NASA NTRS · 19810002566
Semiannalytical satellite theory and sequential estimation
Abstract
Kalman filtering techniques are combined with a semianalytical orbit generator to develop a sequential orbit determination algorithm. The algorithm is investigated for computational efficiency, accuracy, and radius of convergence by comparison with truth ephemerides and a Cowell special perturbations filters (GTDS). Test cases relevant to satellite navigation are examined.
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Taylor, S. P., Cefola, P. J.. 1980-10-01. Semiannalytical satellite theory and sequential estimation. https://ntrs.nasa.gov/citations/19810002566
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