NASA NTRS · 19860063210
Gravity mismodelling on TOPEX orbit determination
Abstract
Gravity 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.
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Wu, S.-C., Lichten, S. M., Yunck, T. P.. 1986-08-01. Gravity mismodelling on TOPEX orbit determination. https://ntrs.nasa.gov/citations/19860063210
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