METHOD FOR EPHEMERAL CONTROL OF SPACECRAFT GLOBAL NAVIGATION SATELLITE SYSTEM

FIELD: physics. ^ SUBSTANCE: low-orbiting spacecraft fitted with apparatus for synchronising onboard time scale with system time scale, apparatus for determining orbit parametres from terrestrial television signals and onboard apparatus for inter-satellite measurements is taken to an orbit. During o...

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Bibliographische Detailangaben
1. Verfasser: STREL'NIKOV SERGEJ VASIL'EVICH
Format: Patent
Sprache:eng ; rus
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