Patent
1977-07-29
1979-11-13
Brown, Thomas W.
179 15AC, 179 15AF, H04J 302
Patent
active
041744659
ABSTRACT:
Apparatus for transmitting particular output signals from a plurality of analog-to-digital converters to the guidance computer of an inertial navigation system. The number of channels of signals to be transmitted exceeds the number of available data lines. The A/D converter output is converted, according to its particular logic code, to a series of pulse counts which are thereafter multiplexed in a pulse combiner and applied to the data lines. During a first selected time interval, the pulses are accumulated for interleaving and transmission with the real time pulses in a second selected time interval. The multiplexing combines such interleaved pulses from one A/D converter output with those from another such output in alternate time intervals. Sync words are transmitted along with the data to permit the guidance computer software to demultiplex the data.
REFERENCES:
patent: 3872257 (1975-03-01), Bleickardt et al.
patent: 3872284 (1975-03-01), Seligman et al.
patent: 3995120 (1976-11-01), Pachynski, Jr.
patent: 4034404 (1977-07-01), Nakagome et al.
patent: 4049917 (1977-09-01), Copperi et al.
Meares Lawrence G.
Simpson Robert D.
Bissell Henry M.
Brown Thomas W.
McDonnell Douglas Corporation
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