| | Apollo Guidance Computer and Other Computer History |
 | | The navigation and control information is obtained inertially by a gyro-servo-stabilized, three-gimbal platform system with three mutually orthogonal pendulous-integrating gyro accelerometers; the single-degree-of-freedom gyros as well as the accelerometers use externally-pressurized gas bearings. |
 | | The development of rocket engines and inertial measurement instruments was basic to turning the dream of poets into the reality of a trip to the moon, but on a narrower scale the development of practical guidance and navigation algorithms was enabled by the development of programmable digital computers and of higher order programming languages. |
 | | Basically, during boost guidance, the computer evaluates in-flight changes in booster speed and position derived from an inertial platform and develops signals to control the rocket engines so as to keep the booster on course. |
| www.klabs.org /richcontent/Misc_Content/AGC_And_History/AGC_History.htm (10792 words) |