Article ID Journal Published Year Pages File Type
1767970 Advances in Space Research 2006 9 Pages PDF
Abstract
In the paper the results of the orbit determination from the September 2003 campaign are reported. More in detail, the outcomes of some classical methods for solving the Lambert theorem, are compared with solutions based on the measurements fitted with the least squares method, with the circular orbit assumption results, with the one-site complete orbit determination and with the TLEs.
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Related Topics
Physical Sciences and Engineering Earth and Planetary Sciences Space and Planetary Science
Preview
Two-site orbit determination: The 2003 GEO observation campaign from Collepardo and Mallorca
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