Gemini Guidance Computer
The Gemini Guidance Computer (sometimes Gemini Spacecraft On-Board Computer, OBC) was a digital, serial computer designed for Project Gemini, America's second human spaceflight project. The computer, which facilitated the control of mission maneuvers, was designed by the IBM Federal Systems Division.
Also recorded as Gemini Spacecraft On-Board Computer · Gemini Digital Computer
Gemini Guidance Computer
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The Gemini Guidance Computer (sometimes Gemini Spacecraft On-Board Computer, OBC) was a digital, serial computer designed for Project Gemini, America's second human spaceflight project. The computer, which facilitated the control of mission maneuvers, was designed by the IBM Federal Systems Division.
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wikidata · Q1501099 · wikipedia · Gemini Guidance Computer
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Key facts
Key facts
• Name — Gemini Guidance Computer • Invent Name — IBM Federal Systems Division • Manufacturer — IBM Federal Systems Division • Type — Avionics Guidance Computer • Processor — Discrete Components • Frequency — 7.143 kilohertz clock • Memory — 39-bit words memory, each composed of three 13-bit syllables, 4,096 words of memory, in a ferrite core array • Ports — Modular Display Keyboard (MDK), Modular Display Readout (MDR), Attitude Control and Maneuver Electronics (ACME), Inertial Measurement Unit (IMU), Horizon Sensors, Time Reference System (TRS) • Dimensions — (H)×(W)×(D)
Functionality
Functionality
• Illustration — Locations of the Gemini Guidance System Project Gemini was the first with an on-board computer, as Project Mercury was controlled by computers on Earth. The Gemini Guidance Computer was responsible for the following functions: • Ascent – serves as a backup guidance system. The switchover is manually controlled by the astronauts • Orbital flight – gives the astronauts the capacity to navigate, allowing them to choose a safe landing spot in an emergency and calculate the timing of retrofire (on extended missions ground data may become unavailable when ground data network rotates out of the orbital plane). • Rendezvous – serves as primary reference by providing guidance information to the astronauts. The orbit parameters are determined by the ground tracking which are then sent to the spacecraft; the guidance computer was responsible for processing the information along with sensed spacecraft attitude. The information was presented to the astronauts in terms of spacecraft coordinates. • Reentry – feeds commands directly to the reentry control system for automatic reentry or provides the guidance information to the astronauts for manual reentry.
Specifications
Specifications
• The computer was architecturally similar to the Saturn Launch Vehicle Digital Computer, in particular in the instruction set; however its circuit integration was less advanced. The GGC weighed 58.98 pounds (26.75 kg) and was powered by 28V DC. During a short power outage it could be powered by the Auxiliary Computer Power Unit (ACPU). • 39-bit words memory, each composed of three 13-bit syllables • Ferrite core memory of 4,096 words • Two's complement integer arithmetic • 7.143 kilohertz clock (140 μs per instruction); all instructions took a single cycle except for multiplication and division
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- Wikidata, structured authority record Q1501099: Gemini Guidance Computer
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- “Gemini Guidance Computer”, English Wikipedia, consulted as further reading
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