METHOD OF DETERMINING ORBIT PARAMETERS OF AN ARTIFICIAL EARTH SATELLITE USING RECEIVING-TRANSMITTING SUPPORTING REFERENCE STATIONS

FIELD: cosmonautics.SUBSTANCE: invention relates to the field of cosmonautics, namely to technique of performing trajectory measurements and determining the parameters of the orbit of an artificial Earth satellite (AES), and can be used on ground and airborne flight control complexes to accurately d...

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Bibliographic Details
Main Authors Vatutin Vladimir Mikhajlovich, Sevidov Vladimir Vitalevich, Matyukhin Aleksandr Sergeevich, Modin Mikhail Ivanovich, Agievich Sergej Nikolaevich
Format Patent
LanguageEnglish
Russian
Published 12.12.2019
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