Journal
Scientific and technical journal «Priborostroenie»
UDK527.62:523.2+623.466.33
Issue:5 (57)
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A method for estimation of orbit elements and spacecraft (SC) orientation parameters relative to a moving orbital coordinate system is proposed. The method is based on analysis of spacecraft axes hodograph formed with the use of astronomic measurements carried out with an optical-electronic device rigidly fixed on the SC body at known angles.