Angles-only orbit updates for low earth satellites
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This paper provides the development of a simplified covariance model for predicting the along-track error uncertainty and error uncertainty growth rate for the single-pass, angles-only orbit update, the validation of the model using simulation and real data cases, a summary of efforts made to characterize the uncertainty of general perturbations based element sets, and conclusions on the practical expectations of the single-pass, angles-only orbit update.
Advances in the Astronautical Sciences
author list (cited authors)
Alfriend, K. T., & Wiese, D.
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