https://github.com/virtualagc/virtualagc
Revision 3577d0b1de1ac147c1710524517c563b2bfe231c authored by Ronald Burkey on 30 May 2021, 19:14:00 UTC, committed by GitHub on 30 May 2021, 19:14:00 UTC
Issue 1143: Fix various symbol name and other minor typos
Tip revision: 3577d0b1de1ac147c1710524517c563b2bfe231c authored by Ronald Burkey on 30 May 2021, 19:14:00 UTC
Merge pull request #1147 from smithery1/Issue/1143
Merge pull request #1147 from smithery1/Issue/1143
Tip revision: 3577d0b
ASSEMBLY_AND_OPERATION_INFORMATION.agc
### FILE="Main.annotation"
## Copyright: Public domain.
## Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
## Purpose: The main source file for Luminary revision 069.
## It is part of the source code for the original release
## of the flight software for the Lunar Module's (LM) Apollo
## Guidance Computer (AGC) for Apollo 10. The actual flown
## version was Luminary 69 revision 2, which included a
## newer lunar gravity model and only affected module 2.
## This file is intended to be a faithful transcription, except
## that the code format has been changed to conform to the
## requirements of the yaYUL assembler rather than the
## original YUL assembler.
## Reference: pp. 1-26
## Assembler: yaYUL
## Contact: Ron Burkey <info@sandroid.org>.
## Website: www.ibiblio.org/apollo/index.html
## Mod history: 2016-12-13 MAS Created from Luminary 99.
## 2016-12-23 MAS Began updating for Luminary 69
## 2017-01-04 MAS Completed updating for Luminary 69.
## 2017-01-25 RSB Proofed comment text using octopus/prooferComments
## and fixed the (single) error found.
## 2017-01-29 RSB Some of my fixes disappeared, for some reason.
## 2017-03-14 RSB Comment-text fixes identified in 5-way
## side-by-side diff of Luminary 69/99/116/131/210.
## Page 1
# 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
## Page 2
# TABLE OF LOG CARDS
# ASSEMBLY AND OPERATION INFORMATION
# TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
# PADLOADS
# 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
# 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
# GENERAL LAMBERT AIMPOINT GUIDANCE
# KISSING
# GROUND TRACKING DETERMINATION PROGRAM - P21
# P34-P35, P74-P75
# R31
# P76
# R30
## Page 3
# STABLE ORBIT - P38-P39
# 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
# 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
## Page 4
# 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
# 60 COMMAND LR TO POSITION 2.
# 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 CAUSES IMMEDIATE SWITCHING FROM P63 TO P64.
# 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, 2COMP XXXX.X NAUT MI DEC ONLY
# DELTA V, XXXX.X FT/SEC
# 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 DELTA R 1COMP XXXX.X NAUT MI DEC ONLY
# 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 HORIZONTAL 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
# CROSS RANGE DISTANCE XXXX.X NAUT MI
## Page 11
# 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 SPARE
# 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 CROSS-RANGE DISTANCE 2COMP XXXX.X NAUT MI DEC ONLY
# APOCYNTHION ALTITUDE 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 2COMP XXX.XX NAUT MI
# RANGE RATE XXXXX. FT/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 SPARE
# 92 SPARE
# 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 2COMP XXX.XX NAUT MI DEC ONLY
# RMS IN VELOCITY XXXX.X FT/SEC
## 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 C
# 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
# 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 1 DELTAR Q
# 58 1 POSTTPI Q
# 2 DELVTPI S
# 3 DELVTPF S
# 59 1 DVLOS S
# 2 DVLOS +2 S
# 3 DVLOS +4 S
# 60 1 VHORIZ S
# 2 HDOTDISP S
## Page 15
# 3 HCALC 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 HCALC 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 SPARE
# 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 XRANGE Q
# 2 APO Q
# 77 1 TTOGO L
# 2 YDOT S
# 78 1 RSTACK U
# 2 RSTACK +2 V
# 79 1 CURSOR D
# 2 SPIRAL D
# 3 POSCODE C
## Page 16
# 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 SPARE
# 92 SPARE
# 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
# 3 DSPTEM1 +2 C
# 98 1 DSPTEM2 C
# 2 DSPTEM2 +1 B
# 3 DSPTEM2 +2 C
# 99 1 WWPOS XX
# 2 WWVEL YY
## Page 17
# 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 18
# -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 19
# -T- -2
# G XXX.XX G SP BIT 1 = 10 G
# (MAX 163.83)
# -U-
# RENDEZVOUS XXX.XX NAUT MI DP LOW ORDER BIT OF LOW ORDER
# RADAR RANGE WORD = 9.38 FEET
# -V-
# RENDEZVOUS XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
# RADAR RANGE RATE WORD = -.6278 FEET/SEC
# -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 XXXXX. FEET/SEC SP LOW ORDER BIT = .5571
# VELOCITY (MAX 09126.) FEET/SEC
# -DD-
# 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
## Page 20
# -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
# 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 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
# (MAX 283.09) -9
# 2 METERS
## Page 21
# -YY-
# VELOCITY 4 XXXX.X FEET/SEC DP FRACTIONAL PART OF
# (MAX 328.0) METERS/CENTI-SEC
# THAT-S ALL ON THE NOUNS.
## Page 22
# ALARM CODES FOR LUMINARY
# *9 *18 *60 COLUMN
# CODE * TYPE SET BY
# 00105 ** AOTMARK SYSTEM IN USE
# 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 NOT IN POSITION 2 OR REPOSITIONING 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
# 00521 COULD NOT READ RADAR P20
# 00522 LANDING RADAR POSITION CHANGE RADAR READ
# 00523 P LR ANTENNA DIDN'T ACHIEVE POSITION 2 SERVICER, V60 (NON-P IN V60)
# 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
# 00526 P RANGE GREATER THAN 400 NAUT. MILES P20,P22
# 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21,R24
# LUNAR SURFACE
# OR VEHICLE MANEUVER REQUIRED R24 (20)
# 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
# 00604 CDH TO TPI TIME LT TMIN23 P32,P72,
## Page 23
# 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 (504 ONLY) P57
# 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
# 01102 AGC SELF TEST ERROR SELF CHECK
# 01103 ** UNUSED CCS BRANCH EXECUTED ABORT
# 01104 * DELAY ROUTINE BUSY EXEC
# 01105 DOWNLINK TOO FAST T4RUPT
# 01106 UPLINK TOO FAST T4RUPT
# 01107 PHASE TABLE FAILURE. ASSUME RESTART
# ERASABLE MEMORY IS SUSPECT. RESTART
# 01201 * EXECUTIVE OVERFLOW-NO VAC AREAS EXEC
# 01202 * EXECUTIVE OVERFLOW-NO CORE SETS EXEC
# 01203 * WAITLIST OVERFLOW-TOO MANY TASKS WAITLIST
# 01204 ** WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
# CALLED WITH ZERO OR NEGATIVE DELTA-TIME
# 01206 ** SECOND JOB ATTEMPTS TO GO TO SLEEP PINBALL
# 01206 VIA KYBD AND DISPLAY PROGRAM
# 01207 * NO VAC AREAS FOR MARKS AOTMARK
# 01210 * TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
# 01211 * ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
# 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
# 01302 ** SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
# 01406 ** BAD RETURN FROM ROOTPSRS LANDING 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
# 01501 ** KEYBOARD AND DISPLAY ALARM DURING PINBALL
# 01501 INTERNAL USE (NVSUB).ABORT
# 01502 ** ILLEGAL FLASHING DISPLAY GOPLAY
# 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
# 02000 * DAP STILL IN PROGRESS AT NEXT TIME5 RUPT DAP
# 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
## Page 24
# 13777 IMU , ICDU FAILS CAUSED THE ISS WARNING T4RUPT
# 14777 IMU,ICDU,PIPA FAILS CAUSED THE ISSWNING T4RUPT
# * INDICATES AN ABORT CODE THAT RESULTS IN A SOFTWARE RESTART.
# ** INDICATES A MORE SERIOUS ABORT CODE THAT RESULTS IN THE
# PROGRAM GOING TO R00.
# P INDICATES A PRIORITY ALARM.
# ALL OTHERS ARE NON-ABORTIVE
## Page 25
# 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 KEY IN FINE ALIGN OPTION P51,P63,P57
# 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 26
# 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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