Statements (163)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:computer
gptkb:sensors |
| gptkbp:availability |
Triple modular redundancy
|
| gptkbp:average_temperature |
-40 to 85 ° C
|
| gptkbp:clock_speed |
1 MHz
|
| gptkbp:components |
gptkb:software
gptkb:computer |
| gptkbp:contributed_to |
gptkb:Mars_Rover
|
| gptkbp:data_usage |
1 MHz
|
| gptkbp:designed_by |
gptkb:MIT_Instrumentation_Laboratory
|
| gptkbp:designed_for |
spacecraft navigation
|
| gptkbp:developed_by |
gptkb:MIT_Instrumentation_Laboratory
1960s |
| gptkbp:development |
gptkb:Charles_Draper
1960s approximately 5 years |
| gptkbp:development_cost |
$7 million
$150 million |
| gptkbp:economic_impact |
influenced future spacecraft design
|
| gptkbp:error_handling |
Hamming code
parity bits Parity bits |
| gptkbp:features |
real-time computing
|
| gptkbp:first_flight |
gptkb:Apollo_17
gptkb:Apollo_7 gptkb:Apollo_11 |
| gptkbp:first_introduced |
gptkb:Apollo_11
|
| gptkbp:function |
gptkb:navigation
guidance control |
| gptkbp:group_size |
over 100 engineers
|
| gptkbp:historical_significance |
first computer used in space missions
|
| gptkbp:home_port |
gptkb:DSKY
gptkb:keyboard Display screen |
| https://www.w3.org/2000/01/rdf-schema#label |
Apollo Guidance Computer
|
| gptkbp:influenced |
Modern avionics
modern computing |
| gptkbp:influenced_by |
Early computers
previous guidance systems |
| gptkbp:innovation |
integrated circuits
|
| gptkbp:input_data |
astronomical data
|
| gptkbp:input_output |
gptkb:DSKY
gptkb:navigation gptkb:keyboard Dials and switches display screen Lights and sounds display lights |
| gptkbp:interface |
digital
Digital display |
| gptkbp:introduced_in |
gptkb:1966
|
| gptkbp:is_tested_for |
gptkb:MIT_Instrumentation_Laboratory
|
| gptkbp:key_feature |
Real-time computing
Integrated circuits Low power consumption Performance monitoring Compact size High reliability Software updates Fault tolerance Modular design Lightweight construction System diagnostics Control algorithms Simulation capabilities Digital logic Maintenance support User training programs Documentation availability User programmability Analog inputs Digital outputs Navigation algorithms Telemetry capabilities |
| gptkbp:legacy |
influenced modern avionics
|
| gptkbp:manufacturer |
gptkb:Raytheon
|
| gptkbp:memory_type |
core memory
core rope memory |
| gptkbp:mission |
gptkb:Apollo_14
gptkb:Apollo_16 gptkb:Apollo_15 gptkb:Apollo_17 gptkb:Apollo_12 Lunar landing Lunar orbit Earth orbit |
| gptkbp:notable_feature |
gptkb:cloud_storage
research papers advanced algorithms compact size data formats development tools fault tolerance low power consumption modular design patents real-time data processing real-time processing software updates technical specifications user-friendly interface communication protocols signal processing system diagnostics hardware upgrades lightweight design user manuals high reliability system integration testing procedures control algorithms error detection project management techniques redundancy user training programs redundant systems team collaboration tools simulation capabilities navigation algorithms documentation standards multi-tasking capabilities autonomous operation manual override self-diagnostics telemetry capabilities programmable logic input/output interfaces guidance algorithms user programmability synchronization capabilities self-checking capabilities |
| gptkbp:operating_system |
gptkb:AGC_software
AGC Monitor AGC Executive |
| gptkbp:power_consumption |
55 watts
25 watts |
| gptkbp:processor |
custom integrated circuits
custom-built processor Custom integrated circuits |
| gptkbp:produces |
over 100
|
| gptkbp:programming_language |
AGC assembly language
|
| gptkbp:protocol |
Serial communication
serial communication |
| gptkbp:ram |
64 KB
|
| gptkbp:reliability |
gptkb:High
high |
| gptkbp:storage |
Magnetic tape
|
| gptkbp:successor |
gptkb:Apollo_Lunar_Module_Guidance_Computer
Space Shuttle Guidance Computer |
| gptkbp:used_for |
gptkb:navigation
control |
| gptkbp:used_in |
gptkb:Apollo_program
gptkb:Lunar_Module gptkb:Command_Line_Interface |
| gptkbp:user_interface |
Graphical user interface
text-based interface |
| gptkbp:user_manual |
Apollo Guidance Computer User's Manual
|
| gptkbp:weight |
32 kg
70 pounds |
| gptkbp:bfsParent |
gptkb:Columbia_command_module
gptkb:MIT_Instrumentation_Laboratory |
| gptkbp:bfsLayer |
5
|