This paper describes the frame synchronization scheme and mechanism to be used for the Space Shuttle Time-Division-Multiplexing (TDM) communications system. The probability of frame synchronization acquisition, mean acquisition time, the probability of staying in sync after lock and mean time to loss lock as functions of system parameters are analyzed and derived. (DePo)
Frame synchronization for the space shuttle TDM communications systems
Rahmensynchronisation fuer die Uebertragung von Nachrichten an die Raumfaehre TDM
ADVANCES IN INSTRUMENTATION, PART 2. ISA CONF. AND EXHIBIT ; 32 ; 183-191
1977
9 Seiten, 4 Bilder, 2 Tabellen, 1 Quelle
Aufsatz (Konferenz)
Englisch
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