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Open-loop nanosecond-synchronization for wideband satellite communicationsA synchronization technique for use with an onboard processing satellite communication system is discussed. The satellite oscillator is used both as the system time reference and as the frequency source for all downlink carriers and data clocks. Downlink timing is established at each system earth terminal through a combination of carrier and data-clock tracking and a downlink timing epoch signal consisting of one bit per TDMA data burst. Uplink timing is established by an open-loop range prediction process using precision ephemerides calculated and distributed by the central control station. Overall timing accuracy of the uplink signal at the satellite receiver of + or - 7 nanoseconds permits unambiguous identification of each data bit position in a 128 Mbps TDMA burst. This is accomplished by means of simple, inexpensive terminal hardware using available crystal oscillators for time/frequency references and digital synthesis techniques that may be implemented in digital LSI chips.
Document ID
19820043689
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Holmes, W. M., Jr.
(TRW Defense and Space Systems Group, Space Systems Div., Redondo Beach CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Meeting Information
Meeting: In: ITC/USA/''80
Location: San Diego, CA
Start Date: October 14, 1980
End Date: October 16, 1980
Accession Number
82A27224
Funding Number(s)
CONTRACT_GRANT: NAS3-22341
Distribution Limits
Public
Copyright
Other

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