajectories to support the TOPEX/Poseidon scientific data. These latter solutions use the geodynamics (GEODYN) orbit determination system with laser ranging and Doppler Orbitography and Radiopositioning integrated by satellite (DORIS) tracking measurements. The TOPEX/Poseidon trajectories were estimated for November 7 through November 11, 1992, the timeframe under study. Independent assessments were made of the consistencies of solutions produced by the batch and sequential methods. The batch-least-squares solutions were assessed based on the solution residuals, while the sequential solutions were assessed based on primarily the estimated covariances. The batch-least-squares and sequential orbit solutions were compared with the definitive POD orbit solutions. The solution differences were generally less than 2 meters for the batch-least-squares and less than 13 meters for the sequential estimation solutions. After the sequential estimation solutions were processed with a smoother algorithm, position differences with POD orbit solutions of less than 7 meters were obtained. The differences among the POD, GTDS, and filter/smoother solutions can be traced to differences in modeling and tracking data types, which are being analyzed in detail.
Document ID
19940031113
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Doll, C. E.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Mistretta, G. D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Hart, R. C.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Oza, D. H.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Bolvin, D. T.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Cox, C. M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Nemesure, M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Niklewski, D. J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Samii, M. V.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1994
Publication Information
Publication: Flight Mechanics(Estimation Theory Symposium, 1994
Subject Category
Astrodynamics
Accession Number
94N35620
Funding Number(s)
CONTRACT_GRANT: NAS5-31500
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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