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The Spartan attitude control system - Control electronics assemblyThe Spartan attitude control system (ACS) represents an evolutionary development of the previous STRAP-5 ACS through the use of state-of-the-art microprocessors and hardware. Despite a gyro rate signal noise problem that caused the early depletion of argon gas, the Spartan 101 experiment was able to collect several hours of data from two targets. Attention is presently given to the ACS sequencer module, sensor interface box, valve driver box, control electronics software, jam tables, and sequencer programs.
Document ID
19870028434
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stone, R. W. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AIAA PAPER 86-2524
Accession Number
87A15708
Distribution Limits
Public
Copyright
Other

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