AGC EXECUTIVE SIMULATOR MIT IL / HAMILTON 1969

DSKY Primary Display P64 APPROACH
TEMP
PRIO DISP
RESTART
PROG ALARM
OPR ERR
VERB
16
NOUN
68
PROG
64
R1 (ALT FT): +03240
R2 (V/FPS): -00042
R3 (ALARM): NONE
Scheduler Architecture HAMILTON ASYNC
Hamilton Priority Exec: Preemptive core sets drop low-priority telemetry/radar traps during CPU overload (>100%), keeping DAP thrusters & guidance alive.
Mission Scenarios
Lunar Module Descent Trajectory GUIDANCE LOCKED
AGC 8-Slot Core Set Memory (Vac Area / Job Table) 7/8 SLOTS
SLOT JOB NAME PRIO RATE CYCLES STATE
CPU Load & Cycle Stealing Real-Time Telemetry
Workload Injector

Historical 15% bit-stealing counter trap (12.8 kHz phase lock sync bug).

Landing Radar Interrupt:
DAP Thruster Control:
DSKY Display Refresh:
Telemetry Downlink:
Mission Flight Telemetry
CPU UTILIZATION
114.2%
CORE SATURATION
7 / 8
DROPPED JOBS (SHED)
42
RESTARTS (1202)
3
DAP THRUS. LATENCY
19.8 ms
PROPELLANT LEFT
4.8%
Data Export & Logs
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