https://github.com/virtualagc/virtualagc
Revision 078c79d8734a9ed2860303a7c1662004284fe853 authored by Ron Burkey on 07 August 2022, 15:04:04 UTC, committed by Ron Burkey on 07 August 2022, 15:04:04 UTC
assembly listings from yaASM and yaLEMAP. Added some debugging messages to 'make install'. Tweaked debugging messages that VirtualAGC embeds in 'simulate'. Verified buildability in Mint 21, 20, 19, 17, and verified buildability using clang in Mint 17.
1 parent 6bb1acc
Tip revision: 078c79d8734a9ed2860303a7c1662004284fe853 authored by Ron Burkey on 07 August 2022, 15:04:04 UTC
Fixed a potential string-overflow bug in yaASM. Removed timestamps from
Fixed a potential string-overflow bug in yaASM. Removed timestamps from
Tip revision: 078c79d
ASSEMBLY_AND_OPERATION_INFORMATION.agc
### FILE="Main.annotation"
## Copyright: Public domain.
## Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
## Purpose: A section of Luminary revision 173.
## It is part of the reconstructed source code for the second
## (unflown) release of the flight software for the Lunar
## Module's (LM) Apollo Guidance Computer (AGC) for Apollo 14.
## The code has been recreated from a reconstructed copy of
## Luminary 178, as well as Luminary memo 167 (revision 1).
## It has been adapted such that the resulting bugger words
## exactly match those specified for Luminary 173 in NASA
## drawing 2021152N, which gives relatively high confidence
## that the reconstruction is correct.
## Reference: pp. 2-27
## Assembler: yaYUL
## Contact: Ron Burkey <info@sandroid.org>.
## Website: www.ibiblio.org/apollo/index.html
## Mod history: 2019-09-18 MAS Created from Luminary 178.
## 2019-09-21 MAS Removed VELOCITY5 (ZZ) scaling and gave
## FORVEL its original CC scaling.
## Page 2
# THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
# THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
# GUIDANCE SYSTEM OPERATIONS PLAN
# FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
# USING PROGRAM LUMINARY
# THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
# TECHNOLOGY 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS UNDER PROJECT55-238-70, SPONSORED BY THE MANNED
# SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065.
# THIS PROGRAM IS REFERRED TO AS LUMINARY 1D
# TABLE OF LOG CARDS
# ABSOLUTE ADDRESSES FOR UPDATE PROGRAM
# ASSEMBLY AND OPERATION INFORMATION
# TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
# CONTROLLED CONSTANTS
# INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
# FLAGWORD ASSIGNMENTS
# SUBROUTINE CALLS
# TABLE OF SUBROUTINE LOG SECTIONS
# LUMERASE
# ERASABLE ASSIGNMENTS
# LEMONAID
# INTERRUPT LEAD INS
# T4RUPT PROGRAM
# RCS FAILURE MONITOR
# DOWNLINK LISTS
# AGS INITIALIZATION
# FRESH START AND RESTART
# RESTART TABLES
# AOTMARK
# EXTENDED VERBS
# PINBALL NOUN TABLES
# LEM GEOMETRY
# IMU COMPENSATION PACKAGE
# R63
# ATTITUDE MANEUVER ROUTINE
# GIMBAL LOCK AVOIDANCE
# KALCMANU STEERING
# SYSTEM TEST STANDARD LEAD INS
# IMU PERFORMANCE TESTS 2
# IMU PERFORMANCE TESTS 4
## Page 3
# PINBALL GAMES BUTTONS AND LIGHTS
# R60,R62
# S-BAND ANTENNA FOR LM
# LEMP20S
# RADAR LEADIN ROUTINES
# P20-P25
# LEMP30S
# P30,P37
# P32-P35, P72-P75
# KISSING
# GROUND TRACKING DETERMINATION PROGRAM - P21
# P34-P35, P74-P75
# R31
# P76
# R30
# FLY
# BURN, BABY, BURN -- MASTER IGNITION ROUTINE
# P40-P47
# THE LUNAR LANDING
# THROTTLE CONTROL ROUTINES
# LUNAR LANDING GUIDANCE EQUATIONS
# P70-P71
# P12
# ASCENT GUIDANCE
# SERVICER
# LANDING ANALOG DISPLAYS
# FINDCDUW - GUIDAP INTERFACE
# LEMP50S
# P51-P53
# LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
# SKIPPER
# DOWN-TELEMETRY PROGRAM
# INTER-BANK COMMUNICATION
# INTERPRETER
# FIXED-FIXED CONSTANT POOL
# INTERPRETIVE CONSTANTS
# SINGLE PRECISION SUBROUTINES
# EXECUTIVE
# WAITLIST
# LATITUDE LONGITUDE SUBROUTINES
# PLANETARY INERTIAL ORIENTATION
# MEASUREMENT INCORPORATION
# CONIC SUBROUTINES
# INTEGRATION INITIALIZATION
# ORBITAL INTEGRATION
# INFLIGHT ALIGNMENT ROUTINES
# POWERED FLIGHT SUBROUTINES
# TIME OF FREE FALL
# AGC BLOCK TWO SELF-CHECK
# PHASE TABLE MAINTENANCE
## Page 4
# RESTARTS ROUTINE
# IMU MODE SWITCHING ROUTINES
# KEYRUPT, UPRUPT
# DISPLAY INTERFACE ROUTINES
# SERVICE ROUTINES
# ALARM AND ABORT
# UPDATE PROGRAM
# RTB OP CODES
# LMDAP
# T6-RUPT PROGRAMS
# DAP INTERFACE SUBROUTINES
# DAPIDLER PROGRAM
# P-AXIS RCS AUTOPILOT
# Q,R-AXIS RCS AUTOPILOT
# TJET LAW
# KALMAN FILTER
# TRIM GIMBAL CONTROL SYSTEM
# AOSTASK AND AOSJOB
# SPS BACK-UP RCS CONTROL
# SYMBOL TABLE LISTING
# UNREFERENCED SYMBOL LISTING
# ERASABLE & EQUALS CROSS-REFERENCE TABLE
# SUMMARY OF SYMBOL TABLE LISTINGS
# MEMORY TYPE & AVAILABLITY DISPLAY
# COUNT TABLE
# PARAGRAPHS GENERATED FOR THIS ASSEMBLY
# OCTAL LISTING
# OCCUPIED LOCATIONS TABLE
# SUBROS CALLED & PROGRAM STATUS
## Page 5
# VERB LIST FOR LUMINARY
# REGULAR VERBS
# 00 NOT IN USE
# 01 DISPLAY OCTAL COMP 1 IN R1
# 02 DISPLAY OCTAL COMP 2 IN R1
# 03 DISPLAY OCTAL COMP 3 IN R1
# 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
# 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
# 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
# 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
# 08
# 09
# 10
# 11 MONITOR OCTAL COMP 1 IN R1
# 12 MONITOR OCTAL COMP 2 IN R1
# 13 MONITOR OCTAL COMP 3 IN R1
# 14 MONITOR OCTAL COMP 1,2 IN R1,R2
# 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
# 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
# 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
# 18
# 19
# 20
# 21 LOAD COMPONENT 1 INTO R1
# 22 LOAD COMPONENT 2 INTO R2
# 23 LOAD COMPONENT 3 INTO R3
# 24 LOAD COMPONENT 1,2 INTO R1,R2
# 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
# 26
# 27 DISPLAY FIXED MEMORY
# 28
# 29
# 30 REQUEST EXECUTIVE
# 31 REQUEST WAITLIST
# 32 RECYCLE PROGRAM
# 33 PROCEED WITHOUT DSKY INPUTS
# 34 TERMINATE FUNCTION
# 35 TEST LIGHTS
# 36 REQUEST FRESH START
# 37 CHANGE PROGRAM (MAJOR MODE)
# 38
# 39
## Page 6
# EXTENDED VERBS
# 40 ZERO CDU-S
# 41 COARSE ALIGN CDU-S
# 42 FINE ALIGN IMU
# 43 LOAD IMU ATT ERROR METERS
# 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
# 45
# 46
# 47 INITIALIZE AGS (R47)
# 48 REQUEST DAP DATA LOAD ROUTINE (R03)
# 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
# 50 PLEASE PERFORM
# 51
# 52 MARK X-RETICLE
# 53 MARK Y-RETICLE
# 54 MARK X OR Y-RETICLE
# 55 INCREMENT AGC TIME (DECIMAL)
# 56 TERMINATE TRACKING (P20 + P25)
# 57 PERMIT LANDING RADAR UPDATES
# 58 INHIBIT LANDING RADAR UPDATES
# 59 COMMAND LR TO POSITION 2.
# 60 DISPLAY VEHICLE ATTITUDE RATES ON FDAI ERROR NEEDLES.
# 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
# 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
# 63 SAMPLE RADAR ONCE PER SECOND (R04).
# 64 REQUEST S-BAND ANTENNA ROUTINE (R05)
# 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
# 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
# 67 DISPLAY W MATRIX
# 68 DISABLE TERRAIN MODEL
# 69 CAUSE RESTART
# 70 UPDATE LIFTOFF TIME
# 71 UNIVERSAL UPDATE-BLOCK ADR
# 72 UNIVERSAL UPDATE-SINGLE ADR
# 73 UPDATE AGC TIME (OCTAL)
# 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
# 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
# 76 MINIMUM IMPULSE COMMAND MODE
# 77 RATE COMMAND AND ATTITUDE HOLD MODE
# 78 LR SPURIOUS RETURN TEST START (R77)
# 79 LR SPURIOUS RETURN TEST STOP
# 80 UPDATE LEM STATE VECTOR
# 81 UPDATE CSM STATE VECTOR
# 82 REQUEST ORBIT PARAM DISPLAY (R30)
# 83 REQUEST REND PARAM DISPLAY (R31)
# 84
# 85 DISPLAY RR LOS AZ AND ELEV
# 86
# 87
## Page 7
# 88
# 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
# 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
# 91 DISPLAY BANK SUM
# 92 OPERATE IMU PERFORMANCE TEST (P07)
# 93 ENABLE W MATRIX INITIALIZATION
# 94
# 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
# 96 INTERRUPT INTEGRATION AND GO TO POO
# 97 PERFORM ENGINE FAIL PROCEDURE
# 98
# 99 PLEASE ENABLE ENGINE
## Page 8
# IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
# CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
# SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
# IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23
# MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
# ABOVE SCALE TYPES.
# THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
# EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
# NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
# 00 NOT IN USE
# 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH
# 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH
# 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP XXX.XX DEG FOR EACH
# 04 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
# 05 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
# 06 OPTION CODE 3COMP OCTAL ONLY FOR EACH
# LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
# 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
# ONES FOR BITS TO BE MODIFIED
# 1 TO SET OR 0 TO RESET SELECTED BITS
# 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
# 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
# 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
# 11 TIG OF CSI 3COMP 00XXX. HRS DEC ONLY
# 000XX. MIN MUST LOAD 3 COMPS
# 0XX.XX SEC
# 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
# (USED BY EXTENDED VERBS ONLY)
# 13 TIG OF CDH 3COMP 00XXX. HRS DEC ONLY
# 000XX. MIN MUST LOAD 3 COMPS
# 0XX.XX SEC
# 14 CHECKLIST 3COMP XXXXX. FOR EACH
# (USED BY EXTENDED VERBS ONLY)
# (NOUN 25 IS PASTED AFTER DISPLAY)
# 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
# 16 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
# (USED BY EXTENDED VERBS ONLY) 000XX. MIN MUST LOAD 3 COMPS
# 0XX.XX SEC
# 17 SPARE
# 18 AUTO MANEUVER BALL ANGLES 3COMP XXX.XX DEG FOR EACH
# 19 SPARE
# 20 ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
# 21 PIPAS 3COMP XXXXX. PULSES FOR EACH
# 22 NEW ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
# 23 SPARE
# 24 DELTA TIME FOR AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
# 000XX. MIN MUST LOAD 3 COMPS
# 0XX.XX SEC
## Page 9
# 25 CHECKLIST 3COMP XXXXX. FOR EACH
# (USED WITH PLEASE PERFORM ONLY)
# 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
# 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX.
# 28 SPARE
# 29 SPARE
# 30 SPARE
# 31 SPARE
# 32 TIME FROM PERIGEE 3COMP 00XXX. HRS DEC ONLY
# 000XX. MIN MUST LOAD 3 COMPS
# 0XX.XX SEC
# 33 TIME OF IGNITION 3COMP 00XXX. HRS DEC ONLY
# 000XX. MIN MUST LOAD 3 COMPS
# 0XX.XX SEC
# 34 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
# 000XX. MIN MUST LOAD 3 COMPS
# 0XX.XX SEC
# 35 TIME FROM EVENT 3COMP 00XXX. HRS DEC ONLY
# 000XX. MIN MUST LOAD 3 COMPS
# 0XX.XX SEC
# 36 TIME OF AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
# 000XX. MIN MUST LOAD 3 COMPS
# 0XX.XX SEC
# 37 TIG OF TPI 3COMP 00XXX. HRS DEC ONLY
# 000XX. MIN MUST LOAD 3 COMPS
# 0XX.XX SEC
# 38 TIME OF STATE BEING INTEGRATED 3COMP 00XXX. HRS DEC ONLY
# 000XX. MIN MUST LOAD 3 COMPS
# 0XX.XX SEC
# 39 SPARE
## Page 10
# MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
# 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
# VG, XXXX.X FT/SEC
# DELTA V (ACCUMULATED) XXXX.X FT/SEC
# 41 TARGET AZIMUTH, 2COMP XXX.XX DEG (FOR SYSTEM TEST)
# ELEVATION XX.XXX DEG
# 42 APOGEE, 3COMP XXXX.X NAUT MI DEC ONLY
# PERIGEE, XXXX.X NAUT MI
# DELTA V (REQUIRED) XXXX.X FT/SEC
# 43 LATITUDE, 3COMP XXX.XX DEG DEC ONLY
# LONGITUDE, XXX.XX DEG
# ALTITUDE XXXX.X NAUT MI
# 44 APOGEE, 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
# PERIGEE, XXXX.X NAUT MI
# TFF XXBXX MIN/SEC
# 45 MARKS, 3COMP XXXXX. NO LOAD, DEC ONLY
# TFI OF NEXT BURN XXBXX MIN/SEC
# MGA XXX.XX DEG
# 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
# 47 LEM WEIGHT, 2COMP XXXXX. LBS DEC ONLY
# CSM WEIGHT XXXXX. LBS
# 48 GIMBAL PITCH TRIM, 2COMP XXX.XX DEG DEC ONLY
# GIMBAL ROLL TRIM XXX.XX DEG
# 49 DELTA R, 3COMP XXXX.X NAUT MI DEC ONLY
# DELTA V, XXXX.X FT/SEC
# RADAR DATA SOURCE CODE XXXXX.
# 50 SPARE
# 51 S-BAND ANTENNA ANGLES PITCH 2COMP XXX.XX DEG DEC ONLY
# YAW XXX.XX DEG
# 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG
# 53 SPARE
# 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
# RANGE RATE, XXXX.X FT/SEC
# THETA XXX.XX DEG
# 55 NO. OF APSIDAL CROSSINGS 3COMP XXXXX. DEC ONLY
# ELEVATION ANGLE XXX.XX DEG
# CENTRAL ANGLE OF PASSIVE VEHICLE XXX.XX DEG
# 56 RR LOS AZIMUTH 2COMP XXX.XX DEG
# ELEVATION XXX.XX DEG
# 57 SPARE
# 58 PERIGEE ALT (POST TPI) 3COMP XXXX.X NAUT MI DEC ONLY
# DELTA V TPI XXXX.X FT/SEC
# DELTA V TPF XXXX.X FT/SEC
# 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY
# 60 FORWARD VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
# ALTITUDE RATE XXXX.X FT/SEC
# COMPUTED ALTITUDE XXXXX. FEET
# 61 TIME TO GO IN BRAKING PHASE 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
# TIME FROM IGNITION XXBXX MIN/SEC
## Page 11
# CROSS RANGE DISTANCE XXXX.X NAUT MI
# 62 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC NO LOAD, DEC ONLY
# TIME FROM IGNITION XXBXX MIN/SEC
# DELTA V (ACCUMULATED) XXXX.X FT/SEC
# 63 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
# ALTITUDE RATE XXXX.X FT/SEC
# COMPUTED ALTITUDE XXXXX. FEET
# 64 TIME LEFT FOR REDESIGNATION- LPD ANGLE 3COMP XXBXX NO LOAD, DEC ONLY
# ALTITUDE RATE XXXX.X FT/SEC
# COMPUTED ALTITUDE XXXXX. FEET
# 65 SAMPLED AGC TIME 3COMP 00XXX. HRS DEC ONLY
# (FETCHED IN INTERRUPT) 000XX. MIN MUST LOAD 3 COMPS
# 0XX.XX SEC
# 66 LR RANGE 2COMP XXXXX. FEET NO LOAD, DEC ONLY
# POSITION +0000X
# 67 LRVX 3COMP XXXXX. FT/SEC
# LRVY XXXXX. FT/SEC
# LRVZ XXXXX. FT/SEC
# 68 SLANT RANGE TO LANDING SITE 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
# TIME TO GO IN BRAKING PHASE XXBXX MIN/SEC
# LR ALTITUDE - COMPUTED ALTITUDE XXXXX. FEET
# 69 LANDING SITE CORRECTION, Z-COMPONENT 3COMP XXXXX. FEET DEC ONLY
# LANDING SITE CORRECTION, Y-COMPONENT XXXXX. FEET
# LANDING SITE CORRECTION, X-COMPONENT XXXXX. FEET
# 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
# 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
# 72 RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
# SHAFT ANGLE XXX.XX DEG
# 73 NEW RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
# SHAFT ANGLE XXX.XX DEG
# 74 TIME FROM IGNITION 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
# YAW AFTER VEHICLE RISE XXX.XX DEG
# PITCH AFTER VEHICLE RISE XXX.XX DEG
# 75 DELTA ALTITUDE CDH 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
# DELTA TIME (CDH-CSI OR TPI-CDH) XXBXX MIN/SEC
# DELTA TIME (TPI-CDH OR TPI-NOMTPI) XXBXX MIN/SEC
# 76 DESIRED HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
# DESIRED RADIAL VELOCITY XXXX.X FT/SEC
# CROSS-RANGE DISTANCE XXXX.X NAUT MI
# 77 TIME TO ENGINE CUTOFF 2COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
# VELOCITY NORMAL TO CSM PLANE XXXX.X FT/SEC
# 78 RR RANGE 3COMP XXX.XX NAUT MI NO LOAD, DEC ONLY
# RANGE RATE XXXXX. FT/SEC
# TIME FROM IGNITION XXBXX MIN/SEC
# 79 CURSOR ANGLE 3COMP XXX.XX DEG DEC ONLY
# SPIRAL ANGLE XXX.XX DEG
# POSITION CODE XXXXX.
# 80 DATA INDICATOR, 2COMP XXXXX.
# OMEGA XXX.XX DEG
# 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
## Page 12
# 82 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
# 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
# 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
# 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
# 86 VG (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
# 87 BACKUP OPTICS LOS AZIMUTH 2COMP XXX.XX DEG
# ELEVATION XXX.XX DEG
# 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY
# 89 LANDMARK LATITUDE 3COMP XX.XXX DEG DEC ONLY
# LONGITUDE/2 XX.XXX DEC
# ALTITUDE XXX.XX NAUT MI
# 90 Y 3COMP XXX.XX NM DEC ONLY
# Y DOT XXXX.X FPS
# PSI XXX.XX DEG
# 91 ALTITUDE 3COMP XXXXXB. NAUT MI
# VELOCITY XXXXX. FT/SEC
# FLIGHT PATH ANGLE XXX.XX DEG
# 92 PCT FTP(10,5KLB) AT PRESENT THRUST 3COMP XXXXX.
# ALTITUDE RATE XXXX.X FT/SEC
# COMPUTED ALTITUDE XXXXX.FEET
# 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
# 94 SPARE
# 95 SPARE
# 96 SPARE
# 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH
# 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX.
# .XXXXX
# XXXXX.
# 99 RMS IN POSITION 3COMP XXXXX.FT DEC ONLY
# RMS IN VELOCITY XXXX.X FT/SEC
# RMS IN BIAS XX.XXX RADIANS
## Page 13
# REGISTERS AND SCALING FOR NORMAL NOUNS
# NOUN REGISTER SCALE TYPE
# 00 NOT IN USE
# 01 SPECIFY ADDRESS B
# 02 SPECIFY ADDRESS C
# 03 SPECIFY ADDRESS D
# 04 DSPTEM1 H
# 05 DSPTEM1 H
# 06 OPTION1 A
# 07 XREG A
# 08 ALMCADR A
# 09 FAILREG A
# 10 SPECIFY CHANNEL A
# 11 TCSI K
# 12 OPTIONX A
# 13 TCDH K
# 14 DSPTEMX C
# 15 INCREMENT ADDRESS A
# 16 DSPTEMX K
# 17 SPARE
# 18 FDAIX D
# 19 SPARE
# 20 CDUX D
# 21 PIPAX C
# 22 THETAD D
# 23 SPARE
# 24 DSPTEM2 +1 K
# 25 DSPTEM1 C
# 26 DSPTEM1 A
# 27 SMODE C
# 28 SPARE
# 29 SPARE
# 30 SPARE
# 31 SPARE
# 32 -TPER K
# 33 TIG K
# 34 DSPTEM1 K
# 35 TTOGO K
# 36 TIME2 K
# 37 TTPI K
# 38 TET K
# 39 SPARE
## Page 14
# REGISTERS AND SCALING FOR MIXED NOUNS
# NOUN COMP REGISTER SCALE TYPE
# 40 1 TTOGO L
# 2 VGDISP S
# 3 DVTOTAL S
# 41 1 DSPTEM1 D
# 2 DSPTEM1 +1 E
# 42 1 HAPO Q
# 2 HPER Q
# 3 VGDISP S
# 43 1 LAT H
# 2 LONG H
# 3 ALT Q
# 44 1 HAPOX Q
# 2 HPERX Q
# 3 TFF L
# 45 1 TRKMKCNT C
# 2 TTOGO L
# 3 +MGA H
# 46 1 DAPDATR1 A
# 47 1 LEMMASS KK
# 2 CSMMASS KK
# 48 1 PITTIME NN
# 2 ROLLTIME NN
# 49 1 R22DISP Q
# 2 R22DISP +2 S
# 3 WHCHREAD C
# 50 SPARE
# 51 1 ALPHASB H
# 2 BETASB H
# 52 1 ACTCENT H
# 53 SPARE
# 54 1 RANGE JJ
# 2 RRATE S
# 3 RTHETA H
# 55 1 NN C
# 2 ELEV H
# 3 CENTANG H
# 56 1 RR-AZ H
# 2 RR-ELEV H
# 57 SPARE
# 58 1 POSTTPI Q
# 2 DELVTPI S
# 3 DELVTPF S
# 59 1 DVLOS S
# 2 DVLOS +2 S
# 3 DVLOS +4 S
# 60 1 FORVEL CC
## Page 15
# 2 HDOTDISP S
# 3 HCALC1 RR
# 61 1 TTFDISP L
# 2 TTOGO L
# 3 OUTOFPLN QQ
# 62 1 ABVEL S
# 2 TTOGO L
# 3 DVTOTAL S
# 63 1 ABVEL S
# 2 HDOTDISP S
# 3 HCALC1 RR
# 64 1 FUNNYDSP PP
# 2 HDOTDISP S
# 3 HCALC RR
# 65 1 SAMPTIME K
# 2 SAMPTIME K
# 3 SAMPTIME K
# 66 1 RSTACK +6 W
# 2 CHANNEL 33 TT
# 67 1 RSTACK X
# 2 RSTACK +2 Y
# 3 RSTACK +4 Z
# 68 1 RANGEDSP QQ
# 2 TTFDISP L
# 3 DELTAH RR
# 69 1 DLANDZ RR
# 2 DLANDY RR
# 3 DLANDX RR
# 70 1 AOTCODE A
# 2 AOTCODE +1 A
# 3 AOTCODE +2 A
# 71 1 AOTCODE A
# 2 AOTCODE +1 A
# 3 AOTCODE +2 A
# 72 1 CDUT WW
# 2 CDUS D
# 73 1 TANG WW
# 2 TANG +1 D
# 74 1 TTOGO L
# 2 YAW H
# 3 PITCH H
# 75 1 DIFFALT Q
# 2 T1TOT2 L
# 3 T2TOT3 L
# 76 1 ZDOTD S
# 2 RDOTD S
# 3 XRANGE Q
# 77 1 TTOGO L
# 2 YDOT S
# 78 1 DNRRANGE U
## Page 16
# 2 DNRRDOT V
# 3 TTOTIG L
# 79 1 CURSOR D
# 2 SPIRAL D
# 3 POSCODE C
# 80 1 DATAGOOD C
# 2 OMEGAD H
# 81 1 DELVLVC S
# 2 DELVLVC +2 S
# 3 DELVLVC +4 S
# 82 1 DELVLVC S
# 2 DELVLVC +2 S
# 3 DELVLVC +4 S
# 83 1 DELVIMU S
# 2 DELVIMU +2 S
# 3 DELVIMU +4 S
# 84 1 DELVOV S
# 2 DELVOV +2 S
# 3 DELVOV +4 S
# 85 1 VGBODY S
# 2 VGBODY +2 S
# 3 VGBODY +4 S
# 86 1 DELVLVC S
# 2 DELVLVC +2 S
# 3 DELVLVC +4 S
# 87 1 AZ D
# 2 EL D
# 88 1 STARAD B
# 2 STARAD +2 B
# 3 STARAD +4 B
# 89 1 LANDLAT G
# 2 LANDLONG G
# 3 LANDALT JJ
# 90 1 RANGE JJ
# 2 RRATE S
# 3 RTHETA H
# 91 1 P21ALT Q (MEMORY/100 TO DIPLAY TENS N.M.)
# 2 P21VEL P
# 3 P21GAM H
# 92 1 THRDISP C
# 2 HDOTDISP S
# 3 HCALC1 RR
# 93 1 OGC G
# 2 OGC +2 G
# 3 OGC +4 G
# 94 SPARE
# 95 SPARE
# 96 SPARE
# 97 1 DSPTEM1 C
# 2 DSPTEM1 +1 C
## Page 17
# 3 DSPTEM1 +2 C
# 98 1 DSPTEM2 C
# 2 DSPTEM2 +1 B
# 3 DSPTEM2 +2 C
# 99 1 WWPOS XX
# 2 WWVEL YY
# 3 WWBIAS AAA
## Page 18
# NOUN SCALES AND FORMATS
# -SCALE TYPE- PRECISION
# UNITS DECIMAL FORMAT -- AGC FORMAT
# ------------ -------------- -- ----------
# -A-
# OCTAL XXXXX SP OCTAL
# -B- -14
# FRACTIONAL .XXXXX SP BIT 1 = 2 UNITS
# (MAX .99996)
# -C-
# WHOLE XXXXX. SP BIT 1 = 1 UNIT
# (MAX 16383.)
# -D- 15
# CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360/2 DEGREES
# (MAX 359.99) (USES 15 BITS FOR MAGNI-
# TUDE AND 2-S COMP.)
# -E- 14
# ELEVATION DEGREES XX.XXX DEGREES SP BIT 1 = 90/2 DEGREES
# (MAX 89.999)
# -F- 14
# DEGREES (180) XXX.XX DEGREES SP BIT 1 = 180/2 DEGREES
# (MAX 179.99)
# -G-
# DP DEGREES(90) XX.XXX DEGREES DP BIT 1 OF LOW REGISTER =
# 28
# 360/2 DEGREES
# -H-
# DP DEGREES (360) XXX.XX DEGREES DP BIT 1 OF LOW REGISTER =
# 28
# (MAX 359.99) 360/2 DEGREES
## Page 19
# -K-
# TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER =
# 000XX. MIN -2
# 0XX.XX SEC 10 SEC
# (DECIMAL ONLY.
# MAX MIN COMP=59
# MAX SEC COMP=59.99
# MAX CAPACITY=745 HRS
# 39 MINS
# 14.55 SECS.
# WHEN LOADING, ALL 3
# COMPONENTS MUST BE
# SUPPLIED.)
# -L-
# TIME (MIN/SEC) XXBXX MIN/SEC DP BIT 1 OF LOW REGISTER =
# (B IS A BLANK -2
# POSITION, DECIMAL 10 SEC
# ONLY, DISPLAY OR
# MONITOR ONLY. CANNOT
# BE LOADED.
# MAX MIN COMP=59
# MAX SEC COMP=59
# VALUES GREATER THAN
# 59 MIN 59 SEC
# ARE DISPLAYED AS
# 59 MIN 59 SEC.)
# -M- -2
# TIME (SEC) XXX.XX SEC SP BIT 1 = 10 SEC
# (MAX 163.83)
# -N-
# TIME(SEC) DP XXX.XX SEC DP BIT 1 OF LOW REGISTER =
# -2
# 10 SEC
# -P-
# VELOCITY 2 XXXXX. FEET/SEC DP BIT 1 OF HIGH REGISTER =
# (MAX 41994.) -7
# 2 METERS/CENTI-SEC
# -Q-
# POSITION 4 XXXX.X NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
# 2 METERS
# -S-
# VELOCITY 3 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
# -7
# 2 METERS/CENTI-SEC
## Page 20
# -T- -2
# G XXX.XX G SP BIT 1 = 10 G
# (MAX 163.83)
# -U-
# RENDEZVOUS XXX.XX NAUT MI SP USES 15 BITS FOR UNSIGNED
# RADAR RANGE (DECIMAL ONLY. MAGNITUDE.
# DISPLAY OR MONITOR BIT 1 = 9.38 FEET
# ONLY. CANNOT BE
# LOADED.)
# -V-
# RENDEZVOUS XXXXX. FEET/SEC SP USES 15 BITS FOR UNSIGNED
# RADAR RANGE RATE (DECIMAL ONLY. MAGNITUDE.
# DISPLAY OR MONITOR BIT 1 = -.6278 FEET/SEC
# ONLY. CANNOT BE
# LOADED.
# BIAS OF 17000 COUNTS
# SUBTRACTED BEFORE
# DISPLAY.)
# -W-
# LANDING RADAR XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
# ALTITUDE WORD = 1.079 FEET
# -X-
# LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
# VELX WORD = -.6440 FEET/SEC
# -Y-
# LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
# VELY WORD = 1.212 FEET/SEC
# -Z-
# LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
# VELZ WORD = .8668 FEET/SEC
# -AA-
# INITIAL/FINAL XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
# ALTITUDE WORD = 2.345 FEET
# -BB-
# ALTITUDE RATE XXXXX. FEET/SEC SP LOW ORDER BIT = .5
# (MAX 08191.) FEET/SEC
# -CC-
# FORWARD/LATERAL XXXX.X FEET/SEC SP LOW ORDER BIT = .5571
# VELOCITY (MAX 09126.) FEET/SEC
# -DD-
## Page 21
# ROTATIONAL HAND XXXXX. DEG/SEC SP FRACTIONAL PART OF PI RAD
# CONTROLLER ANGULAR (MAX 00044.) 4 SEC
# RATES
# -EE-
# OPTICAL TRACKER XXX.XX DEG. DP LOW ORDER BIT OF LOW ORDER
# AZIMUTH ANGLE 15
# WORD = 360/2 DEGREES
# -JJ-
# POSITION5 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
# 2 METERS
# -KK- 16
# WEIGHT2 XXXXX. LBS SP FRACTIONAL PART OF 2 KG
# -NN-
# TRIM DEGREES 2 XXX.XX DEG SP BIT 1=.01SEC(TIME)
# (MAX 032.76)
# -PP-
# 2 INTEGERS +XXBYY DP BIT 1 OF HIGH REGISTER =
# (B IS A BLANK 1 UNIT OF XX
# POSITION. DECIMAL BIT 1 OF LOW REGISTER =
# ONLY, DISPLAY OR 1 UNIT OF YY
# MONITOR ONLY. CANNOT (EACH REGISTER MUST
# BE LOADED.) CONTAIN A POSITIVE INTEGER
# (MAX 99B99) LESS THAN 100)
# -QQ-
# POSITION7 XXXX.X NAUT MI DP BIT 1 OF LOW REGISTER =
# (MAX 9058.9) -4
# 2 METERS
# -RR-
# COMPUTED ALTITUDE XXXXX. FEET DP BIT 1 OF LOW REGISTER =
# -4
# 2 METERS
# -SS-
# DP DEGREES XXXX.X DEGREES DP BIT 1 OF HIGH REGISTER =
# 1 DEGREE
# -TT-
# LANDING RADAR +0000X CHANNEL 33,BIT 6=NOT POSIT. 1
# POSITION (DECIMAL ONLY. CHANNEL 33,BIT 7=NOT POSIT. 2
# DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
# ONLY. CANNOT BE X = 2 FOR LR POSITION 2
# LOADED.)
# -WW- 15
## Page 22
# 360-CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360 - (360/2 )
# (MAX 359.99) DEGREES
# (USES 15 BITS FOR MAGNI-
# TUDE AND 2-S COMP.)
# -XX-
# POSITION 9 XXXXX. FEET DP BIT 1 OF LOW REGISTER =
# -9
# 2 METERS
# -YY-
# VELOCITY 4 XXXX.X FEET/SEC DP FRACTIONAL PART OF
# (MAX 328.0) METERS/CENTI-SEC
# -AAA-
# RADIANS XX.XXX RADIANS DP BIT 1 OF HIGH REGISTER =
# (MAX 31.999) -9
# 2 RADIANS
# THAT-S ALL ON THE NOUNS.
## Page 23
# ALARM CODES FOR LUMINARY
# *9 *18 *60 COLUMN
# CODE * TYPE SET BY
# 00107 MORE THAN 5 MARK PAIRS AOTMARK
# 00111 MARK MISSING AOTMARK
# 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
# 00113 NO INBITS AOTMARK
# 00114 MARK MADE BUT NOT DESIRED AOTMARK
# 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
# 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING
# 00206 + GIMBAL LOCK.
# 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
# 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51, P57
# 00211 COARSE ALIGN ERROR IMU MODE SWITCH
# 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH,T4RPT
# 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
# 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
# 00217 BAD RETURN FROM IMUSTALL P51,P52,P57
# 00220 IMU NOT ALIGNED - NO REFSMMAT R02,R47
# 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
# FINDCDUW
# 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
# 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
# 00405 TWO STARS NOT AVAILABLE P52
# 00421 W-MATRIX OVERFLOW INTEGRV
# 00501 P RADAR ANTENNA OUT OF LIMITS R23
# 00502 BAD RADAR GIMBAL ANGLE INPUT V41N72
# 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V41N72
# 00510 RADAR AUTO DESCRETE NOT PRESENT R25
# 00511 LR ANTENNA MOVED AND NOT REPOSITIONED SERVICER
# 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
# 00515 RR CDU FAIL DISCRETE PRESENT R25
# 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
# 00522 LANDING RADAR POSITION CHANGE R04
# 00523 LR ANTENNA DIDN'T ACHIEVE POSITION 2 V59 IN V60)
# 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
# 00526 RANGE GREATER THAN 400 NAUTICAL MILES P20
# 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21,R24
# LUNAR SURFACE
# OR VEHICLE MANEUVER REQUIRED R24 (20)
# 00530 P LOS NOT IN MODE2 COVERAGE R21
# ON LUNAR SURFACE AFTER 600 SECS.
# 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
# 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32,P72,
# 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32,P72,
# 00603 CSI TO CDH TIME LT TMIN12 P32,P72,P33,P73
## Page 24
# 00604 CDH TO TPI TIME LT TMIN23 P32,P72,
# OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
# 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
# 00606 DV EXCEEDS MAXIMUM P32,P72,
# 00611 NO TIG FOR GIVEN ELEV ANGLE P34,P74
# 00701 ILLEGAL OPTION CODE SELECTED P57
# 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
# 01102 AGC SELF TEST ERROR SELF CHECK
# 01105 DOWNLINK TOO FAST T4RUPT
# 01106 UPLINK TOO FAST T4RUPT
# 01107 PHASE TABLE FAILURE. ASSUME RESTART
# ERASABLE MEMORY IS SUSPECT. RESTART
# 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
# 01406 BAD RETURN FROM ROOTPSRS DESCENT GUIDANCE EQS.
# 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
# .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
# VECTOR.) S40.8
# 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
# 01412 DESCENT IGNALG NOT CONVERGING P63
# 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
# 01600 OVERFLOW IN DRIFT TEST IMU 4
# 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
# 01601 IMU 4 (LEM)
# 01703 IGNITION TIME SLIPPED MIDTOAVE
# 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
# CONFIGURATION P40, P42
# 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
# 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
# 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
# 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
# 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
# 04777 ICDU , PIPA FAILS CAUSED THE ISS WARNING T4RUPT
# 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
# 10777 IMU , PIPA FAILS CAUSED THE ISS WARNING T4RUPT
# 13777 IMU , ICDU FAILS CAUSED THE ISS WARNING T4RUPT
# 14777 IMU,ICDU,PIPA FAILS CAUSED ISS WARNING T4RUPT
# THE FOLLOWING CODES INDICATE THE MORE SERIOUS POODOO ABORTS THAT RESULT
# IN THE PROGRAM GOING TO ROO.
# 20105 AOTMARK SYSTEM IN USE AOTMARK
# 20430 ACCELERATION OVERFLOW IN INTEGRATION ORBITAL INTEGRATION
# 20607 NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET, TIMERAD
# 21103 UNUSED CCS BRANCH EXECUTED ABORT
# 21204 WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
# CALLED WITH ZERO OR NEGATIVE DELTA-TIME
# 21302 SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
# 21406 BAD RETURN FROM ROOTPSRS IGNITION ALGORITHMN
# 21501 KEYBOARD AND DISPLAY ALARM DURING PINBALL
# INTERNAL USE(NVSUB).ABORT
## Page 25
# THE FOLLOWING CODES INDICATE A BAILOUT ABORT THAT RESULTS IN A SOFTWARE
# RESTART
# 31104 DELAY ROUTINE BUSY EXEC
# 31201 EXECUTIVE OVERFLOW-NO VAC AREAS EXEC
# 31202 EXECUTIVE OVERFLOW-NO CORE SETS EXEC
# 31203 WAITLIST OVERFLOW-TOO MANY TASKS WAITLIST
# 31206 SECOND JOB ATTEMPTS TO GO TO SLEEP VIA PINBALL
# KEYBOARD AND DISPLAY PROGRAM
# 31207 NO VAC AREAS FOR MARKS AOTMARK
# 31210 TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
# 31211 ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
# 31502 TWO PRIO DISPLAYS WAITING DSP INTRFCE
# 32000 DAP STILL IN PROGRESS AT NEXT TIME5 RUPT DAP
## Page 26
# CHECKLIST CODES FOR LUMINARY
# *9 *17 *26 *9 COLUMN
# R1CODE ACTION TO BE EFFECTED PROGRAM
# 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
# 00014 PROCEED DO IMU FINE ALIGN ROUTINE P51,P63,P57
# 00014 ENTER DO LANDING SITE DETERMINATION(N89DISP) P57OPTION2
# 00015 PERFORM CELESTIAL BODY ACQUISITION R51,P51
# 00062 SWITCH AGC POWER DOWN P06
# 00201 SWITCH RR MODE TO AUTOMATIC P20,P22,R04
# 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12,P42,P71
# ALSO THR CONT TO AUTO P40,P63,P70
# 00205 PERFORM MANUAL ACQUISITION OF RR R23
# 00500 SWITCH LR ANTENNA TO POSITION 1 P63
# SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
# PERFORM DENOTES START OR END OF A TASK
# KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
## Page 27
# OPTION CODES FOR LUMINARY
# THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
# CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
# ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
# *9 *17 *52 *11 *25 COLUMN
# OPTION
# CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
# 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
# 4=LAND SITE
# 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
# 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
# 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
# 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
# 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
# 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
# 2=TWO BODIES 3=ONE BODY + G
# 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
# ORBIT TO PASS OVER LM
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