The Apollo Flight Director/Attitude Indicator (FDAI) was a critical instrument that showed spacecraft orientation using a rotating ball mechanism nicknamed the "8-ball". The device used three motors and servo loops with synchros to control ball rotation across roll, pitch, and yaw axes. The mechanism employed slip rings to
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The FDAI in ApolloThe FDAI mechanismSynchros and the servo loopThe amplifiersHistory of the FDAIComparing the ARU/11-A and the FDAIDifferences from ApolloThe Shuttle's ADI (Attitude Director Indicator)ConclusionsNotes and referencesSort: