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Summary Of: Apollo Guidance Computer
Encyclodia Page On: Apollo Guidance Computer
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Eldon C. Hall
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architectural work
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Raytheon
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user interface
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command module
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lunar module
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Primary Guidance, Navigation and Control System
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Saturn V
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Launch Vehicle Digital Computer (LVDC)
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Abort Guidance System (AGS)
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TRW
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fly-by-wire
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F-8 Crusader
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Space Shuttle
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integrated circuits (ICs)
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NOR
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logic gate
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Fairchild Semiconductor
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resistor-transistor logic
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wire wrap
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PC boards
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epoxy
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Minuteman II
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guidance computer
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diode-transistor logic
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diode logic
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Texas Instruments
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RAM
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magnetic core memory
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ROM
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core rope memory
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microseconds
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parity bit
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CPU
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16-bit
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overflow
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one's complement
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user interface
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calculator
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electroluminescent
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seven segment displays
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relays
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silicon controlled rectifiers
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octal
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vectors
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attitude
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delta-V
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sextant
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inertial guidance
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Flight Director Attitude Indicator
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kHz
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crystal
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clock
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real-time clock
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registers
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accumulator
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program counter
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return address
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instruction format
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opcode
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ones' complement
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IBM 360's
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base address
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overflows
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single precision
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double precision
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fixed-point numbers
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interrupts
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real-time clock
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counters
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ms
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De Morgan's theorem
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assembly language
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real-time operating system
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version control
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octal
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Monitor
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Apollo 4
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6
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Apollo I
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far pointers
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Lunar Module
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PGNC System
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Apollo 11
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fail-safe
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Steve Bales
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Jack Garman
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Inertial Measurement Unit
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HTTP
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404
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World Wide Web
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programmable handheld calculator
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HP-65
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Apollo-Soyuz Test Project
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AP-101
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Space Shuttle
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History of computer hardware
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AIAA
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ISBN 1-56347-185-X
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PDF
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PDF
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Australian Broadcasting Corporation
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Orbiter
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Categories
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Embedded systems
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Avionics computers
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Apollo program
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Wikipedia references cleanup
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This article is licensed under the
GNU Free Documentation License
. It uses material from the
Wikipedia article "Apollo Guidance Computer"
.