Stabilization and Control System: Difference between revisions

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[[Category:Stabilization and Control System (CSM)| ]]
[[Category:Stabilization and Control System (CSM)| ]]
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Revision as of 20:13, 29 November 2006

The Stabilization and Control System (SCS) provides a capability for monitoring and controlling the attitude of the spacecraft, for translational manoeuvers and SPS thrust vector control. Also the SCS is the backup system for the Primary Guidance, Navigation and Control System (PGNCS), which is the Apollo Guidance Computer basically.

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