Real time orbit determination using GPS navigation solution

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Data

2007-07-01

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Resumo

This work analyses a real time orbit estimator using the raw navigation solution provided by GPS receivers. The estimation algorithm considers a Kalman filter with a rather simple orbit dynamic model and random walk modeling of the receiver clock bias and drift. Using the Topex/Poseidon satellite as test bed, characteristics of model truncation, sampling rates and degradation of the GPS receiver (Selective Availability) were analysed. Copyright © 2007 by ABCM.

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Palavras-chave

GPS, Kalman filter, Navigation solution, Orbit determination, Model truncation, Orbit estimator, Algorithms, Dynamic models, Global positioning system, Kalman filters, Real time systems, Signal receivers, Orbits

Como citar

Journal of the Brazilian Society of Mechanical Sciences and Engineering, v. 29, n. 3, p. 274-278, 2007.

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