Source Code
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These source-code files are part of a reconstructed copy of LM131 revision 1,
the final release of the Apollo 13 Lunar Module (LM) Apollo Guidance Computer
(AGC) software.
The source reconstruction began with source code of Luminary 131 previously
transcribed from a digitized copy of that program. A dump of the flight spare
core rope memory module B5, part number 2010802-171, serial number RAY 411,
was obtained. This module is the only module different between Luminary 131
and LM131 revision 1. The dump was disassembled and all changes were incorporated
into these source files. Note that page numbers in the reconstructed code match
those on the Luminary 131 printout, although the changed code would likely have
changed page numbers for a real LM131 revision 1 listing.
Comments from the original source code are prefixed with a single '#' symbol,
whereas comments added later are prefixed by "##" or "###". Report any errors
noted by creating an
issue report at the Virtual AGC
project's GitHub repository.
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000022,000002: ## Copyright: Public domain.
000023,000003: ## Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
000024,000004: ## Purpose: A section of LM131 revision 1.
000025,000005: ## It is part of the reconstructed source code for the final
000026,000006: ## release of the flight software for the Lunar Module's (LM)
000027,000007: ## Apollo Guidance Computer (AGC) for Apollo 13. The code has
000028,000008: ## been reconstructed from a listing of Luminary 131 and a dump
000029,000009: ## of a core rope memory module B5, part number 2010802-171,
000030,000010: ## which is the only module different between LM131 revision 1
000031,000011: ## and Luminary 131. The executable generated from this source
000032,000012: ## has been verified against the module dump, so while the names,
000033,000013: ## comments, and ordering may not be exactly correct, the
000034,000014: ## resulting binary is.
000035,000015: ## Reference: pp. 1-27
000036,000016: ## Assembler: yaYUL
000037,000017: ## Contact: Ron Burkey <info@sandroid.org>.
000038,000018: ## Website: www.ibiblio.org/apollo/index.html
000039,000019: ## Mod history: 2022-10-28 MAS Created from Luminary 131 and added a line
000040,000020: ## for alarm code 1466.
000041,000021:
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Page 1
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000043,000023:
000044,000024: # THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
000045,000025: # THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
000046,000026:
000047,000027: # GUIDANCE SYSTEM OPERATIONS PLAN
000048,000028: # FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
000049,000029: # USING PROGRAM LUMINARY
000050,000030:
000051,000031: # THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
000052,000032: # TECHNOLOGY 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS UNDER PROJECT 55-238-70, SPONSORED BY THE MANNED
000053,000033: # SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065.
000054,000034:
000055,000035: # THIS PROGRAM IS REFERRED TO AS LUMINARY 1C
000056,000036:
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Page 2
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000058,000038: # TABLE OF LOG CARDS
000059,000039: # ABSOLUTE ADDRESSES FOR UPDATE PROGRAM
000060,000040: # ASSEMBLY AND OPERATION INFORMATION
000061,000041: # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
000062,000042: # CONTROLLED CONSTANTS
000063,000043: # INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
000064,000044: # FLAGWORD ASSIGNMENTS
000065,000045: # SUBROUTINE CALLS
000066,000046:
000067,000047: # TABLE OF SUBROUTINE LOG SECTIONS
000068,000048: # LUMERASE
000069,000049: # ERASABLE ASSIGNMENTS
000070,000050: # LEMONAID
000071,000051: # INTERRUPT LEAD INS
000072,000052: # T4RUPT PROGRAM
000073,000053: # RCS FAILURE MONITOR
000074,000054: # DOWNLINK LISTS
000075,000055: # AGS INITIALIZATION
000076,000056: # FRESH START AND RESTART
000077,000057: # RESTART TABLES
000078,000058: # AOTMARK
000079,000059: # EXTENDED VERBS
000080,000060: # PINBALL NOUN TABLES
000081,000061: # LEM GEOMETRY
000082,000062: # IMU COMPENSATION PACKAGE
000083,000063: # R63
000084,000064: # ATTITUDE MANEUVER ROUTINE
000085,000065: # GIMBAL LOCK AVOIDANCE
000086,000066: # KALCMANU STEERING
000087,000067: # SYSTEM TEST STANDARD LEAD INS
000088,000068: # IMU PERFORMANCE TESTS 2
000089,000069: # IMU PERFORMANCE TESTS 4
000090,000070: # PINBALL GAMES BUTTONS AND LIGHTS
000091,000071: # R60,R62
000092,000072: # S-BAND ANTENNA FOR LM
000093,000073: # LEMP20S
000094,000074: # RADAR LEADIN ROUTINES
000095,000075: # P20-P25
000096,000076: # LEMP30S
000097,000077: # P30,P37
000098,000078: # P32-P35, P72-P75
000099,000079: # KISSING
000100,000080: # GROUND TRACKING DETERMINATION PROGRAM - P21
000101,000081: # P34-P35, P74-P75
000102,000082: # R31
000103,000083: # P76
000104,000084: # R30
000105,000085: # FLY
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Page 3
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000107,000087: # BURN, BABY, BURN -- MASTER IGNITION ROUTINE
000108,000088: # P40-P47
000109,000089: # THE LUNAR LANDING
000110,000090: # THROTTLE CONTROL ROUTINES
000111,000091: # LUNAR LANDING GUIDANCE EQUATIONS
000112,000092: # P70-P71
000113,000093: # P12
000114,000094: # ASCENT GUIDANCE
000115,000095: # SERVICER
000116,000096: # LANDING ANALOG DISPLAYS
000117,000097: # FINDCDUW - GUIDAP INTERFACE
000118,000098: # LEMP50S
000119,000099: # P51-P53
000120,000100: # LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
000121,000101: # SKIPPER
000122,000102: # DOWN-TELEMETRY PROGRAM
000123,000103: # INTER-BANK COMMUNICATION
000124,000104: # INTERPRETER
000125,000105: # FIXED-FIXED CONSTANT POOL
000126,000106: # INTERPRETIVE CONSTANTS
000127,000107: # SINGLE PRECISION SUBROUTINES
000128,000108: # EXECUTIVE
000129,000109: # WAITLIST
000130,000110: # LATITUDE LONGITUDE SUBROUTINES
000131,000111: # PLANETARY INERTIAL ORIENTATION
000132,000112: # MEASUREMENT INCORPORATION
000133,000113: # CONIC SUBROUTINES
000134,000114: # INTEGRATION INITIALIZATION
000135,000115: # ORBITAL INTEGRATION
000136,000116: # INFLIGHT ALIGNMENT ROUTINES
000137,000117: # POWERED FLIGHT SUBROUTINES
000138,000118: # TIME OF FREE FALL
000139,000119: # AGC BLOCK TWO SELF-CHECK
000140,000120: # PHASE TABLE MAINTENANCE
000141,000121: # RESTARTS ROUTINE
000142,000122: # IMU MODE SWITCHING ROUTINES
000143,000123: # KEYRUPT, UPRUPT
000144,000124: # DISPLAY INTERFACE ROUTINES
000145,000125: # SERVICE ROUTINES
000146,000126: # ALARM AND ABORT
000147,000127: # UPDATE PROGRAM
000148,000128: # RTB OP CODES
000149,000129: # LMDAP
000150,000130: # T6-RUPT PROGRAMS
000151,000131: # DAP INTERFACE SUBROUTINES
000152,000132: # DAPIDLER PROGRAM
000153,000133: # P-AXIS RCS AUTOPILOT
000154,000134: # Q,R-AXIS RCS AUTOPILOT
000155,000135: # TJET LAW
000156,000136: # KALMAN FILTER
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Page 4
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000158,000138: # TRIM GIMBAL CONTROL SYSTEM
000159,000139: # AOSTASK AND AOSJOB
000160,000140: # SPS BACK-UP RCS CONTROL
000161,000141:
000162,000142: # SYMBOL TABLE LISTING
000163,000143: # UNREFERENCED SYMBOL LISTING
000164,000144: # ERASABLE & EQUALS CROSS-REFERENCE TABLE
000165,000145: # SUMMARY OF SYMBOL TABLE LISTINGS
000166,000146: # MEMORY TYPE & AVAILABLITY DISPLAY
000167,000147: # COUNT TABLE
000168,000148: # PARAGRAPHS GENERATED FOR THIS ASSEMBLY
000169,000149: # OCTAL LISTING
000170,000150: # OCCUPIED LOCATIONS TABLE
000171,000151: # SUBROS CALLED & PROGRAM STATUS
000172,000152:
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Page 5
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000174,000154: # VERB LIST FOR LUMINARY
000175,000155:
000176,000156: # REGULAR VERBS
000177,000157:
000178,000158: # 00 NOT IN USE
000179,000159: # 01 DISPLAY OCTAL COMP 1 IN R1
000180,000160: # 02 DISPLAY OCTAL COMP 2 IN R1
000181,000161: # 03 DISPLAY OCTAL COMP 3 IN R1
000182,000162: # 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
000183,000163: # 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
000184,000164: # 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000185,000165: # 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
000186,000166: # 08
000187,000167: # 09
000188,000168: # 10
000189,000169: # 11 MONITOR OCTAL COMP 1 IN R1
000190,000170: # 12 MONITOR OCTAL COMP 2 IN R1
000191,000171: # 13 MONITOR OCTAL COMP 3 IN R1
000192,000172: # 14 MONITOR OCTAL COMP 1,2 IN R1,R2
000193,000173: # 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
000194,000174: # 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000195,000175: # 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
000196,000176: # 18
000197,000177: # 19
000198,000178: # 20
000199,000179: # 21 LOAD COMPONENT 1 INTO R1
000200,000180: # 22 LOAD COMPONENT 2 INTO R2
000201,000181: # 23 LOAD COMPONENT 3 INTO R3
000202,000182: # 24 LOAD COMPONENT 1,2 INTO R1,R2
000203,000183: # 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
000204,000184: # 26
000205,000185: # 27 DISPLAY FIXED MEMORY
000206,000186: # 28
000207,000187: # 29
000208,000188: # 30 REQUEST EXECUTIVE
000209,000189: # 31 REQUEST WAITLIST
000210,000190: # 32 RECYCLE PROGRAM
000211,000191: # 33 PROCEED WITHOUT DSKY INPUTS
000212,000192: # 34 TERMINATE FUNCTION
000213,000193: # 35 TEST LIGHTS
000214,000194: # 36 REQUEST FRESH START
000215,000195: # 37 CHANGE PROGRAM (MAJOR MODE)
000216,000196: # 38
000217,000197: # 39
000218,000198:
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Page 6
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000220,000200: # EXTENDED VERBS
000221,000201:
000222,000202: # 40 ZERO CDU-S
000223,000203: # 41 COARSE ALIGN CDU-S
000224,000204: # 42 FINE ALIGN IMU
000225,000205: # 43 LOAD IMU ATT ERROR METERS
000226,000206: # 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
000227,000207: # 45
000228,000208: # 46
000229,000209: # 47 INITIALIZE AGS (R47)
000230,000210: # 48 REQUEST DAP DATA LOAD ROUTINE (R03)
000231,000211: # 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
000232,000212: # 50 PLEASE PERFORM
000233,000213: # 51
000234,000214: # 52 MARK X-RETICLE
000235,000215: # 53 MARK Y-RETICLE
000236,000216: # 54 MARK X OR Y-RETICLE
000237,000217: # 55 INCREMENT AGC TIME (DECIMAL)
000238,000218: # 56 TERMINATE TRACKING (P20 + P25)
000239,000219: # 57 PERMIT LANDING RADAR UPDATES
000240,000220: # 58 INHIBIT LANDING RADAR UPDATES
000241,000221: # 59 COMMAND LR TO POSITION 2.
000242,000222: # 60 DISPLAY VEHICLE ATTITUDE RATES ON FDAI ERROR NEEDLES.
000243,000223: # 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
000244,000224: # 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
000245,000225: # 63 SAMPLE RADAR ONCE PER SECOND (R04).
000246,000226: # 64 REQUEST S-BAND ANTENNA ROUTINE (R05)
000247,000227: # 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
000248,000228: # 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
000249,000229: # 67 DISPLAY W MATRIX
000250,000230: # 68
000251,000231: # 69 CAUSE RESTART
000252,000232: # 70 UPDATE LIFTOFF TIME
000253,000233: # 71 UNIVERSAL UPDATE-BLOCK ADR
000254,000234: # 72 UNIVERSAL UPDATE-SINGLE ADR
000255,000235: # 73 UPDATE AGC TIME (OCTAL)
000256,000236: # 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
000257,000237: # 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
000258,000238: # 76 MINIMUM IMPULSE COMMAND MODE
000259,000239: # 77 RATE COMMAND AND ATTITUDE HOLD MODE
000260,000240: # 78 LR SPURIOUS RETURN TEST START (R77)
000261,000241: # 79 LR SPURIOUS RETURN TEST STOP
000262,000242: # 80 UPDATE LEM STATE VECTOR
000263,000243: # 81 UPDATE CSM STATE VECTOR
000264,000244: # 82 REQUEST ORBIT PARAM DISPLAY (R30)
000265,000245: # 83 REQUEST REND PARAM DISPLAY (R31)
000266,000246: # 84
000267,000247: # 85 DISPLAY RR LOS AZ AND ELEV
000268,000248: # 86
000269,000249: # 87
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Page 7
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000271,000251: # 88
000272,000252: # 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
000273,000253: # 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
000274,000254: # 91 DISPLAY BANK SUM
000275,000255: # 92 OPERATE IMU PERFORMANCE TEST (P07)
000276,000256: # 93 ENABLE W MATRIX INITIALIZATION
000277,000257: # 94
000278,000258: # 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
000279,000259: # 96 INTERRUPT INTEGRATION AND GO TO POO
000280,000260: # 97 PERFORM ENGINE FAIL PROCEDURE
000281,000261: # 98
000282,000262: # 99 PLEASE ENABLE ENGINE
000283,000263:
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Page 8
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000285,000265: # IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
000286,000266: # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
000287,000267: # SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
000288,000268: # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23
000289,000269: # MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
000290,000270: # ABOVE SCALE TYPES.
000291,000271:
000292,000272: # THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
000293,000273: # EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
000294,000274:
000295,000275: # NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000296,000276: # 00 NOT IN USE
000297,000277: # 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH
000298,000278: # 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH
000299,000279: # 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP XXX.XX DEG FOR EACH
000300,000280: # 04 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000301,000281: # 05 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000302,000282: # 06 OPTION CODE 3COMP OCTAL ONLY FOR EACH
000303,000283: # LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
000304,000284: # 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
000305,000285: # ONES FOR BITS TO BE MODIFIED
000306,000286: # 1 TO SET OR 0 TO RESET SELECTED BITS
000307,000287: # 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
000308,000288: # 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
000309,000289: # 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
000310,000290: # 11 TIG OF CSI 3COMP 00XXX. HRS DEC ONLY
000311,000291: # 000XX. MIN MUST LOAD 3 COMPS
000312,000292: # 0XX.XX SEC
000313,000293: # 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
000314,000294: # (USED BY EXTENDED VERBS ONLY)
000315,000295: # 13 TIG OF CDH 3COMP 00XXX. HRS DEC ONLY
000316,000296: # 000XX. MIN MUST LOAD 3 COMPS
000317,000297: # 0XX.XX SEC
000318,000298: # 14 CHECKLIST 3COMP XXXXX. FOR EACH
000319,000299: # (USED BY EXTENDED VERBS ONLY)
000320,000300: # (NOUN 25 IS PASTED AFTER DISPLAY)
000321,000301: # 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
000322,000302: # 16 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000323,000303: # (USED BY EXTENDED VERBS ONLY) 000XX. MIN MUST LOAD 3 COMPS
000324,000304: # 0XX.XX SEC
000325,000305: # 17 SPARE
000326,000306: # 18 AUTO MANEUVER BALL ANGLES 3COMP XXX.XX DEG FOR EACH
000327,000307: # 19 SPARE
000328,000308: # 20 ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000329,000309: # 21 PIPAS 3COMP XXXXX. PULSES FOR EACH
000330,000310: # 22 NEW ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000331,000311: # 23 SPARE
000332,000312: # 24 DELTA TIME FOR AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000333,000313: # 000XX. MIN MUST LOAD 3 COMPS
000334,000314: # 0XX.XX SEC
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Page 9
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000336,000316: # 25 CHECKLIST 3COMP XXXXX. FOR EACH
000337,000317: # (USED WITH PLEASE PERFORM ONLY)
000338,000318: # 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
000339,000319: # 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX.
000340,000320: # 28 SPARE
000341,000321: # 29 SPARE
000342,000322: # 30 SPARE
000343,000323: # 31 SPARE
000344,000324: # 32 TIME FROM PERIGEE 3COMP 00XXX. HRS DEC ONLY
000345,000325: # 000XX. MIN MUST LOAD 3 COMPS
000346,000326: # 0XX.XX SEC
000347,000327: # 33 TIME OF IGNITION 3COMP 00XXX. HRS DEC ONLY
000348,000328: # 000XX. MIN MUST LOAD 3 COMPS
000349,000329: # 0XX.XX SEC
000350,000330: # 34 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000351,000331: # 000XX. MIN MUST LOAD 3 COMPS
000352,000332: # 0XX.XX SEC
000353,000333: # 35 TIME FROM EVENT 3COMP 00XXX. HRS DEC ONLY
000354,000334: # 000XX. MIN MUST LOAD 3 COMPS
000355,000335: # 0XX.XX SEC
000356,000336: # 36 TIME OF AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000357,000337: # 000XX. MIN MUST LOAD 3 COMPS
000358,000338: # 0XX.XX SEC
000359,000339: # 37 TIG OF TPI 3COMP 00XXX. HRS DEC ONLY
000360,000340: # 000XX. MIN MUST LOAD 3 COMPS
000361,000341: # 0XX.XX SEC
000362,000342: # 38 TIME OF STATE BEING INTEGRATED 3COMP 00XXX. HRS DEC ONLY
000363,000343: # 000XX. MIN MUST LOAD 3 COMPS
000364,000344: # 0XX.XX SEC
000365,000345: # 39 SPARE
000366,000346:
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Page 10
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000368,000348: # MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000369,000349: # 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000370,000350: # VG, XXXX.X FT/SEC
000371,000351: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000372,000352: # 41 TARGET AZIMUTH , 2COMP XXX.XX DEG (FOR SYSTEM TEST)
000373,000353: # ELEVATION XX.XXX DEG
000374,000354: # 42 APOGEE, 3COMP XXXX.X NAUT MI DEC ONLY
000375,000355: # PERIGEE, XXXX.X NAUT MI
000376,000356: # DELTA V (REQUIRED) XXXX.X FT/SEC
000377,000357: # 43 LATITUDE, 3COMP XXX.XX DEG DEC ONLY
000378,000358: # LONGITUDE, XXX.XX DEG
000379,000359: # ALTITUDE XXXX.X NAUT MI
000380,000360: # 44 APOGEE, 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000381,000361: # PERIGEE, XXXX.X NAUT MI
000382,000362: # TFF XXBXX MIN/SEC
000383,000363: # 45 MARKS, 3COMP XXXXX. NO LOAD, DEC ONLY
000384,000364: # TFI OF NEXT BURN XXBXX MIN/SEC
000385,000365: # MGA XXX.XX DEG
000386,000366: # 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
000387,000367: # 47 LEM WEIGHT, 2COMP XXXXX. LBS DEC ONLY
000388,000368: # CSM WEIGHT XXXXX. LBS
000389,000369: # 48 GIMBAL PITCH TRIM, 2COMP XXX.XX DEG DEC ONLY
000390,000370: # GIMBAL ROLL TRIM XXX.XX DEG
000391,000371: # 49 DELTA R, 3COMP XXXX.X NAUT MI DEC ONLY
000392,000372: # DELTA V, XXXX.X FT/SEC
000393,000373: # RADAR DATA SOURCE CODE XXXXX.
000394,000374: # 50 SPARE
000395,000375: # 51 S-BAND ANTENNA ANGLES PITCH 2COMP XXX.XX DEG DEC ONLY
000396,000376: # YAW XXX.XX DEG
000397,000377: # 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG
000398,000378: # 53 SPARE
000399,000379: # 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
000400,000380: # RANGE RATE, XXXX.X FT/SEC
000401,000381: # THETA XXX.XX DEG
000402,000382: # 55 NO. OF APSIDAL CROSSINGS 3COMP XXXXX. DEC ONLY
000403,000383: # ELEVATION ANGLE XXX.XX DEG
000404,000384: # CENTRAL ANGLE OF PASSIVE VEHICLE XXX.XX DEG
000405,000385: # 56 RR LOS AZIMUTH 2COMP XXX.XX DEG
000406,000386: # ELEVATION XXX.XX DEG
000407,000387: # 57 SPARE
000408,000388: # 58 PERIGEE ALT (POST TPI) 3COMP XXXX.X NAUT MI DEC ONLY
000409,000389: # DELTA V TPI XXXX.X FT/SEC
000410,000390: # DELTA V TPF XXXX.X FT/SEC
000411,000391: # 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY
000412,000392: # 60 FORWARD VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000413,000393: # ALTITUDE RATE XXXX.X FT/SEC
000414,000394: # COMPUTED ALTITUDE XXXXX. FEET
000415,000395: # 61 TIME TO GO IN BRAKING PHASE 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000416,000396: # TIME FROM IGNITION XXBXX MIN/SEC
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Page 11
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000418,000398: # CROSS RANGE DISTANCE XXXX.X NAUT MI
000419,000399: # 62 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC NO LOAD, DEC ONLY
000420,000400: # TIME FROM IGNITION XXBXX MIN/SEC
000421,000401: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000422,000402: # 63 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000423,000403: # ALTITUDE RATE XXXX.X FT/SEC
000424,000404: # COMPUTED ALTITUDE XXXXX. FEET
000425,000405: # 64 TIME LEFT FOR REDESIGNATION- LPD ANGLE 3COMP XXBXX NO LOAD, DEC ONLY
000426,000406: # ALTITUDE RATE XXXX.X FT/SEC
000427,000407: # COMPUTED ALTITUDE XXXXX. FEET
000428,000408: # 65 SAMPLED AGC TIME 3COMP 00XXX. HRS DEC ONLY
000429,000409: # (FETCHED IN INTERRUPT) 000XX. MIN MUST LOAD 3 COMPS
000430,000410: # 0XX.XX SEC
000431,000411: # 66 LR RANGE 2COMP XXXXX. FEET NO LOAD, DEC ONLY
000432,000412: # POSITION +0000X
000433,000413: # 67 LRVX 3COMP XXXXX. FT/SEC
000434,000414: # LRVY XXXXX. FT/SEC
000435,000415: # LRVZ XXXXX. FT/SEC
000436,000416: # 68 SLANT RANGE TO LANDING SITE 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000437,000417: # TIME TO GO IN BRAKING PHASE XXBXX MIN/SEC
000438,000418: # LR ALTITUDE - COMPUTED ALTITUDE XXXXX. FEET
000439,000419: # 69 LANDING SITE CORRECTION, Z-COMPONENT 3COMP XXXXX. FEET DEC ONLY
000440,000420: # LANDING SITE CORRECTION, Y-COMPONENT XXXXX. FEET
000441,000421: # LANDING SITE CORRECTION, X-COMPONENT XXXXX. FEET
000442,000422: # 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000443,000423: # 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000444,000424: # 72 RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000445,000425: # SHAFT ANGLE XXX.XX DEG
000446,000426: # 73 NEW RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000447,000427: # SHAFT ANGLE XXX.XX DEG
000448,000428: # 74 TIME FROM IGNITION 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000449,000429: # YAW AFTER VEHICLE RISE XXX.XX DEG
000450,000430: # PITCH AFTER VEHICLE RISE XXX.XX DEG
000451,000431: # 75 DELTA ALTITUDE CDH 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000452,000432: # DELTA TIME (CDH-CSI OR TPI-CDH) XXBXX MIN/SEC
000453,000433: # DELTA TIME (TPI-CDH OR TPI-NONTPI) XXBXX MIN/SEC
000454,000434: # 76 DESIRED HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000455,000435: # DESIRED RADIAL VELOCITY XXXX.X FT/SEC
000456,000436: # CROSS-RANGE DISTANCE XXXX.X NAUT MI
000457,000437: # 77 TIME TO ENGINE CUTOFF 2COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000458,000438: # VELOCITY NORMAL TO CSM PLANE XXXX.X FT/SEC
000459,000439: # 78 RR RANGE 3COMP XXX.XX NAUT MI NO LOAD, DEC ONLY
000460,000440: # RANGE RATE XXXXX. FT/SEC
000461,000441: # TIME FROM IGNITION XXBXX MIN/SEC
000462,000442: # 79 CURSOR ANGLE 3COMP XXX.XX DEG DEC ONLY
000463,000443: # SPIRAL ANGLE XXX.XX DEG
000464,000444: # POSITION CODE XXXXX.
000465,000445: # 80 DATA INDICATOR, 2COMP XXXXX.
000466,000446: # OMEGA XXX.XX DEG
000467,000447: # 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
|
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Page 12
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000469,000449: # 82 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000470,000450: # 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000471,000451: # 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000472,000452: # 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000473,000453: # 86 VG (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000474,000454: # 87 BACKUP OPTICS LOS AZIMUTH 2COMP XXX.XX DEG
000475,000455: # ELEVATION XXX.XX DEG
000476,000456: # 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY
000477,000457: # 89 LANDMARK LATITUDE 3COMP XX.XXX DEG DEC ONLY
000478,000458: # LONGITUDE/2 XX.XXX DEC
000479,000459: # ALTITUDE XXX.XX NAUT MI
000480,000460: # 90 Y 3COMP XXX.XX NM DEC ONLY
000481,000461: # Y DOT XXXX.X FPS
000482,000462: # PSI XXX.XX DEG
000483,000463: # 91 ALTITUDE 3COMP XXXXXB. NAUT MI
000484,000464: # VELOCITY XXXXX. FT/SEC
000485,000465: # FLIGHT PATH ANGLE XXX.XX DEG
000486,000466: # 92 PCT FTP (10,5K LB) AT PRESENT THRUST 3COMP XXXXX.
000487,000467: # ALTITUDE RATE XXXX.X FT/SEC
000488,000468: # COMPUTED ALTITUDE XXXXX. FEET
000489,000469: # 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
000490,000470: # 94 SPARE
000491,000471: # 95 SPARE
000492,000472: # 96 SPARE
000493,000473: # 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH
000494,000474: # 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX.
000495,000475: # .XXXXX
000496,000476: # XXXXX.
000497,000477: # 99 RMS IN POSITION 3COMP XXXXX. FT DEC ONLY
000498,000478: # RMS IN VELOCITY XXXX.X FT/SEC
000499,000479: # RMS IN BIAS XX.XXX RADIANS
000500,000480:
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Page 13
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000502,000482: # REGISTERS AND SCALING FOR NORMAL NOUNS
000503,000483:
000504,000484: # NOUN REGISTER SCALE TYPE
000505,000485: # 00 NOT IN USE
000506,000486: # 01 SPECIFY ADDRESS B
000507,000487: # 02 SPECIFY ADDRESS C
000508,000488: # 03 SPECIFY ADDRESS D
000509,000489: # 04 DSPTEM1 H
000510,000490: # 05 DSPTEM1 H
000511,000491: # 06 OPTION1 A
000512,000492: # 07 XREG A
000513,000493: # 08 ALMCADR A
000514,000494: # 09 FAILREG A
000515,000495: # 10 SPECIFY CHANNEL A
000516,000496: # 11 TCSI K
000517,000497: # 12 OPTIONX A
000518,000498: # 13 TCDH K
000519,000499: # 14 DSPTEMX C
000520,000500: # 15 INCREMENT ADDRESS A
000521,000501: # 16 DSPTEMX K
000522,000502: # 17 SPARE
000523,000503: # 18 FDAIX D
000524,000504: # 19 SPARE
000525,000505: # 20 CDUX D
000526,000506: # 21 PIPAX C
000527,000507: # 22 THETAD D
000528,000508: # 23 SPARE
000529,000509: # 24 DSPTEM2 +1 K
000530,000510: # 25 DSPTEM1 C
000531,000511: # 26 DSPTEM1 A
000532,000512: # 27 SMODE C
000533,000513: # 28 SPARE
000534,000514: # 29 SPARE
000535,000515: # 30 SPARE
000536,000516: # 31 SPARE
000537,000517: # 32 -TPER K
000538,000518: # 33 TIG K
000539,000519: # 34 DSPTEM1 K
000540,000520: # 35 TTOGO K
000541,000521: # 36 TIME2 K
000542,000522: # 37 TTPI K
000543,000523: # 38 TET K
000544,000524: # 39 SPARE
000545,000525:
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Page 14
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000547,000527: # REGISTERS AND SCALING FOR MIXED NOUNS
000548,000528:
000549,000529: # NOUN COMP REGISTER SCALE TYPE
000550,000530: # 40 1 TTOGO L
000551,000531: # 2 VGDISP S
000552,000532: # 3 DVTOTAL S
000553,000533: # 41 1 DSPTEM1 D
000554,000534: # 2 DSPTEM1 +1 E
000555,000535: # 42 1 HAPO Q
000556,000536: # 2 HPER Q
000557,000537: # 3 VGDISP S
000558,000538: # 43 1 LAT H
000559,000539: # 2 LONG H
000560,000540: # 3 ALT Q
000561,000541: # 44 1 HAPOX Q
000562,000542: # 2 HPERX Q
000563,000543: # 3 TFF L
000564,000544: # 45 1 TRKMKCNT C
000565,000545: # 2 TTOGO L
000566,000546: # 3 +MGA H
000567,000547: # 46 1 DAPDATR1 A
000568,000548: # 47 1 LEMMASS KK
000569,000549: # 2 CSMMASS KK
000570,000550: # 48 1 PITTIME NN
000571,000551: # 2 ROLLTIME NN
000572,000552: # 49 1 R22DISP Q
000573,000553: # 2 R22DISP +2 S
000574,000554: # 3 WHCHREAD C
000575,000555: # 50 SPARE
000576,000556: # 51 1 ALPHASB H
000577,000557: # 2 BETASB H
000578,000558: # 52 1 ACTCENT H
000579,000559: # 53 SPARE
000580,000560: # 54 1 RANGE JJ
000581,000561: # 2 RRATE S
000582,000562: # 3 RTHETA H
000583,000563: # 55 1 NN C
000584,000564: # 2 ELEV H
000585,000565: # 3 CENTANG H
000586,000566: # 56 1 RR-AZ H
000587,000567: # 2 RR-ELEV H
000588,000568: # 57 SPARE
000589,000569: # 58 1 POSTTPI Q
000590,000570: # 2 DELVTPI S
000591,000571: # 3 DELVTPF S
000592,000572: # 59 1 DVLOS S
000593,000573: # 2 DVLOS +2 S
000594,000574: # 3 DVLOS +4 S
000595,000575: # 60 1 FORVEL CC
|
|
Page 15
|
000597,000577: # 2 HDOTDISP S
000598,000578: # 3 HCALC1 RR
000599,000579: # 61 1 TTFDISP L
000600,000580: # 2 TTOGO L
000601,000581: # 3 OUTOFPLN QQ
000602,000582: # 62 1 ABVEL S
000603,000583: # 2 TTOGO L
000604,000584: # 3 DVTOTAL S
000605,000585: # 63 1 ABVEL S
000606,000586: # 2 HDOTDISP S
000607,000587: # 3 HCALC1 RR
000608,000588: # 64 1 FUNNYDSP PP
000609,000589: # 2 HDOTDISP S
000610,000590: # 3 HCALC RR
000611,000591: # 65 1 SAMPTIME K
000612,000592: # 2 SAMPTIME K
000613,000593: # 3 SAMPTIME K
000614,000594: # 66 1 RSTACK +6 W
000615,000595: # 2 CHANNEL 33 TT
000616,000596: # 67 1 RSTACK X
000617,000597: # 2 RSTACK +2 Y
000618,000598: # 3 RSTACK +4 Z
000619,000599: # 68 1 RANGEDSP QQ
000620,000600: # 2 TTFDISP L
000621,000601: # 3 DELTAH RR
000622,000602: # 69 1 DLANDZ RR
000623,000603: # 2 DLANDY RR
000624,000604: # 3 DLANDX RR
000625,000605: # 70 1 AOTCODE A
000626,000606: # 2 AOTCODE +1 A
000627,000607: # 3 AOTCODE +2 A
000628,000608: # 71 1 AOTCODE A
000629,000609: # 2 AOTCODE +1 A
000630,000610: # 3 AOTCODE +2 A
000631,000611: # 72 1 CDUT WW
000632,000612: # 2 CDUS D
000633,000613: # 73 1 TANG WW
000634,000614: # 2 TANG +1 D
000635,000615: # 74 1 TTOGO L
000636,000616: # 2 YAW H
000637,000617: # 3 PITCH H
000638,000618: # 75 1 DIFFALT Q
000639,000619: # 2 T1TOT2 L
000640,000620: # 3 T2TOT3 L
000641,000621: # 76 1 ZDOTD S
000642,000622: # 2 RDOTD S
000643,000623: # 3 XRANGE Q
000644,000624: # 77 1 TTOGO L
000645,000625: # 2 YDOT S
000646,000626: # 78 1 DNRRANGE U
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|
Page 16
|
000648,000628: # 2 DNRRDOT V
000649,000629: # 3 TTOTIG L
000650,000630: # 79 1 CURSOR D
000651,000631: # 2 SPIRAL D
000652,000632: # 3 POSCODE C
000653,000633: # 80 1 DATAGOOD C
000654,000634: # 2 OMEGAD H
000655,000635: # 81 1 DELVLVC S
000656,000636: # 2 DELVLVC +2 S
000657,000637: # 3 DELVLVC +4 S
000658,000638: # 82 1 DELVLVC S
000659,000639: # 2 DELVLVC +2 S
000660,000640: # 3 DELVLVC +4 S
000661,000641: # 83 1 DELVIMU S
000662,000642: # 2 DELVIMU +2 S
000663,000643: # 3 DELVIMU +4 S
000664,000644: # 84 1 DELVOV S
000665,000645: # 2 DELVOV +2 S
000666,000646: # 3 DELVOV +4 S
000667,000647: # 85 1 VGBODY S
000668,000648: # 2 VGBODY +2 S
000669,000649: # 3 VGBODY +4 S
000670,000650: # 86 1 DELVLVC S
000671,000651: # 2 DELVLVC +2 S
000672,000652: # 3 DELVLVC +4 S
000673,000653: # 87 1 AZ D
000674,000654: # 2 EL D
000675,000655: # 88 1 STARAD B
000676,000656: # 2 STARAD +2 B
000677,000657: # 3 STARAD +4 B
000678,000658: # 89 1 LANDLAT G
000679,000659: # 2 LANDLONG G
000680,000660: # 3 LANDALT JJ
000681,000661: # 90 1 RANGE JJ
000682,000662: # 2 RRATE S
000683,000663: # 3 RTHETA H
000684,000664: # 91 1 P21ALT Q (MEMORY/100 TO DIPLAY TENS N.M.)
000685,000665: # 2 P21VEL P
000686,000666: # 3 P21GAM H
000687,000667: # 92 1 THRDISP C
000688,000668: # 2 HDOTDISP S
000689,000669: # 3 HCALC1 RR
000690,000670: # 93 1 OGC G
000691,000671: # 2 OGC +2 G
000692,000672: # 3 OGC +4 G
000693,000673: # 94 SPARE
000694,000674: # 95 SPARE
000695,000675: # 96 SPARE
000696,000676: # 97 1 DSPTEM1 C
000697,000677: # 2 DSPTEM1 +1 C
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|
Page 17
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000699,000679: # 3 DSPTEM1 +2 C
000700,000680: # 98 1 DSPTEM2 C
000701,000681: # 2 DSPTEM2 +1 B
000702,000682: # 3 DSPTEM2 +2 C
000703,000683: # 99 1 WWPOS XX
000704,000684: # 2 WWVEL YY
000705,000685: # 3 WWBIAS AAA
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|
Page 18
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000707,000687: # NOUN SCALES AND FORMATS
000708,000688:
000709,000689: # -SCALE TYPE- PRECISION
000710,000690: # UNITS DECIMAL FORMAT -- AGC FORMAT
000711,000691: # ------------ -------------- -- ----------
000712,000692:
000713,000693: # -A-
000714,000694: # OCTAL XXXXX SP OCTAL
000715,000695:
000716,000696: # -B- -14
000717,000697: # FRACTIONAL .XXXXX SP BIT 1 = 2 UNITS
000718,000698: # (MAX .99996)
000719,000699:
000720,000700: # -C-
000721,000701: # WHOLE XXXXX. SP BIT 1 = 1 UNIT
000722,000702: # (MAX 16383.)
000723,000703:
000724,000704: # -D- 15
000725,000705: # CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360/2 DEGREES
000726,000706: # (MAX 359.99) (USES 15 BITS FOR MAGNI-
000727,000707: # TUDE AND 2-S COMP.)
000728,000708:
000729,000709: # -E- 14
000730,000710: # ELEVATION DEGREES XX.XXX DEGREES SP BIT 1 = 90/2 DEGREES
000731,000711: # (MAX 89.999)
000732,000712:
000733,000713: # -F- 14
000734,000714: # DEGREES (180) XXX.XX DEGREES SP BIT 1 = 180/2 DEGREES
000735,000715: # (MAX 179.99)
000736,000716:
000737,000717: # -G-
000738,000718: # DP DEGREES (90) XX.XXX DEGREES DP BIT 1 OF LOW REGISTER =
000739,000719: # 28
000740,000720: # 360/2 DEGREES
000741,000721:
000742,000722: # -H-
000743,000723: # DP DEGREES (360) XXX.XX DEGREES DP BIT 1 OF LOW REGISTER =
000744,000724: # 28
000745,000725: # (MAX 359.99) 360/2 DEGREES
000746,000726:
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|
Page 19
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000748,000728: # -K-
000749,000729: # TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER =
000750,000730: # 000XX. MIN -2
000751,000731: # 0XX.XX SEC 10 SEC
000752,000732: # (DECIMAL ONLY.
000753,000733: # MAX MIN COMP=59
000754,000734: # MAX SEC COMP=59.99
000755,000735: # MAX CAPACITY=745 HRS
000756,000736: # 39 MINS
000757,000737: # 14.55 SECS.
000758,000738: # WHEN LOADING, ALL 3
000759,000739: # COMPONENTS MUST BE
000760,000740: # SUPPLIED.)
000761,000741:
000762,000742: # -L-
000763,000743: # TIME (MIN/SEC) XXBXX MIN/SEC DP BIT 1 OF LOW REGISTER =
000764,000744: # (B IS A BLANK -2
000765,000745: # POSITION, DECIMAL 10 SEC
000766,000746: # ONLY, DISPLAY OR
000767,000747: # MONITOR ONLY. CANNOT
000768,000748: # BE LOADED.
000769,000749: # MAX MIN COMP=59
000770,000750: # MAX SEC COMP=59
000771,000751: # VALUES GREATER THAN
000772,000752: # 59 MIN 59 SEC
000773,000753: # ARE DISPLAYED AS
000774,000754: # 59 MIN 59 SEC.)
000775,000755:
000776,000756: # -M- -2
000777,000757: # TIME (SEC) XXX.XX SEC SP BIT 1 = 10 SEC
000778,000758: # (MAX 163.83)
000779,000759:
000780,000760: # -N-
000781,000761: # TIME(SEC) DP XXX.XX SEC DP BIT 1 OF LOW REGISTER =
000782,000762: # -2
000783,000763: # 10 SEC
000784,000764:
000785,000765: # -P-
000786,000766: # VELOCITY 2 XXXXX. FEET/SEC DP BIT 1 OF HIGH REGISTER =
000787,000767: # (MAX 41994.) -7
000788,000768: # 2 METERS/CENTI-SEC
000789,000769:
000790,000770: # -Q-
000791,000771: # POSITION 4 XXXX.X NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
000792,000772: # 2 METERS
000793,000773:
000794,000774: # -S-
000795,000775: # VELOCITY 3 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
000796,000776: # -7
000797,000777: # 2 METERS/CENTI-SEC
000798,000778:
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|
Page 20
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000800,000780: # -T- -2
000801,000781: # G XXX.XX G SP BIT 1 = 10 G
000802,000782: # (MAX 163.83)
000803,000783:
000804,000784: # -U-
000805,000785: # RENDEZVOUS XXX.XX NAUT MI SP USES 15 BITS FOR UNSIGNED
000806,000786: # RADAR RANGE (DECIMAL ONLY. MAGNITUDE.
000807,000787: # DISPLAY OR MONITOR BIT 1 = 9.38 FEET
000808,000788: # ONLY. CANNOT BE
000809,000789: # LOADED.)
000810,000790:
000811,000791: # -V-
000812,000792: # RENDEZVOUS XXXXX. FEET/SEC SP USES 15 BITS FOR UNSIGNED
000813,000793: # RADAR RANGE RATE (DECIMAL ONLY. MAGNITUDE.
000814,000794: # DISPLAY OR MONITOR BIT 1 = -.6278 FEET/SEC
000815,000795: # ONLY. CANNOT BE
000816,000796: # LOADED.
000817,000797: # BIAS OF 17000 COUNTS
000818,000798: # SUBTRACTED BEFORE
000819,000799: # DISPLAY.)
000820,000800:
000821,000801: # -W-
000822,000802: # LANDING RADAR XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000823,000803: # ALTITUDE WORD = 1.079 FEET
000824,000804:
000825,000805: # -X-
000826,000806: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000827,000807: # VELX WORD = -.6440 FEET/SEC
000828,000808:
000829,000809: # -Y-
000830,000810: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000831,000811: # VELY WORD = 1.212 FEET/SEC
000832,000812:
000833,000813: # -Z-
000834,000814: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000835,000815: # VELZ WORD = .8668 FEET/SEC
000836,000816:
000837,000817: # -AA-
000838,000818: # INITIAL/FINAL XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000839,000819: # ALTITUDE WORD = 2.345 FEET
000840,000820:
000841,000821: # -BB-
000842,000822: # ALTITUDE RATE XXXXX. FEET/SEC SP LOW ORDER BIT = .5
000843,000823: # (MAX 08191.) FEET/SEC
000844,000824:
000845,000825: # -CC-
000846,000826: # FORWARD/LATERAL XXXX.X FEET/SEC SP LOW ORDER BIT = .5571
000847,000827: # VELOCITY (MAX 09126.) FEET/SEC
000848,000828:
000849,000829: # -DD-
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Page 21
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000851,000831: # ROTATIONAL HAND XXXXX. DEG/SEC SP FRACTIONAL PART OF PI RAD
000852,000832: # CONTROLLER ANGULAR (MAX 00044.) 4 SEC
000853,000833: # RATES
000854,000834:
000855,000835: # -EE-
000856,000836: # OPTICAL TRACKER XXX.XX DEG. DP LOW ORDER BIT OF LOW ORDER
000857,000837: # AZIMUTH ANGLE 15
000858,000838: # WORD = 360/2 DEGREES
000859,000839:
000860,000840: # -JJ-
000861,000841: # POSITION5 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
000862,000842: # 2 METERS
000863,000843:
000864,000844: # -KK- 16
000865,000845: # WEIGHT2 XXXXX. LBS SP FRACTIONAL PART OF 2 KG
000866,000846:
000867,000847: # -NN-
000868,000848: # TRIM DEGREES 2 XXX.XX DEG SP BIT 1=.01 SEC(TIME)
000869,000849: # (MAX 032.76)
000870,000850:
000871,000851: # -PP-
000872,000852: # 2 INTEGERS +XXBYY DP BIT 1 OF HIGH REGISTER =
000873,000853: # (B IS A BLANK 1 UNIT OF XX
000874,000854: # POSITION. DECIMAL BIT 1 OF LOW REGISTER =
000875,000855: # ONLY, DISPLAY OR 1 UNIT OF YY
000876,000856: # MONITOR ONLY. CANNOT (EACH REGISTER MUST
000877,000857: # BE LOADED.) CONTAIN A POSITIVE INTEGER
000878,000858: # (MAX 99B99) LESS THAN 100)
000879,000859:
000880,000860: # -QQ-
000881,000861: # POSITION7 XXXX.X NAUT MI DP BIT 1 OF LOW REGISTER =
000882,000862: # (MAX 9058.9) -4
000883,000863: # 2 METERS
000884,000864:
000885,000865: # -RR-
000886,000866: # COMPUTED ALTITUDE XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000887,000867: # -4
000888,000868: # 2 METERS
000889,000869:
000890,000870: # -SS-
000891,000871: # DP DEGREES XXXX.X DEGREES DP BIT 1 OF HIGH REGISTER =
000892,000872: # 1 DEGREE
000893,000873:
000894,000874: # -TT-
000895,000875: # LANDING RADAR +0000X CHANNEL 33, BIT 6 = NOT POSIT. 1
000896,000876: # POSITION (DECIMAL ONLY. CHANNEL 33, BIT 7 = NOT POSIT. 2
000897,000877: # DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
000898,000878: # ONLY. CANNOT BE X = 2 FOR LR POSITION 2
000899,000879: # LOADED.)
000900,000880:
000901,000881: # -WW- 15
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Page 22
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000903,000883: # 360-CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360 - (360/2 )
000904,000884: # (MAX 359.99) DEGREES
000905,000885: # (USES 15 BITS FOR MAGNI-
000906,000886: # TUDE AND 2-S COMP.)
000907,000887:
000908,000888: # -XX-
000909,000889: # POSITION 9 XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000910,000890: # -9
000911,000891: # 2 METERS
000912,000892:
000913,000893: # -YY-
000914,000894: # VELOCITY 4 XXXX.X FEET/SEC DP FRACTIONAL PART OF
000915,000895: # (MAX 328.0) METERS/CENTI-SEC
000916,000896:
000917,000897: # -AAA-
000918,000898: # RADIANS XX.XXX RADIANS DP BIT 1 OF HIGH REGISTER =
000919,000899: # (MAX 31.999) -9
000920,000900: # 2 RADIANS
000921,000901:
000922,000902:
000923,000903: # THAT-S ALL ON THE NOUNS.
000924,000904:
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Page 23
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000926,000906: # ALARM CODES FOR LUMINARY
000927,000907:
000928,000908: # *9 *18 *60 COLUMN
000929,000909:
000930,000910: # CODE * TYPE SET BY
000931,000911:
000932,000912: # 00107 MORE THAN 5 MARK PAIRS AOTMARK
000933,000913: # 00111 MARK MISSING AOTMARK
000934,000914: # 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
000935,000915: # 00113 NO INBITS AOTMARK
000936,000916: # 00114 MARK MADE BUT NOT DESIRED AOTMARK
000937,000917: # 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
000938,000918: # 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING
000939,000919: # 00206 + GIMBAL LOCK.
000940,000920: # 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
000941,000921: # 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51, P57
000942,000922: # 00211 COARSE ALIGN ERROR IMU MODE SWITCH
000943,000923: # 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH, T4RPT
000944,000924: # 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
000945,000925: # 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
000946,000926: # 00217 BAD RETURN FROM IMUSTALL P51, P52, P57
000947,000927: # 00220 IMU NOT ALIGNED - NO REFSMMAT R02, R47
000948,000928: # 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
000949,000929: # FINDCDUW
000950,000930: # 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
000951,000931: # 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
000952,000932: # 00405 TWO STARS NOT AVAILABLE P52
000953,000933: # 00421 W-MATRIX OVERFLOW INTEGRV
000954,000934: # 00501 P RADAR ANTENNA OUT OF LIMITS R23
000955,000935: # 00502 BAD RADAR GIMBAL ANGLE INPUT V41N72
000956,000936: # 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V41N72
000957,000937: # 00510 RADAR AUTO DESCRETE NOT PRESENT R25
000958,000938: # 00511 L4 NOT IN POSITION 2 OR REPOSITIONING SERVICER
000959,000939: # 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
000960,000940: # 00515 RR CDU FAIL DISCRETE PRESENT R25
000961,000941: # 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
000962,000942: # 00521 COULD NOT READ RADAR P20
000963,000943: # 00522 LANDING RADAR POSITION CHANGE RADAR READ
000964,000944: # 00523 P LR ANTENNA DIDN'T ACHIEVE POSITION 2 SERVICER, V60 (NON-P IN V60)
000965,000945: # 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
000966,000946: # 00526 P RANGE GREATER THAN 400 NAUT. MILES P20, P22
000967,000947: # 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21, R24
000968,000948: # LUNAR SURFACE
000969,000949: # OR VEHICLE MANEUVER REQUIRED R24 (20)
000970,000950: # 00530 P LOS NOT IN MODE2 COVERAGE R21
000971,000951: # ON LUNAR SURFACE AFTER 600 SECS.
000972,000952: # 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
000973,000953: # 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32, P72,
000974,000954: # 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32, P72,
000975,000955: # 00603 CSI TO CDH TIME LT TMIN12 P32, P72, P33, P73
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000977,000957: # 00604 CDH TO TPI TIME LT TMIN23 P32, P72,
000978,000958: # OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
000979,000959: # 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
000980,000960: # 00606 DV EXCEEDS MAXIMUM P32, P72,
000981,000961: # 00611 NO TIG FOR GIVEN ELEV ANGLE P34, P74
000982,000962: # 00701 ILLEGAL OPTION CODE SELECTED P57
000983,000963: # 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
000984,000964: # 01102 AGC SELF TEST ERROR SELF CHECK
000985,000965: # 01105 DOWNLINK TOO FAST T4RUPT
000986,000966: # 01106 UPLINK TOO FAST T4RUPT
000987,000967: # 01107 PHASE TABLE FAILURE. ASSUME RESTART
000988,000968: # ERASABLE MEMORY IS SUSPECT. RESTART
000989,000969: # 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
000990,000970: # 01406 BAD RETURN FROM ROOTPSRS DESCENT GUIDANCE EQS.
000991,000971: # 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
000992,000972: # .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
000993,000973: # VECTOR.) S40.8
000994,000974: # 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
000995,000975: # 01412 DESCENT IGNALG NOT CONVERGING P63
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The following alarm code was added in LM131 rev 1.
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000997,000977: # 01466 INSUF. THROTTLINGS BETWEEN SKIPPED THROTS P66
000998,000978: # 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
000999,000979: # 01600 OVERFLOW IN DRIFT TEST IMU 4
001000,000980: # 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
001001,000981: # 01601 IMU 4 (LEM)
001002,000982: # 01703 IGNITION TIME SLIPPED MIDTOAVE
001003,000983: # 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
001004,000984: # CONFIGURATION P40, P42
001005,000985: # 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
001006,000986: # 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
001007,000987: # 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
001008,000988: # 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
001009,000989: # 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
001010,000990: # 04777 ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001011,000991: # 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
001012,000992: # 10777 IMU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001013,000993: # 13777 IMU, ICDU FAILS CAUSED THE ISS WARNING T4RUPT
001014,000994: # 14777 IMU, ICDU, PIPA FAILS CAUSED ISS WARNING T4RUPT
001015,000995:
001016,000996: # THE FOLLOWING CODES INDICATE THE MORE SERIOUS POODOO ABORTS THAT RESULT
001017,000997: # IN THE PROGRAM GOING TO ROO.
001018,000998:
001019,000999: # 20105 AOTMARK SYSTEM IN USE AOTMARK
001020,001000: # 20430 ACCELERATION OVERFLOW IN INTEGRATION ORBITAL INTEGRATION
001021,001001: # 20607 NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET, TIMERAD
001022,001002: # 21103 UNUSED CCS BRANCH EXECUTED ABORT
001023,001003: # 21204 WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
001024,001004: # CALLED WITH ZERO OR NEGATIVE DELTA-TIME
001025,001005: # 21302 SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
001026,001006: # 21406 BAD RETURN FROM ROOTPSRS IGNITION ALGORITHMN
001027,001007: # 21501 KEYBOARD AND DISPLAY ALARM DURING PINBALL
001028,001008: # INTERNAL USE(NVSUB).ABORT
001029,001009:
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001031,001011: # THE FOLLOWING CODES INDICATE A BAILOUT ABORT THAT RESULTS IN A SOFTWARE
001032,001012: # RESTART
001033,001013:
001034,001014: # 31104 DELAY ROUTINE BUSY EXEC
001035,001015: # 31201 EXECUTIVE OVERFLOW-NO VAC AREAS EXEC
001036,001016: # 31202 EXECUTIVE OVERFLOW-NO CORE SETS EXEC
001037,001017: # 31203 WAITLIST OVERFLOW-TOO MANY TASKS WAITLIST
001038,001018: # 31206 SECOND JOB ATTEMPTS TO GO TO SLEEP VIA PINBALL
001039,001019: # KEYBOARD AND DISPLAY PROGRAM
001040,001020: # 31207 NO VAC AREAS FOR MARKS AOTMARK
001041,001021: # 31210 TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
001042,001022: # 31211 ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
001043,001023: # 31502 TWO PRIO DISPLAYS WAITING DSP INTRFCE
001044,001024: # 32000 DAP STILL IN PROGRESS AT NEXT TIME5 RUPT DAP
001045,001025:
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001047,001027: # CHECKLIST CODES FOR LUMINARY
001048,001028:
001049,001029: # *9 *17 *26 *9 COLUMN
001050,001030:
001051,001031: # R1CODE ACTION TO BE EFFECTED PROGRAM
001052,001032:
001053,001033: # 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
001054,001034: # 00014 PROCEED DO IMU FINE ALIGN ROUTINE P51, P63, P57
001055,001035: # 00014 ENTER DO LANDING SITE DETERMINATION(N89DISP) P57OPTION2
001056,001036: # 00015 PERFORM CELESTIAL BODY ACQUISITION R51, P51
001057,001037: # 00062 SWITCH AGC POWER DOWN P06
001058,001038: # 00201 SWITCH RR MODE TO AUTOMATIC P20, P22, R04
001059,001039: # 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12, P42, P71
001060,001040: # ALSO THR CONT TO AUTO P40, P63, P70
001061,001041: # 00205 PERFORM MANUAL ACQUISITION OF RR R23
001062,001042: # 00500 SWITCH LR ANTENNA TO POSITION 1 P63
001063,001043:
001064,001044: # SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
001065,001045: # PERFORM DENOTES START OR END OF A TASK
001066,001046: # KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
001067,001047:
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001069,001049: # OPTION CODES FOR LUMINARY
001070,001050:
001071,001051: # THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
001072,001052: # CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
001073,001053: # ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
001074,001054:
001075,001055: # *9 *17 *52 *11 *25 COLUMN
001076,001056:
001077,001057: # OPTION
001078,001058: # CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
001079,001059:
001080,001060: # 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
001081,001061: # 4=LAND SITE
001082,001062: # 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
001083,001063: # 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
001084,001064: # 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
001085,001065: # 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
001086,001066: # 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
001087,001067: # 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
001088,001068: # 2=TWO BODIES 3=ONE BODY + G
001089,001069: # 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
001090,001070: # ORBIT TO PASS OVER LM
001091,001071:
End of include-file ASSEMBLY_AND_OPERATION_INFORMATION.agc. Parent file is MAIN.agc