Source Code
These source-code files were transcribed from scans made from Don Eyles's personal
copy of Luminary 069. They were scanned at archive.org's Boston
facility, and the scanning was sponsored by Onno Hommes. The code was transcribed
from these scans by a team of volunteers who are referenced in the program
comments. Comments from the original source code are prefixed with a single '#' symbol,
whereas comments added later are prefixed by "##" or "###". In some cases, where
similar code blocks exist in previously-transcribed AGC programs (primarily
Luminary 99, from Apollo 11) those code blocks were used as a starting point and
then corrected to agree with the Luminary 69 scans. The full scans are available
at the Virtual AGC
project's collection at archive.org, while more-convenient reduced-size (but reduced-quality)
images are available at
the main Virtual AGC website. Report any errors noted by creating an
issue report at the Virtual AGC
project's GitHub repository. Notations on the program listing read, in part:GAP: ASSEMBLE REVISION 069 OF AGC PROGRAM LUMINARY BY NASA 2021112-011 19:02 NOV. 25,1968Note that the date is the date of the printout, not the date of the program revision. |
000017,000002: ## Copyright: Public domain.
000018,000003: ## Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
000019,000004: ## Purpose: The main source file for Luminary revision 069.
000020,000005: ## It is part of the source code for the original release
000021,000006: ## of the flight software for the Lunar Module's (LM) Apollo
000022,000007: ## Guidance Computer (AGC) for Apollo 10. The actual flown
000023,000008: ## version was Luminary 69 revision 2, which included a
000024,000009: ## newer lunar gravity model and only affected module 2.
000025,000010: ## This file is intended to be a faithful transcription, except
000026,000011: ## that the code format has been changed to conform to the
000027,000012: ## requirements of the yaYUL assembler rather than the
000028,000013: ## original YUL assembler.
000029,000014: ## Reference: pp. 1-26
000030,000015: ## Assembler: yaYUL
000031,000016: ## Contact: Ron Burkey <info@sandroid.org>.
000032,000017: ## Website: www.ibiblio.org/apollo/index.html
000033,000018: ## Mod history: 2016-12-13 MAS Created from Luminary 99.
000034,000019: ## 2016-12-23 MAS Began updating for Luminary 69
000035,000020: ## 2017-01-04 MAS Completed updating for Luminary 69.
000036,000021: ## 2017-01-25 RSB Proofed comment text using octopus/prooferComments
000037,000022: ## and fixed the (single) error found.
000038,000023: ## 2017-01-29 RSB Some of my fixes disappeared, for some reason.
000039,000024: ## 2017-03-14 RSB Comment-text fixes identified in 5-way
000040,000025: ## side-by-side diff of Luminary 69/99/116/131/210.
000041,000026:
Page 1 |
000043,000028: # THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
000044,000029: # THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
000045,000030:
000046,000031:
000047,000032: # GUIDANCE SYSTEM OPERATIONS PLAN
000048,000033: # FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
000049,000034: # USING PROGRAM LUMINARY
000050,000035:
000051,000036:
000052,000037: # THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
000053,000038: # TECHNOLOGY 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS UNDER PROJECT55-238-70, SPONSORED BY THE MANNED
000054,000039: # SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065
000055,000040:
Page 2 |
000057,000042: # TABLE OF LOG CARDS
000058,000043:
000059,000044: # ASSEMBLY AND OPERATION INFORMATION
000060,000045: # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
000061,000046: # PADLOADS
000062,000047: # CONTROLLED CONSTANTS
000063,000048: # INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
000064,000049: # FLAGWORD ASSIGNMENTS
000065,000050: # SUBROUTINE CALLS
000066,000051:
000067,000052:
000068,000053: # TABLE OF SUBROUTINE LOG SECTIONS
000069,000054: # LUMERASE
000070,000055: # ERASABLE ASSIGNMENTS
000071,000056: # LEMONAID
000072,000057: # INTERRUPT LEAD INS
000073,000058: # T4RUPT PROGRAM
000074,000059: # RCS FAILURE MONITOR
000075,000060: # DOWNLINK LISTS
000076,000061: # AGS INITIALIZATION
000077,000062: # FRESH START AND RESTART
000078,000063: # RESTART TABLES
000079,000064: # AOTMARK
000080,000065: # EXTENDED VERBS
000081,000066: # PINBALL NOUN TABLES
000082,000067: # LEM GEOMETRY
000083,000068: # IMU COMPENSATION PACKAGE
000084,000069: # R63
000085,000070: # ATTITUDE MANEUVER ROUTINE
000086,000071: # GIMBAL LOCK AVOIDANCE
000087,000072: # KALCMANU STEERING
000088,000073: # SYSTEM TEST STANDARD LEAD INS
000089,000074: # IMU PERFORMANCE TESTS 2
000090,000075: # IMU PERFORMANCE TESTS 4
000091,000076: # PINBALL GAMES BUTTONS AND LIGHTS
000092,000077: # R60,R62
000093,000078: # S-BAND ANTENNA FOR LM
000094,000079: # LEMP20S
000095,000080: # RADAR LEADIN ROUTINES
000096,000081: # P20-P25
000097,000082: # LEMP30S
000098,000083: # P30,P37
000099,000084: # P32-P35, P72-P75
000100,000085: # GENERAL LAMBERT AIMPOINT GUIDANCE
000101,000086: # KISSING
000102,000087: # GROUND TRACKING DETERMINATION PROGRAM - P21
000103,000088: # P34-P35, P74-P75
000104,000089: # R31
000105,000090: # P76
000106,000091: # R30
Page 3 |
000108,000093: # STABLE ORBIT - P38-P39
000109,000094: # FLY
000110,000095: # BURN, BABY, BURN -- MASTER IGNITION ROUTINE
000111,000096: # P40-P47
000112,000097: # THE LUNAR LANDING
000113,000098: # THROTTLE CONTROL ROUTINES
000114,000099: # LUNAR LANDING GUIDANCE EQUATIONS
000115,000100: # P70-P71
000116,000101: # P12
000117,000102: # ASCENT GUIDANCE
000118,000103: # SERVICER
000119,000104: # LANDING ANALOG DISPLAYS
000120,000105: # FINDCDUW - GUIDAP INTERFACE
000121,000106: # LEMP50S
000122,000107: # P51-P53
000123,000108: # LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
000124,000109: # SKIPPER
000125,000110: # DOWN-TELEMETRY PROGRAM
000126,000111: # INTER-BANK COMMUNICATION
000127,000112: # INTERPRETER
000128,000113: # FIXED-FIXED CONSTANT POOL
000129,000114: # INTERPRETIVE CONSTANTS
000130,000115: # SINGLE PRECISION SUBROUTINES
000131,000116: # EXECUTIVE
000132,000117: # WAITLIST
000133,000118: # LATITUDE LONGITUDE SUBROUTINES
000134,000119: # PLANETARY INERTIAL ORIENTATION
000135,000120: # MEASUREMENT INCORPORATION
000136,000121: # CONIC SUBROUTINES
000137,000122: # INTEGRATION INITIALIZATION
000138,000123: # ORBITAL INTEGRATION
000139,000124: # INFLIGHT ALIGNMENT ROUTINES
000140,000125: # POWERED FLIGHT SUBROUTINES
000141,000126: # TIME OF FREE FALL
000142,000127: # AGC BLOCK TWO SELF-CHECK
000143,000128: # PHASE TABLE MAINTENANCE
000144,000129: # RESTARTS ROUTINE
000145,000130: # IMU MODE SWITCHING ROUTINES
000146,000131: # KEYRUPT, UPRUPT
000147,000132: # DISPLAY INTERFACE ROUTINES
000148,000133: # SERVICE ROUTINES
000149,000134: # ALARM AND ABORT
000150,000135: # UPDATE PROGRAM
000151,000136: # RTB OP CODES
000152,000137: # LMDAP
000153,000138: # T6-RUPT PROGRAMS
000154,000139: # DAP INTERFACE SUBROUTINES
000155,000140: # DAPIDLER PROGRAM
000156,000141: # P-AXIS RCS AUTOPILOT
000157,000142: # Q,R-AXIS RCS AUTOPILOT
Page 4 |
000159,000144: # TJET LAW
000160,000145: # KALMAN FILTER
000161,000146: # TRIM GIMBAL CONTROL SYSTEM
000162,000147: # AOSTASK AND AOSJOB
000163,000148: # SPS BACK-UP RCS CONTROL
000164,000149:
000165,000150:
000166,000151: # SYMBOL TABLE LISTING
000167,000152: # UNREFERENCED SYMBOL LISTING
000168,000153: # ERASABLE & EQUALS CROSS-REFERENCE TABLE
000169,000154: # SUMMARY OF SYMBOL TABLE LISTINGS
000170,000155: # MEMORY TYPE & AVAILABLITY DISPLAY
000171,000156: # COUNT TABLE
000172,000157: # PARAGRAPHS GENERATED FOR THIS ASSEMBLY
000173,000158: # OCTAL LISTING
000174,000159: # OCCUPIED LOCATIONS TABLE
000175,000160: # SUBROS CALLED & PROGRAM STATUS
000176,000161:
Page 5 |
000178,000163: # VERB LIST FOR LUMINARY
000179,000164:
000180,000165: # REGULAR VERBS
000181,000166:
000182,000167: # 00 NOT IN USE
000183,000168: # 01 DISPLAY OCTAL COMP 1 IN R1
000184,000169: # 02 DISPLAY OCTAL COMP 2 IN R1
000185,000170: # 03 DISPLAY OCTAL COMP 3 IN R1
000186,000171: # 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
000187,000172: # 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
000188,000173: # 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000189,000174: # 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
000190,000175: # 08
000191,000176: # 09
000192,000177: # 10
000193,000178: # 11 MONITOR OCTAL COMP 1 IN R1
000194,000179: # 12 MONITOR OCTAL COMP 2 IN R1
000195,000180: # 13 MONITOR OCTAL COMP 3 IN R1
000196,000181: # 14 MONITOR OCTAL COMP 1,2 IN R1,R2
000197,000182: # 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
000198,000183: # 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000199,000184: # 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
000200,000185: # 18
000201,000186: # 19
000202,000187: # 20
000203,000188: # 21 LOAD COMPONENT 1 INTO R1
000204,000189: # 22 LOAD COMPONENT 2 INTO R2
000205,000190: # 23 LOAD COMPONENT 3 INTO R3
000206,000191: # 24 LOAD COMPONENT 1,2 INTO R1,R2
000207,000192: # 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
000208,000193: # 26
000209,000194: # 27 DISPLAY FIXED MEMORY
000210,000195: # 28
000211,000196: # 29
000212,000197: # 30 REQUEST EXECUTIVE
000213,000198: # 31 REQUEST WAITLIST
000214,000199: # 32 RECYCLE PROGRAM
000215,000200: # 33 PROCEED WITHOUT DSKY INPUTS
000216,000201: # 34 TERMINATE FUNCTION
000217,000202: # 35 TEST LIGHTS
000218,000203: # 36 REQUEST FRESH START
000219,000204: # 37 CHANGE PROGRAM (MAJOR MODE)
000220,000205: # 38
000221,000206: # 39
000222,000207:
Page 6 |
000224,000209: # EXTENDED VERBS
000225,000210:
000226,000211: # 40 ZERO CDU-S
000227,000212: # 41 COARSE ALIGN CDU-S
000228,000213: # 42 FINE ALIGN IMU
000229,000214: # 43 LOAD IMU ATT ERROR METERS
000230,000215: # 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
000231,000216: # 45
000232,000217: # 46
000233,000218: # 47 INITIALIZE AGS (R47)
000234,000219: # 48 REQUEST DAP DATA LOAD ROUTINE (R03)
000235,000220: # 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
000236,000221: # 50 PLEASE PERFORM
000237,000222: # 51
000238,000223: # 52 MARK X-RETICLE
000239,000224: # 53 MARK Y-RETICLE
000240,000225: # 54 MARK X OR Y-RETICLE
000241,000226: # 55 INCREMENT AGC TIME (DECIMAL)
000242,000227: # 56 TERMINATE TRACKING (P20 + P25)
000243,000228: # 57 PERMIT LANDING RADAR UPDATES
000244,000229: # 58 INHIBIT LANDING RADAR UPDATES
000245,000230: # 59
000246,000231: # 60 COMMAND LR TO POSITION 2.
000247,000232: # 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
000248,000233: # 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
000249,000234: # 63 SAMPLE RADAR ONCE PER SECOND (R04).
000250,000235: # 64 REQUEST S-BAND ANTENNA ROUTINE (R05)
000251,000236: # 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
000252,000237: # 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
000253,000238: # 67 DISPLAY W MATRIX
000254,000239: # 68 CAUSES IMMEDIATE SWITCHING FROM P63 TO P64.
000255,000240: # 69 CAUSE RESTART
000256,000241: # 70 UPDATE LIFTOFF TIME
000257,000242: # 71 UNIVERSAL UPDATE-BLOCK ADR
000258,000243: # 72 UNIVERSAL UPDATE-SINGLE ADR
000259,000244: # 73 UPDATE AGC TIME (OCTAL)
000260,000245: # 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
000261,000246: # 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
000262,000247: # 76 MINIMUM IMPULSE COMMAND MODE
000263,000248: # 77 RATE COMMAND AND ATTITUDE HOLD MODE
000264,000249: # 78 LR SPURIOUS RETURN TEST START (R77)
000265,000250: # 79 LR SPURIOUS RETURN TEST STOP
000266,000251: # 80 UPDATE LEM STATE VECTOR
000267,000252: # 81 UPDATE CSM STATE VECTOR
000268,000253: # 82 REQUEST ORBIT PARAM DISPLAY (R30)
000269,000254: # 83 REQUEST REND PARAM DISPLAY (R31)
000270,000255: # 84
000271,000256: # 85 DISPLAY RR LOS AZ AND ELEV
000272,000257: # 86
000273,000258: # 87
Page 7 |
000275,000260: # 88
000276,000261: # 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
000277,000262: # 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
000278,000263: # 91 DISPLAY BANK SUM
000279,000264: # 92 OPERATE IMU PERFORMANCE TEST (P07)
000280,000265: # 93 ENABLE W MATRIX INITIALIZATION
000281,000266: # 94
000282,000267: # 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
000283,000268: # 96 INTERRUPT INTEGRATION AND GO TO POO
000284,000269: # 97 PERFORM ENGINE FAIL PROCEDURE
000285,000270: # 98
000286,000271: # 99 PLEASE ENABLE ENGINE
000287,000272:
Page 8 |
000289,000274: # IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
000290,000275: # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
000291,000276: # SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
000292,000277: # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23
000293,000278: # MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
000294,000279: # ABOVE SCALE TYPES.
000295,000280: # THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
000296,000281: # EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
000297,000282:
000298,000283: # NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000299,000284:
000300,000285: # 00 NOT IN USE
000301,000286: # 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH
000302,000287: # 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH
000303,000288: # 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP XXX.XX DEG FOR EACH
000304,000289: # 04 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000305,000290: # 05 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000306,000291: # 06 OPTION CODE 3COMP OCTAL ONLY FOR EACH
000307,000292: # LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
000308,000293: # 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
000309,000294: # ONES FOR BITS TO BE MODIFIED
000310,000295: # 1 TO SET OR 0 TO RESET SELECTED BITS
000311,000296: # 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
000312,000297: # 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
000313,000298: # 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
000314,000299: # 11 TIG OF CSI 3COMP 00XXX. HRS DEC ONLY
000315,000300: # 000XX. MIN MUST LOAD 3 COMPS
000316,000301: # 0XX.XX SEC
000317,000302: # 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
000318,000303: # (USED BY EXTENDED VERBS ONLY)
000319,000304: # 13 TIG OF CDH 3COMP 00XXX. HRS DEC ONLY
000320,000305: # 000XX. MIN MUST LOAD 3 COMPS
000321,000306: # 0XX.XX SEC
000322,000307: # 14 CHECKLIST 3COMP XXXXX. FOR EACH
000323,000308: # (USED BY EXTENDED VERBS ONLY)
000324,000309: # (NOUN 25 IS PASTED AFTER DISPLAY)
000325,000310: # 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
000326,000311: # 16 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000327,000312: # (USED BY EXTENDED VERBS ONLY) 000XX. MIN MUST LOAD 3 COMPS
000328,000313: # 0XX.XX SEC
000329,000314: # 17 SPARE
000330,000315: # 18 AUTO MANEUVER BALL ANGLES 3COMP XXX.XX DEG FOR EACH
000331,000316: # 19 SPARE
000332,000317: # 20 ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000333,000318: # 21 PIPAS 3COMP XXXXX. PULSES FOR EACH
000334,000319: # 22 NEW ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000335,000320: # 23 SPARE
000336,000321: # 24 DELTA TIME FOR AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000337,000322: # 000XX. MIN MUST LOAD 3 COMPS
000338,000323: # 0XX.XX SEC
Page 9 |
000340,000325: # 25 CHECKLIST 3COMP XXXXX. FOR EACH
000341,000326: # (USED WITH PLEASE PERFORM ONLY)
000342,000327: # 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
000343,000328: # 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX.
000344,000329: # 28 SPARE
000345,000330: # 29 SPARE
000346,000331: # 30 SPARE
000347,000332: # 31 SPARE
000348,000333: # 32 TIME FROM PERIGEE 3COMP 00XXX. HRS DEC ONLY
000349,000334: # 000XX. MIN MUST LOAD 3 COMPS
000350,000335: # 0XX.XX SEC
000351,000336: # 33 TIME OF IGNITION 3COMP 00XXX. HRS DEC ONLY
000352,000337: # 000XX. MIN MUST LOAD 3 COMPS
000353,000338: # 0XX.XX SEC
000354,000339: # 34 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000355,000340: # 000XX. MIN MUST LOAD 3 COMPS
000356,000341: # 0XX.XX SEC
000357,000342: # 35 TIME FROM EVENT 3COMP 00XXX. HRS DEC ONLY
000358,000343: # 000XX. MIN MUST LOAD 3 COMPS
000359,000344: # 0XX.XX SEC
000360,000345: # 36 TIME OF AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000361,000346: # 000XX. MIN MUST LOAD 3 COMPS
000362,000347: # 0XX.XX SEC
000363,000348: # 37 TIG OF TPI 3COMP 00XXX. HRS DEC ONLY
000364,000349: # 000XX. MIN MUST LOAD 3 COMPS
000365,000350: # 0XX.XX SEC
000366,000351: # 38 TIME OF STATE BEING INTEGRATED 3COMP 00XXX. HRS DEC ONLY
000367,000352: # 000XX. MIN MUST LOAD 3 COMPS
000368,000353: # 0XX.XX SEC
000369,000354: # 39 SPARE
000370,000355:
Page 10 |
000372,000357: # MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000373,000358:
000374,000359: # 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000375,000360: # VG, XXXX.X FT/SEC
000376,000361: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000377,000362: # 41 TARGET AZIMUTH, 2COMP XXX.XX DEG (FOR SYSTEM TEST)
000378,000363: # ELEVATION XX.XXX DEG
000379,000364: # 42 APOGEE, 3COMP XXXX.X NAUT MI DEC ONLY
000380,000365: # PERIGEE, XXXX.X NAUT MI
000381,000366: # DELTA V (REQUIRED) XXXX.X FT/SEC
000382,000367: # 43 LATITUDE, 3COMP XXX.XX DEG DEC ONLY
000383,000368: # LONGITUDE, XXX.XX DEG
000384,000369: # ALTITUDE XXXX.X NAUT MI
000385,000370: # 44 APOGEE, 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000386,000371: # PERIGEE, XXXX.X NAUT MI
000387,000372: # TFF XXBXX MIN/SEC
000388,000373: # 45 MARKS, 3COMP XXXXX. NO LOAD, DEC ONLY
000389,000374: # TFI OF NEXT BURN XXBXX MIN/SEC
000390,000375: # MGA XXX.XX DEG
000391,000376: # 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
000392,000377: # 47 LEM WEIGHT, 2COMP XXXXX. LBS DEC ONLY
000393,000378: # CSM WEIGHT XXXXX. LBS
000394,000379: # 48 GIMBAL PITCH TRIM, 2COMP XXX.XX DEG DEC ONLY
000395,000380: # GIMBAL ROLL TRIM XXX.XX DEG
000396,000381: # 49 DELTA R, 2COMP XXXX.X NAUT MI DEC ONLY
000397,000382: # DELTA V, XXXX.X FT/SEC
000398,000383: # 50 SPARE
000399,000384: # 51 S-BAND ANTENNA ANGLES PITCH 2COMP XXX.XX DEG DEC ONLY
000400,000385: # YAW XXX.XX DEG
000401,000386: # 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG
000402,000387: # 53 SPARE
000403,000388: # 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
000404,000389: # RANGE RATE, XXXX.X FT/SEC
000405,000390: # THETA XXX.XX DEG
000406,000391: # 55 NO. OF APSIDAL CROSSINGS 3COMP XXXXX. DEC ONLY
000407,000392: # ELEVATION ANGLE XXX.XX DEG
000408,000393: # CENTRAL ANGLE OF PASSIVE VEHICLE XXX.XX DEG
000409,000394: # 56 RR LOS AZIMUTH 2COMP XXX.XX DEG
000410,000395: # ELEVATION XXX.XX DEG
000411,000396: # 57 DELTA R 1COMP XXXX.X NAUT MI DEC ONLY
000412,000397: # 58 PERIGEE ALT (POST TPI) 3COMP XXXX.X NAUT MI DEC ONLY
000413,000398: # DELTA V TPI XXXX.X FT/SEC
000414,000399: # DELTA V TPF XXXX.X FT/SEC
000415,000400: # 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY
000416,000401: # 60 HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000417,000402: # ALTITUDE RATE XXXX.X FT/SEC
000418,000403: # COMPUTED ALTITUDE XXXXX. FEET
000419,000404: # 61 TIME TO GO IN BRAKING PHASE 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000420,000405: # TIME FROM IGNITION XXBXX MIN/SEC
000421,000406: # CROSS RANGE DISTANCE XXXX.X NAUT MI
Page 11 |
000423,000408: # 62 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC NO LOAD, DEC ONLY
000424,000409: # TIME FROM IGNITION XXBXX MIN/SEC
000425,000410: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000426,000411: # 63 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000427,000412: # ALTITUDE RATE XXXX.X FT/SEC
000428,000413: # COMPUTED ALTITUDE XXXXX. FEET
000429,000414: # 64 TIME LEFT FOR REDESIGNATION- LPD ANGLE 3COMP XXBXX NO LOAD, DEC ONLY
000430,000415: # ALTITUDE RATE XXXX.X FT/SEC
000431,000416: # COMPUTED ALTITUDE XXXXX. FEET
000432,000417: # 65 SAMPLED AGC TIME 3COMP 00XXX. HRS DEC ONLY
000433,000418: # (FETCHED IN INTERRUPT) 000XX. MIN MUST LOAD 3 COMPS
000434,000419: # 0XX.XX SEC
000435,000420: # 66 LR RANGE 2COMP XXXXX. FEET NO LOAD, DEC ONLY
000436,000421: # POSITION +0000X
000437,000422: # 67 LRVX 3COMP XXXXX. FT/SEC
000438,000423: # LRVY XXXXX. FT/SEC
000439,000424: # LRVZ XXXXX. FT/SEC
000440,000425: # 68 SLANT RANGE TO LANDING SITE 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000441,000426: # TIME TO GO IN BRAKING PHASE XXBXX MIN/SEC
000442,000427: # LR ALTITUDE - COMPUTED ALTITUDE XXXXX. FEET
000443,000428: # 69 SPARE
000444,000429: # 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000445,000430: # 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000446,000431: # 72 RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000447,000432: # SHAFT ANGLE XXX.XX DEG
000448,000433: # 73 NEW RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000449,000434: # SHAFT ANGLE XXX.XX DEG
000450,000435: # 74 TIME FROM IGNITION 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000451,000436: # YAW AFTER VEHICLE RISE XXX.XX DEG
000452,000437: # PITCH AFTER VEHICLE RISE XXX.XX DEG
000453,000438: # 75 DELTA ALTITUDE CDH 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000454,000439: # DELTA TIME (CDH-CSI OR TPI-CDH) XXBXX MIN/SEC
000455,000440: # DELTA TIME (TPI-CDH OR TPI-NOMTPI) XXBXX MIN/SEC
000456,000441: # 76 CROSS-RANGE DISTANCE 2COMP XXXX.X NAUT MI DEC ONLY
000457,000442: # APOCYNTHION ALTITUDE XXXX.X NAUT MI
000458,000443: # 77 TIME TO ENGINE CUTOFF 2COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000459,000444: # VELOCITY NORMAL TO CSM PLANE XXXX.X FT/SEC
000460,000445: # 78 RR RANGE 2COMP XXX.XX NAUT MI
000461,000446: # RANGE RATE XXXXX. FT/SEC
000462,000447: # 79 CURSOR ANGLE 3COMP XXX.XX DEG DEC ONLY
000463,000448: # SPIRAL ANGLE XXX.XX DEG
000464,000449: # POSITION CODE XXXXX.
000465,000450: # 80 DATA INDICATOR, 2COMP XXXXX.
000466,000451: # OMEGA XXX.XX DEG
000467,000452: # 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
Page 12 |
000469,000454: # 82 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000470,000455: # 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000471,000456: # 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000472,000457: # 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000473,000458: # 86 VG (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000474,000459: # 87 BACKUP OPTICS LOS AZIMUTH 2COMP XXX.XX DEG
000475,000460: # ELEVATION XXX.XX DEG
000476,000461: # 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY
000477,000462: # 89 LANDMARK LATITUDE 3COMP XX.XXX DEG DEC ONLY
000478,000463: # LONGITUDE/2 XX.XXX DEC
000479,000464: # ALTITUDE XXX.XX NAUT MI
000480,000465: # 90 Y 3COMP XXX.XX NM DEC ONLY
000481,000466: # Y DOT XXXX.X FPS
000482,000467: # PSI XXX.XX DEG
000483,000468: # 91 SPARE
000484,000469: # 92 SPARE
000485,000470: # 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
000486,000471: # 94 SPARE
000487,000472: # 95 SPARE
000488,000473: # 96 SPARE
000489,000474: # 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH
000490,000475: # 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX.
000491,000476: # .XXXXX
000492,000477: # XXXXX.
000493,000478: # 99 RMS IN POSITION 2COMP XXX.XX NAUT MI DEC ONLY
000494,000479: # RMS IN VELOCITY XXXX.X FT/SEC
000495,000480:
Page 13 |
000497,000482: # REGISTERS AND SCALING FOR NORMAL NOUNS
000498,000483:
000499,000484: # NOUN REGISTER SCALE TYPE
000500,000485:
000501,000486: # 00 NOT IN USE
000502,000487: # 01 SPECIFY ADDRESS B
000503,000488: # 02 SPECIFY ADDRESS C
000504,000489: # 03 SPECIFY ADDRESS D
000505,000490: # 04 DSPTEM1 H
000506,000491: # 05 DSPTEM1 H
000507,000492: # 06 OPTION1 A
000508,000493: # 07 XREG A
000509,000494: # 08 ALMCADR A
000510,000495: # 09 FAILREG A
000511,000496: # 10 SPECIFY CHANNEL A
000512,000497: # 11 TCSI K
000513,000498: # 12 OPTIONX A
000514,000499: # 13 TCDH K
000515,000500: # 14 DSPTEMX C
000516,000501: # 15 INCREMENT ADDRESS A
000517,000502: # 16 DSPTEMX C
000518,000503: # 17 SPARE
000519,000504: # 18 FDAIX D
000520,000505: # 19 SPARE
000521,000506: # 20 CDUX D
000522,000507: # 21 PIPAX C
000523,000508: # 22 THETAD D
000524,000509: # 23 SPARE
000525,000510: # 24 DSPTEM2 +1 K
000526,000511: # 25 DSPTEM1 C
000527,000512: # 26 DSPTEM1 A
000528,000513: # 27 SMODE C
000529,000514: # 28 SPARE
000530,000515: # 29 SPARE
000531,000516: # 30 SPARE
000532,000517: # 31 SPARE
000533,000518: # 32 -TPER K
000534,000519: # 33 TIG K
000535,000520: # 34 DSPTEM1 K
000536,000521: # 35 TTOGO K
000537,000522: # 36 TIME2 K
000538,000523: # 37 TTPI K
000539,000524: # 38 TET K
000540,000525: # 39 SPARE
000541,000526:
Page 14 |
000543,000528: # REGISTERS AND SCALING FOR MIXED NOUNS
000544,000529:
000545,000530: # NOUN COMP REGISTER SCALE TYPE
000546,000531:
000547,000532: # 40 1 TTOGO L
000548,000533: # 2 VGDISP S
000549,000534: # 3 DVTOTAL S
000550,000535: # 41 1 DSPTEM1 D
000551,000536: # 2 DSPTEM1 +1 E
000552,000537: # 42 1 HAPO Q
000553,000538: # 2 HPER Q
000554,000539: # 3 VGDISP S
000555,000540: # 43 1 LAT H
000556,000541: # 2 LONG H
000557,000542: # 3 ALT Q
000558,000543: # 44 1 HAPOX Q
000559,000544: # 2 HPERX Q
000560,000545: # 3 TFF L
000561,000546: # 45 1 TRKMKCNT C
000562,000547: # 2 TTOGO L
000563,000548: # 3 +MGA H
000564,000549: # 46 1 DAPDATR1 A
000565,000550: # 47 1 LEMMASS KK
000566,000551: # 2 CSMMASS KK
000567,000552: # 48 1 PITTIME NN
000568,000553: # 2 ROLLTIME NN
000569,000554: # 49 1 R22DISP Q
000570,000555: # 2 R22DISP +2 S
000571,000556: # 50 SPARE
000572,000557: # 51 1 ALPHASB H
000573,000558: # 2 BETASB H
000574,000559: # 52 1 ACTCENT H
000575,000560: # 53 SPARE
000576,000561: # 54 1 RANGE JJ
000577,000562: # 2 RRATE S
000578,000563: # 3 RTHETA H
000579,000564: # 55 1 NN C
000580,000565: # 2 ELEV H
000581,000566: # 3 CENTANG H
000582,000567: # 56 1 RR-AZ H
000583,000568: # 2 RR-ELEV H
000584,000569: # 57 1 DELTAR Q
000585,000570: # 58 1 POSTTPI Q
000586,000571: # 2 DELVTPI S
000587,000572: # 3 DELVTPF S
000588,000573: # 59 1 DVLOS S
000589,000574: # 2 DVLOS +2 S
000590,000575: # 3 DVLOS +4 S
000591,000576: # 60 1 VHORIZ S
000592,000577: # 2 HDOTDISP S
Page 15 |
000594,000579: # 3 HCALC RR
000595,000580: # 61 1 TTFDISP L
000596,000581: # 2 TTOGO L
000597,000582: # 3 OUTOFPLN QQ
000598,000583: # 62 1 ABVEL S
000599,000584: # 2 TTOGO L
000600,000585: # 3 DVTOTAL S
000601,000586: # 63 1 ABVEL S
000602,000587: # 2 HDOTDISP S
000603,000588: # 3 HCALC RR
000604,000589: # 64 1 FUNNYDSP PP
000605,000590: # 2 HDOTDISP S
000606,000591: # 3 HCALC RR
000607,000592: # 65 1 SAMPTIME K
000608,000593: # 2 SAMPTIME K
000609,000594: # 3 SAMPTIME K
000610,000595: # 66 1 RSTACK +6 W
000611,000596: # 2 CHANNEL 33 TT
000612,000597: # 67 1 RSTACK X
000613,000598: # 2 RSTACK +2 Y
000614,000599: # 3 RSTACK +4 Z
000615,000600: # 68 1 RANGEDSP QQ
000616,000601: # 2 TTFDISP L
000617,000602: # 3 DELTAH RR
000618,000603: # 69 SPARE
000619,000604: # 70 1 AOTCODE A
000620,000605: # 2 AOTCODE +1 A
000621,000606: # 3 AOTCODE +2 A
000622,000607: # 71 1 AOTCODE A
000623,000608: # 2 AOTCODE +1 A
000624,000609: # 3 AOTCODE +2 A
000625,000610: # 72 1 CDUT WW
000626,000611: # 2 CDUS D
000627,000612: # 73 1 TANG WW
000628,000613: # 2 TANG +1 D
000629,000614: # 74 1 TTOGO L
000630,000615: # 2 YAW H
000631,000616: # 3 PITCH H
000632,000617: # 75 1 DIFFALT Q
000633,000618: # 2 T1TOT2 L
000634,000619: # 3 T2TOT3 L
000635,000620: # 76 1 XRANGE Q
000636,000621: # 2 APO Q
000637,000622: # 77 1 TTOGO L
000638,000623: # 2 YDOT S
000639,000624: # 78 1 RSTACK U
000640,000625: # 2 RSTACK +2 V
000641,000626: # 79 1 CURSOR D
000642,000627: # 2 SPIRAL D
000643,000628: # 3 POSCODE C
Page 16 |
000645,000630: # 80 1 DATAGOOD C
000646,000631: # 2 OMEGAD H
000647,000632: # 81 1 DELVLVC S
000648,000633: # 2 DELVLVC +2 S
000649,000634: # 3 DELVLVC +4 S
000650,000635: # 82 1 DELVLVC S
000651,000636: # 2 DELVLVC +2 S
000652,000637: # 3 DELVLVC +4 S
000653,000638: # 83 1 DELVIMU S
000654,000639: # 2 DELVIMU +2 S
000655,000640: # 3 DELVIMU +4 S
000656,000641: # 84 1 DELVOV S
000657,000642: # 2 DELVOV +2 S
000658,000643: # 3 DELVOV +4 S
000659,000644: # 85 1 VGBODY S
000660,000645: # 2 VGBODY +2 S
000661,000646: # 3 VGBODY +4 S
000662,000647: # 86 1 DELVLVC S
000663,000648: # 2 DELVLVC +2 S
000664,000649: # 3 DELVLVC +4 S
000665,000650: # 87 1 AZ D
000666,000651: # 2 EL D
000667,000652: # 88 1 STARAD B
000668,000653: # 2 STARAD +2 B
000669,000654: # 3 STARAD +4 B
000670,000655: # 89 1 LANDLAT G
000671,000656: # 2 LANDLONG G
000672,000657: # 3 LANDALT JJ
000673,000658: # 90 1 RANGE JJ
000674,000659: # 2 RRATE S
000675,000660: # 3 RTHETA H
000676,000661: # 91 SPARE
000677,000662: # 92 SPARE
000678,000663: # 93 1 OGC G
000679,000664: # 2 OGC +2 G
000680,000665: # 3 OGC +4 G
000681,000666: # 94 SPARE
000682,000667: # 95 SPARE
000683,000668: # 96 SPARE
000684,000669: # 97 1 DSPTEM1 C
000685,000670: # 2 DSPTEM1 +1 C
000686,000671: # 3 DSPTEM1 +2 C
000687,000672: # 98 1 DSPTEM2 C
000688,000673: # 2 DSPTEM2 +1 B
000689,000674: # 3 DSPTEM2 +2 C
000690,000675: # 99 1 WWPOS XX
000691,000676: # 2 WWVEL YY
000692,000677:
Page 17 |
000694,000679: # NOUN SCALES AND FORMATS
000695,000680:
000696,000681: # -SCALE TYPE- PRECISION
000697,000682: # UNITS DECIMAL FORMAT -- AGC FORMAT
000698,000683: # ------------ -------------- -- ----------
000699,000684:
000700,000685: # -A-
000701,000686: # OCTAL XXXXX SP OCTAL
000702,000687:
000703,000688: # -B- -14
000704,000689: # FRACTIONAL .XXXXX SP BIT 1 = 2 UNITS
000705,000690: # (MAX .99996)
000706,000691:
000707,000692: # -C-
000708,000693: # WHOLE XXXXX. SP BIT 1 = 1 UNIT
000709,000694: # (MAX 16383.)
000710,000695:
000711,000696: # -D- 15
000712,000697: # CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360/2 DEGREES
000713,000698: # (MAX 359.99) (USES 15 BITS FOR MAGNI-
000714,000699: # TUDE AND 2-S COMP.)
000715,000700:
000716,000701: # -E- 14
000717,000702: # ELEVATION DEGREES XX.XXX DEGREES SP BIT 1 = 90/2 DEGREES
000718,000703: # (MAX 89.999)
000719,000704:
000720,000705: # -F- 14
000721,000706: # DEGREES (180) XXX.XX DEGREES SP BIT 1 = 180/2 DEGREES
000722,000707: # (MAX 179.99)
000723,000708:
000724,000709: # -G-
000725,000710: # DP DEGREES (90) XX.XXX DEGREES DP BIT 1 OF LOW REGISTER =
000726,000711: # 28
000727,000712: # 360/2 DEGREES
000728,000713:
000729,000714: # -H-
000730,000715: # DP DEGREES (360) XXX.XX DEGREES DP BIT 1 OF LOW REGISTER =
000731,000716: # 28
000732,000717: # (MAX 359.99) 360/2 DEGREES
000733,000718:
Page 18 |
000735,000720: # -K-
000736,000721: # TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER =
000737,000722: # 000XX. MIN -2
000738,000723: # 0XX.XX SEC 10 SEC
000739,000724: # (DECIMAL ONLY.
000740,000725: # MAX MIN COMP=59
000741,000726: # MAX SEC COMP=59.99
000742,000727: # MAX CAPACITY=745 HRS
000743,000728: # 39 MINS
000744,000729: # 14.55 SECS.
000745,000730: # WHEN LOADING, ALL 3
000746,000731: # COMPONENTS MUST BE
000747,000732: # SUPPLIED.)
000748,000733:
000749,000734: # -L-
000750,000735: # TIME (MIN/SEC) XXBXX MIN/SEC DP BIT 1 OF LOW REGISTER =
000751,000736: # (B IS A BLANK -2
000752,000737: # POSITION, DECIMAL 10 SEC
000753,000738: # ONLY, DISPLAY OR
000754,000739: # MONITOR ONLY. CANNOT
000755,000740: # BE LOADED.
000756,000741: # MAX MIN COMP=59
000757,000742: # MAX SEC COMP=59
000758,000743: # VALUES GREATER THAN
000759,000744: # 59 MIN 59 SEC
000760,000745: # ARE DISPLAYED AS
000761,000746: # 59 MIN 59 SEC.)
000762,000747:
000763,000748: # -M- -2
000764,000749: # TIME (SEC) XXX.XX SEC SP BIT 1 = 10 SEC
000765,000750: # (MAX 163.83)
000766,000751:
000767,000752: # -N-
000768,000753: # TIME(SEC) DP XXX.XX SEC DP BIT 1 OF LOW REGISTER =
000769,000754: # -2
000770,000755: # 10 SEC
000771,000756:
000772,000757: # -P-
000773,000758: # VELOCITY 2 XXXXX. FEET/SEC DP BIT 1 OF HIGH REGISTER =
000774,000759: # (MAX 41994.) -7
000775,000760: # 2 METERS/CENTI-SEC
000776,000761:
000777,000762: # -Q-
000778,000763: # POSITION 4 XXXX.X NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
000779,000764: # 2 METERS
000780,000765:
000781,000766: # -S-
000782,000767: # VELOCITY 3 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
000783,000768: # -7
000784,000769: # 2 METERS/CENTI-SEC
000785,000770:
Page 19 |
000787,000772: # -T- -2
000788,000773: # G XXX.XX G SP BIT 1 = 10 G
000789,000774: # (MAX 163.83)
000790,000775:
000791,000776: # -U-
000792,000777: # RENDEZVOUS XXX.XX NAUT MI DP LOW ORDER BIT OF LOW ORDER
000793,000778: # RADAR RANGE WORD = 9.38 FEET
000794,000779:
000795,000780: # -V-
000796,000781: # RENDEZVOUS XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000797,000782: # RADAR RANGE RATE WORD = -.6278 FEET/SEC
000798,000783:
000799,000784: # -W-
000800,000785: # LANDING RADAR XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000801,000786: # ALTITUDE WORD = 1.079 FEET
000802,000787:
000803,000788: # -X-
000804,000789: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000805,000790: # VELX WORD = -.6440 FEET/SEC
000806,000791:
000807,000792: # -Y-
000808,000793: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000809,000794: # VELY WORD = 1.212 FEET/SEC
000810,000795:
000811,000796: # -Z-
000812,000797: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000813,000798: # VELZ WORD = .8668 FEET/SEC
000814,000799:
000815,000800: # -AA-
000816,000801: # INITIAL/FINAL XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000817,000802: # ALTITUDE WORD = 2.345 FEET
000818,000803:
000819,000804: # -BB-
000820,000805: # ALTITUDE RATE XXXXX. FEET/SEC SP LOW ORDER BIT = .5
000821,000806: # (MAX 08191.) FEET/SEC
000822,000807:
000823,000808: # -CC-
000824,000809: # FORWARD/LATERAL XXXXX. FEET/SEC SP LOW ORDER BIT = .5571
000825,000810: # VELOCITY (MAX 09126.) FEET/SEC
000826,000811:
000827,000812: # -DD-
000828,000813: # ROTATIONAL HAND XXXXX. DEG/SEC SP FRACTIONAL PART OF PI RAD
000829,000814: # CONTROLLER ANGULAR (MAX 00044.) 4 SEC
000830,000815: # RATES
000831,000816:
000832,000817: # -EE-
000833,000818: # OPTICAL TRACKER XXX.XX DEG. DP LOW ORDER BIT OF LOW ORDER
000834,000819: # AZIMUTH ANGLE 15
000835,000820: # WORD = 360/2 DEGREES
000836,000821:
Page 20 |
000838,000823: # -JJ-
000839,000824: # POSITION5 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
000840,000825: # 2 METERS
000841,000826:
000842,000827: # -KK- 16
000843,000828: # WEIGHT2 XXXXX. LBS SP FRACTIONAL PART OF 2 KG
000844,000829:
000845,000830: # -NN-
000846,000831: # TRIM DEGREES 2 XXX.XX DEG SP BIT 1=.01SEC(TIME)
000847,000832: # (MAX 032.76)
000848,000833:
000849,000834: # -PP-
000850,000835: # 2 INTEGERS +XXBYY DP BIT 1 OF HIGH REGISTER =
000851,000836: # (B IS A BLANK 1 UNIT OF XX
000852,000837: # POSITION. DECIMAL BIT 1 OF LOW REGISTER =
000853,000838: # ONLY, DISPLAY OR 1 UNIT OF YY
000854,000839: # MONITOR ONLY. CANNOT (EACH REGISTER MUST
000855,000840: # BE LOADED.) CONTAIN A POSITIVE INTEGER
000856,000841: # (MAX 99B99) LESS THAN 100)
000857,000842:
000858,000843: # -QQ-
000859,000844: # POSITION7 XXXX.X NAUT MI DP BIT 1 OF LOW REGISTER =
000860,000845: # (MAX 9058.9) -4
000861,000846: # 2 METERS
000862,000847:
000863,000848: # -RR-
000864,000849: # COMPUTED ALTITUDE XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000865,000850: # -4
000866,000851: # 2 METERS
000867,000852:
000868,000853: # -SS-
000869,000854: # DP DEGREES XXXX.X DEGREES DP BIT 1 OF HIGH REGISTER =
000870,000855: # 1 DEGREE
000871,000856:
000872,000857: # -TT-
000873,000858: # LANDING RADAR +0000X CHANNEL 33,BIT 6=NOT POSIT. 1
000874,000859: # POSITION (DECIMAL ONLY. CHANNEL 33,BIT 7=NOT POSIT. 2
000875,000860: # DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
000876,000861: # ONLY. CANNOT BE X = 2 FOR LR POSITION 2
000877,000862: # LOADED.)
000878,000863:
000879,000864: # -WW- 15
000880,000865: # 360-CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360 - (360/2 )
000881,000866: # (MAX 359.99) DEGREES
000882,000867: # (USES 15 BITS FOR MAGNI-
000883,000868: # TUDE AND 2-S COMP.)
000884,000869:
000885,000870: # -XX-
000886,000871: # POSITION 9 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
000887,000872: # (MAX 283.09) -9
000888,000873: # 2 METERS
000889,000874:
Page 21 |
000891,000876: # -YY-
000892,000877: # VELOCITY 4 XXXX.X FEET/SEC DP FRACTIONAL PART OF
000893,000878: # (MAX 328.0) METERS/CENTI-SEC
000894,000879: # THAT-S ALL ON THE NOUNS.
000895,000880:
Page 22 |
000897,000882: # ALARM CODES FOR LUMINARY
000898,000883:
000899,000884: # *9 *18 *60 COLUMN
000900,000885:
000901,000886: # CODE * TYPE SET BY
000902,000887:
000903,000888: # 00105 ** AOTMARK SYSTEM IN USE
000904,000889: # 00107 MORE THAN 5 MARK PAIRS AOTMARK
000905,000890: # 00111 MARK MISSING AOTMARK
000906,000891: # 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
000907,000892: # 00113 NO INBITS AOTMARK
000908,000893: # 00114 MARK MADE BUT NOT DESIRED AOTMARK
000909,000894: # 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
000910,000895: # 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING
000911,000896: # 00206 + GIMBAL LOCK.
000912,000897: # 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
000913,000898: # 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51, P57
000914,000899: # 00211 COARSE ALIGN ERROR IMU MODE SWITCH
000915,000900: # 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH,T4RPT
000916,000901: # 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
000917,000902: # 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
000918,000903: # 00217 BAD RETURN FROM IMUSTALL P51,P52,P57
000919,000904: # 00220 IMU NOT ALIGNED - NO REFSMMAT R02,R47
000920,000905: # 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
000921,000906: # FINDCDUW
000922,000907: # 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
000923,000908: # 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
000924,000909: # 00405 TWO STARS NOT AVAILABLE P52
000925,000910: # 00421 W-MATRIX OVERFLOW INTEGRV
000926,000911: # 00501 P RADAR ANTENNA OUT OF LIMITS R23
000927,000912: # 00502 BAD RADAR GIMBAL ANGLE INPUT V41N72
000928,000913: # 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V41N72
000929,000914: # 00510 RADAR AUTO DESCRETE NOT PRESENT R25
000930,000915: # 00511 LR NOT IN POSITION 2 OR REPOSITIONING SERVICER
000931,000916: # 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
000932,000917: # 00515 RR CDU FAIL DISCRETE PRESENT R25
000933,000918: # 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
000934,000919: # 00521 COULD NOT READ RADAR P20
000935,000920: # 00522 LANDING RADAR POSITION CHANGE RADAR READ
000936,000921: # 00523 P LR ANTENNA DIDN'T ACHIEVE POSITION 2 SERVICER, V60 (NON-P IN V60)
000937,000922: # 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
000938,000923: # 00526 P RANGE GREATER THAN 400 NAUT. MILES P20,P22
000939,000924: # 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21,R24
000940,000925: # LUNAR SURFACE
000941,000926: # OR VEHICLE MANEUVER REQUIRED R24 (20)
000942,000927: # 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
000943,000928: # 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32,P72,
000944,000929: # 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32,P72,
000945,000930: # 00603 CSI TO CDH TIME LT TMIN12 P32,P72,P33,P73
000946,000931: # 00604 CDH TO TPI TIME LT TMIN23 P32,P72,
Page 23 |
000948,000933: # OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
000949,000934: # 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
000950,000935: # 00606 DV EXCEEDS MAXIMUM P32,P72,
000951,000936: # 00611 NO TIG FOR GIVEN ELEV ANGLE P34,P74
000952,000937: # 00701 ILLEGAL OPTION CODE SELECTED (504 ONLY) P57
000953,000938: # 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
000954,000939: # 01102 AGC SELF TEST ERROR SELF CHECK
000955,000940: # 01103 ** UNUSED CCS BRANCH EXECUTED ABORT
000956,000941: # 01104 * DELAY ROUTINE BUSY EXEC
000957,000942: # 01105 DOWNLINK TOO FAST T4RUPT
000958,000943: # 01106 UPLINK TOO FAST T4RUPT
000959,000944: # 01107 PHASE TABLE FAILURE. ASSUME RESTART
000960,000945: # ERASABLE MEMORY IS SUSPECT. RESTART
000961,000946: # 01201 * EXECUTIVE OVERFLOW-NO VAC AREAS EXEC
000962,000947: # 01202 * EXECUTIVE OVERFLOW-NO CORE SETS EXEC
000963,000948: # 01203 * WAITLIST OVERFLOW-TOO MANY TASKS WAITLIST
000964,000949: # 01204 ** WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
000965,000950: # CALLED WITH ZERO OR NEGATIVE DELTA-TIME
000966,000951: # 01206 ** SECOND JOB ATTEMPTS TO GO TO SLEEP PINBALL
000967,000952: # 01206 VIA KYBD AND DISPLAY PROGRAM
000968,000953: # 01207 * NO VAC AREAS FOR MARKS AOTMARK
000969,000954: # 01210 * TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
000970,000955: # 01211 * ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
000971,000956: # 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
000972,000957: # 01302 ** SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
000973,000958: # 01406 ** BAD RETURN FROM ROOTPSRS LANDING GUIDANCE EQS.
000974,000959: # 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
000975,000960: # .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
000976,000961: # VECTOR.) S40.8
000977,000962: # 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
000978,000963: # 01412 DESCENT IGNALG NOT CONVERGING P63
000979,000964: # 01501 ** KEYBOARD AND DISPLAY ALARM DURING PINBALL
000980,000965: # 01501 INTERNAL USE (NVSUB).ABORT
000981,000966: # 01502 ** ILLEGAL FLASHING DISPLAY GOPLAY
000982,000967: # 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
000983,000968: # 01600 OVERFLOW IN DRIFT TEST IMU 4
000984,000969: # 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
000985,000970: # 01601 IMU 4 (LEM)
000986,000971: # 01703 IGNITION TIME SLIPPED MIDTOAVE
000987,000972: # 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
000988,000973: # CONFIGURATION P40, P42
000989,000974: # 02000 * DAP STILL IN PROGRESS AT NEXT TIME5 RUPT DAP
000990,000975: # 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
000991,000976: # 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
000992,000977: # 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
000993,000978: # 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
000994,000979: # 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
000995,000980: # 04777 ICDU , PIPA FAILS CAUSED THE ISS WARNING T4RUPT
000996,000981: # 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
000997,000982: # 10777 IMU , PIPA FAILS CAUSED THE ISS WARNING T4RUPT
Page 24 |
000999,000984: # 13777 IMU , ICDU FAILS CAUSED THE ISS WARNING T4RUPT
001000,000985: # 14777 IMU,ICDU,PIPA FAILS CAUSED THE ISSWNING T4RUPT
001001,000986: # * INDICATES AN ABORT CODE THAT RESULTS IN A SOFTWARE RESTART.
001002,000987:
001003,000988: # ** INDICATES A MORE SERIOUS ABORT CODE THAT RESULTS IN THE
001004,000989: # PROGRAM GOING TO R00.
001005,000990:
001006,000991: # P INDICATES A PRIORITY ALARM.
001007,000992:
001008,000993: # ALL OTHERS ARE NON-ABORTIVE
001009,000994:
Page 25 |
001011,000996: # CHECKLIST CODES FOR LUMINARY
001012,000997:
001013,000998: # *9 *17 *26 *9 COLUMN
001014,000999:
001015,001000: # R1CODE ACTION TO BE EFFECTED PROGRAM
001016,001001:
001017,001002: # 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
001018,001003: # 00014 KEY IN FINE ALIGN OPTION P51,P63,P57
001019,001004: # 00015 PERFORM CELESTIAL BODY ACQUISITION R51,P51
001020,001005: # 00062 SWITCH AGC POWER DOWN P06
001021,001006: # 00201 SWITCH RR MODE TO AUTOMATIC P20,P22,R04
001022,001007: # 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12,P42,P71
001023,001008: # ALSO THR CONT TO AUTO P40,P63,P70
001024,001009: # 00205 PERFORM MANUAL ACQUISITION OF RR R23
001025,001010: # 00500 SWITCH LR ANTENNA TO POSITION 1 P63
001026,001011:
001027,001012: # SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
001028,001013: # PERFORM DENOTES START OR END OF A TASK
001029,001014: # KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
001030,001015:
Page 26 |
001032,001017: # OPTION CODES FOR LUMINARY
001033,001018:
001034,001019: # THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
001035,001020: # CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
001036,001021: # ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
001037,001022:
001038,001023: # *9 *17 *52 *11 *25 COLUMN
001039,001024:
001040,001025: # OPTION
001041,001026: # CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
001042,001027:
001043,001028: # 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
001044,001029: # 4=LAND SITE
001045,001030: # 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
001046,001031: # 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
001047,001032: # 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
001048,001033: # 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
001049,001034: # 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
001050,001035: # 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
001051,001036: # 2=TWO BODIES 3=ONE BODY + G
001052,001037: # 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
001053,001038: # ORBIT TO PASS OVER LM
001054,001039:
End of include-file ASSEMBLY_AND_OPERATION_INFORMATION.agc. Parent file is MAIN.agc