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Communication Interface for SAMSAn interface is described that supplies communications between the flight instruments and the analog input of an existing conventional recording unit for the Shuttle Space Acceleration Measurement System (SAMS), a data acquisition unit. The architecture and current implementation of an STD bus/LonTalk communication interface are described.
Document ID
20060036973
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
hdl:2014/29232
Authors
Koffman, M.
Hartley, F.
Date Acquired
August 23, 2013
Publication Date
January 1, 1995
Subject Category
Communications And Radar
Distribution Limits
Public
Copyright
Other
Keywords
SAMS accelerometer communication interface

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