METHOD OF DETERMINING ORBIT PARAMETERS OF AN ARTIFICIAL EARTH SATELLITE USING RECEIVING REFERENCE BENCHMARK STATIONS

FIELD: astronautics.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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Hauptverfasser:	Podyachev Pavel Aleksandrovich, Sevidov Vladimir Vitalevich, Bespalov Vyacheslav Leonidovich, Ledovskaya Elina Gennadevna, Matyukhin Aleksandr Sergeevich, Agievich Sergej Nikolaevich
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	ANALOGOUS ARRANGEMENTS USING OTHER WAVES DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES MEASURING PHYSICS RADIO DIRECTION-FINDING RADIO NAVIGATION TESTING
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