| |
| | The Apollo Guidance Computer (AGC) |
 | | The guidance and navigation (GandN) system measures spacecraft attitude and velocity, determines trajectory, controls spacecraft attitude, controls the thrust vector of the service propulsion engine, and provides abort information and display data. |
 | | The input section consists of four registers which enable inter- communication between the AGC and the other GandN subsystems, the stabilization and control system, the mission sequencer, the S-IVB guidance, and MSFN. |
 | | Output 0 Register Provides the transmission link from the AGC to the DSKYs by control of 14 banks of relays which provide display of data and routing of control signals to the ISS, OSS, and SCS. |
| www.apollosaturn.com /gnc.htm (10716 words) |
|