Real time orbit determination using GPS navigation solution
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2007-07-01
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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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Journal of the Brazilian Society of Mechanical Sciences and Engineering, v. 29, n. 3, p. 274-278, 2007.