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Gravity mismodelling on TOPEX orbit determinationGravity mismodeling limits the dynamic orbit determination accuracy of TOPEX which requires an altitude accuracy of about 15 cm or better. This paper provides an assessment of this effect for a dynamic GPS tracking scheme, and investigates a nondynamic GPS tracking technique that eliminates the problem. Analysis indicates that TOPEX altitude error could be affected by as much as 30-40 cm when dynamic differential GPS tracking is used, although efforts now underway to improve the gravity model could reduce this. With the nondynamic technique, the positional change of TOPEX is inferred from the accurate, continuous GPS carrier phase measurements rather than from a dynamic model which is prone to gravity error. TOPEX altitude accuracy better than 15 cm is attainable with nondynamic tracking over a few hours.
Document ID
19860063210
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wu, S.-C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lichten, S. M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Yunck, T. P.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 12, 2013
Publication Date
August 1, 1986
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AIAA PAPER 86-2056
Report Number: AIAA PAPER 86-2056
Accession Number
86A47948
Distribution Limits
Public
Copyright
Other

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