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The guidance officer monitored on board navigational systems and on board guidance computer software. Responsible for determining the position of the spacecraft in space. One well-known guidance officer was Steve Bales, who gave the go call when the Apollo 11 guidance computer came close to overloading during the first lunar descent.
Apollo Command Module primary guidance system components Apollo Lunar Module primary guidance system components Apollo Inertial Measurement Unit. The Apollo primary guidance, navigation, and control system (PGNCS, pronounced pings) was a self-contained inertial guidance system that allowed Apollo spacecraft to carry out their missions when communications with Earth were interrupted, either as ...
guidance systems for Project Apollo and the Polaris missile [note 3] Fermilab: University of Chicago: Batavia, IL: discovery of the top quark: Georgia Tech Research Institute: Georgia Institute of Technology: Atlanta, GA: Radar, energy and electromagnetics work [1] [2] Idaho National Laboratory: MIT: Arco, ID
A guidance computer provides calculations and electronic interfaces for guidance, navigation, and control of a spacecraft or launch vehicle. Pages in category "Guidance computers" The following 9 pages are in this category, out of 9 total.
The D37D Minuteman III flight computer was initially supplied with the LGM-30G missile, as part of the NS-20 navigation system. The NS-20 D37D flight computer is a miniaturized general purpose (serial transmission) digital computer. The new NS-50 missile guidance computer (MGC) is built around a 16-bit high-speed microprocessor chip set.
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The D-17B (D17B) computer was used in the Minuteman I NS-1OQ missile guidance system. The complete guidance system contained a D-17B computer, the associated stable platform, and power supplies . The D-17B weighed approximately 62 pounds (28 kg), contained 1,521 transistors , 6,282 diodes , 1,116 capacitors , and 5094 resistors .
The Apollo Guidance Computer (AGC) was a digital computer produced for the Apollo program that was installed on board each Apollo command module (CM) and Apollo Lunar Module (LM). The AGC provided computation and electronic interfaces for guidance, navigation, and control of the spacecraft. [ 3 ]