NASA NTRS · 19870028443
The mission configuration process for the Spartan attitude control system
Abstract
The Spartan attitude control system (ACS) control electronics assembly cold plate has a standard connector interface to the rest of the Spartan payload and ground equipment. The connectors carry gyro signals, optical sensor signals, the experiment interface, the gas command decoder interface, and a pneumatics interface. Different flights can employ different optical sensor complements; the ACS engineer must accordingly connect the sensor error signals to the proper pins and connectors on the ACS electronics.
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Stone, R. W.. 1986-01-01. The mission configuration process for the Spartan attitude control system. https://ntrs.nasa.gov/citations/19870028443
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