Source Code
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These source-code files are part of a reconstructed copy of Luminary 178, the
final release of the Apollo 14 Lunar Module (LM) Apollo Guidance Computer
(AGC) software.
The reconstruction began with source code of Zerlina 56, Luminary 210, and
Luminary 131, previously transcribed from digitized copies of those programs.
The code was created by combining the three, using Zerlina 56 as a base, since
it was based off of Luminary 183. The differences between the three were
carefully merged using the Luminary memos as a guide, with all changes made
after Luminary 178 being backed out. The reconstruction was verified by matching
memory-bank checksums to those listed in drawing 2021152N. Note that page numbers
in the reconstructed code match those for the baseline log section mentioned in
each file's changelog; the page numbers for a real Luminary 178 listing would
be different.
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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000056,000002: ## Copyright: Public domain.
000057,000003: ## Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
000058,000004: ## Purpose: A section of Luminary revision 178.
000059,000005: ## It is part of the reconstructed source code for the final
000060,000006: ## release of the flight software for the Lunar Module's
000061,000007: ## (LM) Apollo Guidance Computer (AGC) for Apollo 14. The
000062,000008: ## code has been recreated from copies of Zerlina 56, Luminary
000063,000009: ## 210, and Luminary 131, as well as many Luminary memos.
000064,000010: ## It has been adapted such that the resulting bugger words
000065,000011: ## exactly match those specified for Luminary 178 in NASA
000066,000012: ## drawing 2021152N, which gives relatively high confidence
000067,000013: ## that the reconstruction is correct.
000068,000014: ## Reference: pp. 2-27
000069,000015: ## Assembler: yaYUL
000070,000016: ## Contact: Ron Burkey <info@sandroid.org>.
000071,000017: ## Website: www.ibiblio.org/apollo/index.html
000072,000018: ## Mod history: 2019-08-14 MAS Created from Zerlina 56.
000073,000019: ## 2019-09-17 MAS Updated for Luminary 178. Changed program name
000074,000020: ## and subroutine names. Removed CHECK EQUALS log
000075,000021: ## section. Corrected noun 70 and 78. Removed
000076,000022: ## Zerlina-only -BBB- and 00555 alarm definitions.
000077,000023:
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Page 2
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000079,000025: # THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
000080,000026: # THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
000081,000027:
000082,000028:
000083,000029: # GUIDANCE SYSTEM OPERATIONS PLAN
000084,000030: # FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
000085,000031: # USING PROGRAM LUMINARY
000086,000032:
000087,000033:
000088,000034: # THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
000089,000035: # TECHNOLOGY 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS UNDER PROJECT55-238-70, SPONSORED BY THE MANNED
000090,000036: # SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065.
000091,000037:
000092,000038:
000093,000039: # THIS PROGRAM IS REFERRED TO AS LUMINARY 1D
000094,000040:
000095,000041: # TABLE OF LOG CARDS
000096,000042:
000097,000043: # ABSOLUTE ADDRESSES FOR UPDATE PROGRAM
000098,000044: # ASSEMBLY AND OPERATION INFORMATION
000099,000045: # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
000100,000046: # CONTROLLED CONSTANTS
000101,000047: # INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
000102,000048: # FLAGWORD ASSIGNMENTS
000103,000049: # SUBROUTINE CALLS
000104,000050:
000105,000051:
000106,000052: # TABLE OF SUBROUTINE LOG SECTIONS
000107,000053: # LUMERASE
000108,000054: # ERASABLE ASSIGNMENTS
000109,000055: # LEMONAID
000110,000056: # INTERRUPT LEAD INS
000111,000057: # T4RUPT PROGRAM
000112,000058: # RCS FAILURE MONITOR
000113,000059: # DOWNLINK LISTS
000114,000060: # AGS INITIALIZATION
000115,000061: # FRESH START AND RESTART
000116,000062: # RESTART TABLES
000117,000063: # AOTMARK
000118,000064: # EXTENDED VERBS
000119,000065: # PINBALL NOUN TABLES
000120,000066: # LEM GEOMETRY
000121,000067: # IMU COMPENSATION PACKAGE
000122,000068: # R63
000123,000069: # ATTITUDE MANEUVER ROUTINE
000124,000070: # GIMBAL LOCK AVOIDANCE
000125,000071: # KALCMANU STEERING
000126,000072: # SYSTEM TEST STANDARD LEAD INS
000127,000073: # IMU PERFORMANCE TESTS 2
000128,000074: # IMU PERFORMANCE TESTS 4
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Page 3
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000130,000076: # PINBALL GAMES BUTTONS AND LIGHTS
000131,000077: # R60,R62
000132,000078: # S-BAND ANTENNA FOR LM
000133,000079: # LEMP20S
000134,000080: # RADAR LEADIN ROUTINES
000135,000081: # P20-P25
000136,000082: # LEMP30S
000137,000083: # P30,P37
000138,000084: # P32-P35, P72-P75
000139,000085: # KISSING
000140,000086: # GROUND TRACKING DETERMINATION PROGRAM - P21
000141,000087: # P34-P35, P74-P75
000142,000088: # R31
000143,000089: # P76
000144,000090: # R30
000145,000091: # FLY
000146,000092: # BURN, BABY, BURN -- MASTER IGNITION ROUTINE
000147,000093: # P40-P47
000148,000094: # THE LUNAR LANDING
000149,000095: # THROTTLE CONTROL ROUTINES
000150,000096: # LUNAR LANDING GUIDANCE EQUATIONS
000151,000097: # P70-P71
000152,000098: # P12
000153,000099: # ASCENT GUIDANCE
000154,000100: # SERVICER
000155,000101: # LANDING ANALOG DISPLAYS
000156,000102: # FINDCDUW - GUIDAP INTERFACE
000157,000103: # LEMP50S
000158,000104: # P51-P53
000159,000105: # LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
000160,000106: # SKIPPER
000161,000107: # DOWN-TELEMETRY PROGRAM
000162,000108: # INTER-BANK COMMUNICATION
000163,000109: # INTERPRETER
000164,000110: # FIXED-FIXED CONSTANT POOL
000165,000111: # INTERPRETIVE CONSTANTS
000166,000112: # SINGLE PRECISION SUBROUTINES
000167,000113: # EXECUTIVE
000168,000114: # WAITLIST
000169,000115: # LATITUDE LONGITUDE SUBROUTINES
000170,000116: # PLANETARY INERTIAL ORIENTATION
000171,000117: # MEASUREMENT INCORPORATION
000172,000118: # CONIC SUBROUTINES
000173,000119: # INTEGRATION INITIALIZATION
000174,000120: # ORBITAL INTEGRATION
000175,000121: # INFLIGHT ALIGNMENT ROUTINES
000176,000122: # POWERED FLIGHT SUBROUTINES
000177,000123: # TIME OF FREE FALL
000178,000124: # AGC BLOCK TWO SELF-CHECK
000179,000125: # PHASE TABLE MAINTENANCE
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Page 4
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000181,000127: # RESTARTS ROUTINE
000182,000128: # IMU MODE SWITCHING ROUTINES
000183,000129: # KEYRUPT, UPRUPT
000184,000130: # DISPLAY INTERFACE ROUTINES
000185,000131: # SERVICE ROUTINES
000186,000132: # ALARM AND ABORT
000187,000133: # UPDATE PROGRAM
000188,000134: # RTB OP CODES
000189,000135: # LMDAP
000190,000136: # T6-RUPT PROGRAMS
000191,000137: # DAP INTERFACE SUBROUTINES
000192,000138: # DAPIDLER PROGRAM
000193,000139: # P-AXIS RCS AUTOPILOT
000194,000140: # Q,R-AXIS RCS AUTOPILOT
000195,000141: # TJET LAW
000196,000142: # KALMAN FILTER
000197,000143: # TRIM GIMBAL CONTROL SYSTEM
000198,000144: # AOSTASK AND AOSJOB
000199,000145: # SPS BACK-UP RCS CONTROL
000200,000146:
000201,000147:
000202,000148: # SYMBOL TABLE LISTING
000203,000149: # UNREFERENCED SYMBOL LISTING
000204,000150: # ERASABLE & EQUALS CROSS-REFERENCE TABLE
000205,000151: # SUMMARY OF SYMBOL TABLE LISTINGS
000206,000152: # MEMORY TYPE & AVAILABLITY DISPLAY
000207,000153: # COUNT TABLE
000208,000154: # PARAGRAPHS GENERATED FOR THIS ASSEMBLY
000209,000155: # OCTAL LISTING
000210,000156: # OCCUPIED LOCATIONS TABLE
000211,000157: # SUBROS CALLED & PROGRAM STATUS
000212,000158:
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Page 5
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000214,000160: # VERB LIST FOR LUMINARY
000215,000161:
000216,000162: # REGULAR VERBS
000217,000163:
000218,000164: # 00 NOT IN USE
000219,000165: # 01 DISPLAY OCTAL COMP 1 IN R1
000220,000166: # 02 DISPLAY OCTAL COMP 2 IN R1
000221,000167: # 03 DISPLAY OCTAL COMP 3 IN R1
000222,000168: # 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
000223,000169: # 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
000224,000170: # 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000225,000171: # 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
000226,000172: # 08
000227,000173: # 09
000228,000174: # 10
000229,000175: # 11 MONITOR OCTAL COMP 1 IN R1
000230,000176: # 12 MONITOR OCTAL COMP 2 IN R1
000231,000177: # 13 MONITOR OCTAL COMP 3 IN R1
000232,000178: # 14 MONITOR OCTAL COMP 1,2 IN R1,R2
000233,000179: # 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
000234,000180: # 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000235,000181: # 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
000236,000182: # 18
000237,000183: # 19
000238,000184: # 20
000239,000185: # 21 LOAD COMPONENT 1 INTO R1
000240,000186: # 22 LOAD COMPONENT 2 INTO R2
000241,000187: # 23 LOAD COMPONENT 3 INTO R3
000242,000188: # 24 LOAD COMPONENT 1,2 INTO R1,R2
000243,000189: # 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
000244,000190: # 26
000245,000191: # 27 DISPLAY FIXED MEMORY
000246,000192: # 28
000247,000193: # 29
000248,000194: # 30 REQUEST EXECUTIVE
000249,000195: # 31 REQUEST WAITLIST
000250,000196: # 32 RECYCLE PROGRAM
000251,000197: # 33 PROCEED WITHOUT DSKY INPUTS
000252,000198: # 34 TERMINATE FUNCTION
000253,000199: # 35 TEST LIGHTS
000254,000200: # 36 REQUEST FRESH START
000255,000201: # 37 CHANGE PROGRAM (MAJOR MODE)
000256,000202: # 38
000257,000203: # 39
000258,000204:
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Page 6
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000260,000206: # EXTENDED VERBS
000261,000207:
000262,000208: # 40 ZERO CDU-S
000263,000209: # 41 COARSE ALIGN CDU-S
000264,000210: # 42 FINE ALIGN IMU
000265,000211: # 43 LOAD IMU ATT ERROR METERS
000266,000212: # 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
000267,000213: # 45
000268,000214: # 46
000269,000215: # 47 INITIALIZE AGS (R47)
000270,000216: # 48 REQUEST DAP DATA LOAD ROUTINE (R03)
000271,000217: # 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
000272,000218: # 50 PLEASE PERFORM
000273,000219: # 51
000274,000220: # 52 MARK X-RETICLE
000275,000221: # 53 MARK Y-RETICLE
000276,000222: # 54 MARK X OR Y-RETICLE
000277,000223: # 55 INCREMENT AGC TIME (DECIMAL)
000278,000224: # 56 TERMINATE TRACKING (P20 + P25)
000279,000225: # 57 PERMIT LANDING RADAR UPDATES
000280,000226: # 58 INHIBIT LANDING RADAR UPDATES
000281,000227: # 59 COMMAND LR TO POSITION 2.
000282,000228: # 60 DISPLAY VEHICLE ATTITUDE RATES ON FDAI ERROR NEEDLES.
000283,000229: # 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
000284,000230: # 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
000285,000231: # 63 SAMPLE RADAR ONCE PER SECOND (R04).
000286,000232: # 64 REQUEST S-BAND ANTENNA ROUTINE (R05)
000287,000233: # 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
000288,000234: # 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
000289,000235: # 67 DISPLAY W MATRIX
000290,000236: # 68 DISABLE TERRAIN MODEL
000291,000237: # 69 CAUSE RESTART
000292,000238: # 70 UPDATE LIFTOFF TIME
000293,000239: # 71 UNIVERSAL UPDATE-BLOCK ADR
000294,000240: # 72 UNIVERSAL UPDATE-SINGLE ADR
000295,000241: # 73 UPDATE AGC TIME (OCTAL)
000296,000242: # 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
000297,000243: # 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
000298,000244: # 76 MINIMUM IMPULSE COMMAND MODE
000299,000245: # 77 RATE COMMAND AND ATTITUDE HOLD MODE
000300,000246: # 78 LR SPURIOUS RETURN TEST START (R77)
000301,000247: # 79 LR SPURIOUS RETURN TEST STOP
000302,000248: # 80 UPDATE LEM STATE VECTOR
000303,000249: # 81 UPDATE CSM STATE VECTOR
000304,000250: # 82 REQUEST ORBIT PARAM DISPLAY (R30)
000305,000251: # 83 REQUEST REND PARAM DISPLAY (R31)
000306,000252: # 84
000307,000253: # 85 DISPLAY RR LOS AZ AND ELEV
000308,000254: # 86
000309,000255: # 87
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Page 7
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000311,000257: # 88
000312,000258: # 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
000313,000259: # 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
000314,000260: # 91 DISPLAY BANK SUM
000315,000261: # 92 OPERATE IMU PERFORMANCE TEST (P07)
000316,000262: # 93 ENABLE W MATRIX INITIALIZATION
000317,000263: # 94
000318,000264: # 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
000319,000265: # 96 INTERRUPT INTEGRATION AND GO TO POO
000320,000266: # 97 PERFORM ENGINE FAIL PROCEDURE
000321,000267: # 98
000322,000268: # 99 PLEASE ENABLE ENGINE
000323,000269:
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Page 8
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000325,000271: # IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
000326,000272: # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
000327,000273: # SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
000328,000274: # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23
000329,000275: # MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
000330,000276: # ABOVE SCALE TYPES.
000331,000277: # THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
000332,000278: # EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
000333,000279:
000334,000280: # NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000335,000281:
000336,000282: # 00 NOT IN USE
000337,000283: # 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH
000338,000284: # 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH
000339,000285: # 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP XXX.XX DEG FOR EACH
000340,000286: # 04 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000341,000287: # 05 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000342,000288: # 06 OPTION CODE 3COMP OCTAL ONLY FOR EACH
000343,000289: # LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
000344,000290: # 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
000345,000291: # ONES FOR BITS TO BE MODIFIED
000346,000292: # 1 TO SET OR 0 TO RESET SELECTED BITS
000347,000293: # 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
000348,000294: # 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
000349,000295: # 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
000350,000296: # 11 TIG OF CSI 3COMP 00XXX. HRS DEC ONLY
000351,000297: # 000XX. MIN MUST LOAD 3 COMPS
000352,000298: # 0XX.XX SEC
000353,000299: # 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
000354,000300: # (USED BY EXTENDED VERBS ONLY)
000355,000301: # 13 TIG OF CDH 3COMP 00XXX. HRS DEC ONLY
000356,000302: # 000XX. MIN MUST LOAD 3 COMPS
000357,000303: # 0XX.XX SEC
000358,000304: # 14 CHECKLIST 3COMP XXXXX. FOR EACH
000359,000305: # (USED BY EXTENDED VERBS ONLY)
000360,000306: # (NOUN 25 IS PASTED AFTER DISPLAY)
000361,000307: # 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
000362,000308: # 16 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000363,000309: # (USED BY EXTENDED VERBS ONLY) 000XX. MIN MUST LOAD 3 COMPS
000364,000310: # 0XX.XX SEC
000365,000311: # 17 SPARE
000366,000312: # 18 AUTO MANEUVER BALL ANGLES 3COMP XXX.XX DEG FOR EACH
000367,000313: # 19 SPARE
000368,000314: # 20 ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000369,000315: # 21 PIPAS 3COMP XXXXX. PULSES FOR EACH
000370,000316: # 22 NEW ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000371,000317: # 23 SPARE
000372,000318: # 24 DELTA TIME FOR AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000373,000319: # 000XX. MIN MUST LOAD 3 COMPS
000374,000320: # 0XX.XX SEC
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000376,000322: # 25 CHECKLIST 3COMP XXXXX. FOR EACH
000377,000323: # (USED WITH PLEASE PERFORM ONLY)
000378,000324: # 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
000379,000325: # 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX.
000380,000326: # 28 SPARE
000381,000327: # 29 SPARE
000382,000328: # 30 SPARE
000383,000329: # 31 SPARE
000384,000330: # 32 TIME FROM PERIGEE 3COMP 00XXX. HRS DEC ONLY
000385,000331: # 000XX. MIN MUST LOAD 3 COMPS
000386,000332: # 0XX.XX SEC
000387,000333: # 33 TIME OF IGNITION 3COMP 00XXX. HRS DEC ONLY
000388,000334: # 000XX. MIN MUST LOAD 3 COMPS
000389,000335: # 0XX.XX SEC
000390,000336: # 34 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000391,000337: # 000XX. MIN MUST LOAD 3 COMPS
000392,000338: # 0XX.XX SEC
000393,000339: # 35 TIME FROM EVENT 3COMP 00XXX. HRS DEC ONLY
000394,000340: # 000XX. MIN MUST LOAD 3 COMPS
000395,000341: # 0XX.XX SEC
000396,000342: # 36 TIME OF AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000397,000343: # 000XX. MIN MUST LOAD 3 COMPS
000398,000344: # 0XX.XX SEC
000399,000345: # 37 TIG OF TPI 3COMP 00XXX. HRS DEC ONLY
000400,000346: # 000XX. MIN MUST LOAD 3 COMPS
000401,000347: # 0XX.XX SEC
000402,000348: # 38 TIME OF STATE BEING INTEGRATED 3COMP 00XXX. HRS DEC ONLY
000403,000349: # 000XX. MIN MUST LOAD 3 COMPS
000404,000350: # 0XX.XX SEC
000405,000351: # 39 SPARE
000406,000352:
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Page 10
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000408,000354: # MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000409,000355:
000410,000356: # 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000411,000357: # VG, XXXX.X FT/SEC
000412,000358: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000413,000359: # 41 TARGET AZIMUTH, 2COMP XXX.XX DEG (FOR SYSTEM TEST)
000414,000360: # ELEVATION XX.XXX DEG
000415,000361: # 42 APOGEE, 3COMP XXXX.X NAUT MI DEC ONLY
000416,000362: # PERIGEE, XXXX.X NAUT MI
000417,000363: # DELTA V (REQUIRED) XXXX.X FT/SEC
000418,000364: # 43 LATITUDE, 3COMP XXX.XX DEG DEC ONLY
000419,000365: # LONGITUDE, XXX.XX DEG
000420,000366: # ALTITUDE XXXX.X NAUT MI
000421,000367: # 44 APOGEE, 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000422,000368: # PERIGEE, XXXX.X NAUT MI
000423,000369: # TFF XXBXX MIN/SEC
000424,000370: # 45 MARKS, 3COMP XXXXX. NO LOAD, DEC ONLY
000425,000371: # TFI OF NEXT BURN XXBXX MIN/SEC
000426,000372: # MGA XXX.XX DEG
000427,000373: # 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
000428,000374: # 47 LEM WEIGHT, 2COMP XXXXX. LBS DEC ONLY
000429,000375: # CSM WEIGHT XXXXX. LBS
000430,000376: # 48 GIMBAL PITCH TRIM, 2COMP XXX.XX DEG DEC ONLY
000431,000377: # GIMBAL ROLL TRIM XXX.XX DEG
000432,000378: # 49 DELTA R, 3COMP XXXX.X NAUT MI DEC ONLY
000433,000379: # DELTA V, XXXX.X FT/SEC
000434,000380: # RADAR DATA SOURCE CODE XXXXX.
000435,000381: # 50 SPARE
000436,000382: # 51 S-BAND ANTENNA ANGLES PITCH 2COMP XXX.XX DEG DEC ONLY
000437,000383: # YAW XXX.XX DEG
000438,000384: # 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG
000439,000385: # 53 SPARE
000440,000386: # 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
000441,000387: # RANGE RATE, XXXX.X FT/SEC
000442,000388: # THETA XXX.XX DEG
000443,000389: # 55 NO. OF APSIDAL CROSSINGS 3COMP XXXXX. DEC ONLY
000444,000390: # ELEVATION ANGLE XXX.XX DEG
000445,000391: # CENTRAL ANGLE OF PASSIVE VEHICLE XXX.XX DEG
000446,000392: # 56 RR LOS AZIMUTH 2COMP XXX.XX DEG
000447,000393: # ELEVATION XXX.XX DEG
000448,000394: # 57 SPARE
000449,000395: # 58 PERIGEE ALT (POST TPI) 3COMP XXXX.X NAUT MI DEC ONLY
000450,000396: # DELTA V TPI XXXX.X FT/SEC
000451,000397: # DELTA V TPF XXXX.X FT/SEC
000452,000398: # 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY
000453,000399: # 60 FORWARD VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000454,000400: # ALTITUDE RATE XXXX.X FT/SEC
000455,000401: # COMPUTED ALTITUDE XXXXX. FEET
000456,000402: # 61 TIME TO GO IN BRAKING PHASE 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000457,000403: # TIME FROM IGNITION XXBXX MIN/SEC
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000459,000405: # CROSS RANGE DISTANCE XXXX.X NAUT MI
000460,000406: # 62 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC NO LOAD, DEC ONLY
000461,000407: # TIME FROM IGNITION XXBXX MIN/SEC
000462,000408: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000463,000409: # 63 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000464,000410: # ALTITUDE RATE XXXX.X FT/SEC
000465,000411: # COMPUTED ALTITUDE XXXXX. FEET
000466,000412: # 64 TIME LEFT FOR REDESIGNATION- LPD ANGLE 3COMP XXBXX NO LOAD, DEC ONLY
000467,000413: # ALTITUDE RATE XXXX.X FT/SEC
000468,000414: # COMPUTED ALTITUDE XXXXX. FEET
000469,000415: # 65 SAMPLED AGC TIME 3COMP 00XXX. HRS DEC ONLY
000470,000416: # (FETCHED IN INTERRUPT) 000XX. MIN MUST LOAD 3 COMPS
000471,000417: # 0XX.XX SEC
000472,000418: # 66 LR RANGE 2COMP XXXXX. FEET NO LOAD, DEC ONLY
000473,000419: # POSITION +0000X
000474,000420: # 67 LRVX 3COMP XXXXX. FT/SEC
000475,000421: # LRVY XXXXX. FT/SEC
000476,000422: # LRVZ XXXXX. FT/SEC
000477,000423: # 68 SLANT RANGE TO LANDING SITE 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000478,000424: # TIME TO GO IN BRAKING PHASE XXBXX MIN/SEC
000479,000425: # LR ALTITUDE - COMPUTED ALTITUDE XXXXX. FEET
000480,000426: # 69 LANDING SITE CORRECTION, Z-COMPONENT 3COMP XXXXX. FEET DEC ONLY
000481,000427: # LANDING SITE CORRECTION, Y-COMPONENT XXXXX. FEET
000482,000428: # LANDING SITE CORRECTION, X-COMPONENT XXXXX. FEET
000483,000429: # 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000484,000430: # 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000485,000431: # 72 RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000486,000432: # SHAFT ANGLE XXX.XX DEG
000487,000433: # 73 NEW RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000488,000434: # SHAFT ANGLE XXX.XX DEG
000489,000435: # 74 TIME FROM IGNITION 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000490,000436: # YAW AFTER VEHICLE RISE XXX.XX DEG
000491,000437: # PITCH AFTER VEHICLE RISE XXX.XX DEG
000492,000438: # 75 DELTA ALTITUDE CDH 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000493,000439: # DELTA TIME (CDH-CSI OR TPI-CDH) XXBXX MIN/SEC
000494,000440: # DELTA TIME (TPI-CDH OR TPI-NOMTPI) XXBXX MIN/SEC
000495,000441: # 76 DESIRED HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000496,000442: # DESIRED RADIAL VELOCITY XXXX.X FT/SEC
000497,000443: # CROSS-RANGE DISTANCE XXXX.X NAUT MI
000498,000444: # 77 TIME TO ENGINE CUTOFF 2COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000499,000445: # VELOCITY NORMAL TO CSM PLANE XXXX.X FT/SEC
000500,000446: # 78 RR RANGE 3COMP XXX.XX NAUT MI NO LOAD, DEC ONLY
000501,000447: # RANGE RATE XXXXX. FT/SEC
000502,000448: # TIME FROM IGNITION XXBXX MIN/SEC
000503,000449: # 79 CURSOR ANGLE 3COMP XXX.XX DEG DEC ONLY
000504,000450: # SPIRAL ANGLE XXX.XX DEG
000505,000451: # POSITION CODE XXXXX.
000506,000452: # 80 DATA INDICATOR, 2COMP XXXXX.
000507,000453: # OMEGA XXX.XX DEG
000508,000454: # 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
|
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Page 12
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000510,000456: # 82 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000511,000457: # 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000512,000458: # 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000513,000459: # 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000514,000460: # 86 VG (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000515,000461: # 87 BACKUP OPTICS LOS AZIMUTH 2COMP XXX.XX DEG
000516,000462: # ELEVATION XXX.XX DEG
000517,000463: # 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY
000518,000464: # 89 LANDMARK LATITUDE 3COMP XX.XXX DEG DEC ONLY
000519,000465: # LONGITUDE/2 XX.XXX DEC
000520,000466: # ALTITUDE XXX.XX NAUT MI
000521,000467: # 90 Y 3COMP XXX.XX NM DEC ONLY
000522,000468: # Y DOT XXXX.X FPS
000523,000469: # PSI XXX.XX DEG
000524,000470: # 91 ALTITUDE 3COMP XXXXXB. NAUT MI
000525,000471: # VELOCITY XXXXX. FT/SEC
000526,000472: # FLIGHT PATH ANGLE XXX.XX DEG
000527,000473: # 92 PCT FTP(10,5KLB) AT PRESENT THRUST 3COMP XXXXX.
000528,000474: # ALTITUDE RATE XXXX.X FT/SEC
000529,000475: # COMPUTED ALTITUDE XXXXX.FEET
000530,000476: # 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
000531,000477: # 94 SPARE
000532,000478: # 95 SPARE
000533,000479: # 96 SPARE
000534,000480: # 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH
000535,000481: # 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX.
000536,000482: # .XXXXX
000537,000483: # XXXXX.
000538,000484: # 99 RMS IN POSITION 3COMP XXXXX.FT DEC ONLY
000539,000485: # RMS IN VELOCITY XXXX.X FT/SEC
000540,000486: # RMS IN BIAS XX.XXX RADIANS
000541,000487:
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Page 13
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000543,000489: # REGISTERS AND SCALING FOR NORMAL NOUNS
000544,000490:
000545,000491: # NOUN REGISTER SCALE TYPE
000546,000492:
000547,000493: # 00 NOT IN USE
000548,000494: # 01 SPECIFY ADDRESS B
000549,000495: # 02 SPECIFY ADDRESS C
000550,000496: # 03 SPECIFY ADDRESS D
000551,000497: # 04 DSPTEM1 H
000552,000498: # 05 DSPTEM1 H
000553,000499: # 06 OPTION1 A
000554,000500: # 07 XREG A
000555,000501: # 08 ALMCADR A
000556,000502: # 09 FAILREG A
000557,000503: # 10 SPECIFY CHANNEL A
000558,000504: # 11 TCSI K
000559,000505: # 12 OPTIONX A
000560,000506: # 13 TCDH K
000561,000507: # 14 DSPTEMX C
000562,000508: # 15 INCREMENT ADDRESS A
000563,000509: # 16 DSPTEMX K
000564,000510: # 17 SPARE
000565,000511: # 18 FDAIX D
000566,000512: # 19 SPARE
000567,000513: # 20 CDUX D
000568,000514: # 21 PIPAX C
000569,000515: # 22 THETAD D
000570,000516: # 23 SPARE
000571,000517: # 24 DSPTEM2 +1 K
000572,000518: # 25 DSPTEM1 C
000573,000519: # 26 DSPTEM1 A
000574,000520: # 27 SMODE C
000575,000521: # 28 SPARE
000576,000522: # 29 SPARE
000577,000523: # 30 SPARE
000578,000524: # 31 SPARE
000579,000525: # 32 -TPER K
000580,000526: # 33 TIG K
000581,000527: # 34 DSPTEM1 K
000582,000528: # 35 TTOGO K
000583,000529: # 36 TIME2 K
000584,000530: # 37 TTPI K
000585,000531: # 38 TET K
000586,000532: # 39 SPARE
000587,000533:
|
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Page 14
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000589,000535: # REGISTERS AND SCALING FOR MIXED NOUNS
000590,000536:
000591,000537: # NOUN COMP REGISTER SCALE TYPE
000592,000538:
000593,000539: # 40 1 TTOGO L
000594,000540: # 2 VGDISP S
000595,000541: # 3 DVTOTAL S
000596,000542: # 41 1 DSPTEM1 D
000597,000543: # 2 DSPTEM1 +1 E
000598,000544: # 42 1 HAPO Q
000599,000545: # 2 HPER Q
000600,000546: # 3 VGDISP S
000601,000547: # 43 1 LAT H
000602,000548: # 2 LONG H
000603,000549: # 3 ALT Q
000604,000550: # 44 1 HAPOX Q
000605,000551: # 2 HPERX Q
000606,000552: # 3 TFF L
000607,000553: # 45 1 TRKMKCNT C
000608,000554: # 2 TTOGO L
000609,000555: # 3 +MGA H
000610,000556: # 46 1 DAPDATR1 A
000611,000557: # 47 1 LEMMASS KK
000612,000558: # 2 CSMMASS KK
000613,000559: # 48 1 PITTIME NN
000614,000560: # 2 ROLLTIME NN
000615,000561: # 49 1 R22DISP Q
000616,000562: # 2 R22DISP +2 S
000617,000563: # 3 WHCHREAD C
000618,000564: # 50 SPARE
000619,000565: # 51 1 ALPHASB H
000620,000566: # 2 BETASB H
000621,000567: # 52 1 ACTCENT H
000622,000568: # 53 SPARE
000623,000569: # 54 1 RANGE JJ
000624,000570: # 2 RRATE S
000625,000571: # 3 RTHETA H
000626,000572: # 55 1 NN C
000627,000573: # 2 ELEV H
000628,000574: # 3 CENTANG H
000629,000575: # 56 1 RR-AZ H
000630,000576: # 2 RR-ELEV H
000631,000577: # 57 SPARE
000632,000578: # 58 1 POSTTPI Q
000633,000579: # 2 DELVTPI S
000634,000580: # 3 DELVTPF S
000635,000581: # 59 1 DVLOS S
000636,000582: # 2 DVLOS +2 S
000637,000583: # 3 DVLOS +4 S
000638,000584: # 60 1 FORVEL ZZ
|
|
Page 15
|
000640,000586: # 2 HDOTDISP S
000641,000587: # 3 HCALC1 RR
000642,000588: # 61 1 TTFDISP L
000643,000589: # 2 TTOGO L
000644,000590: # 3 OUTOFPLN QQ
000645,000591: # 62 1 ABVEL S
000646,000592: # 2 TTOGO L
000647,000593: # 3 DVTOTAL S
000648,000594: # 63 1 ABVEL S
000649,000595: # 2 HDOTDISP S
000650,000596: # 3 HCALC1 RR
000651,000597: # 64 1 FUNNYDSP PP
000652,000598: # 2 HDOTDISP S
000653,000599: # 3 HCALC RR
000654,000600: # 65 1 SAMPTIME K
000655,000601: # 2 SAMPTIME K
000656,000602: # 3 SAMPTIME K
000657,000603: # 66 1 RSTACK +6 W
000658,000604: # 2 CHANNEL 33 TT
000659,000605: # 67 1 RSTACK X
000660,000606: # 2 RSTACK +2 Y
000661,000607: # 3 RSTACK +4 Z
000662,000608: # 68 1 RANGEDSP QQ
000663,000609: # 2 TTFDISP L
000664,000610: # 3 DELTAH RR
000665,000611: # 69 1 DLANDZ RR
000666,000612: # 2 DLANDY RR
000667,000613: # 3 DLANDX RR
000668,000614: # 70 1 AOTCODE A
000669,000615: # 2 AOTCODE +1 A
000670,000616: # 3 AOTCODE +2 A
000671,000617: # 71 1 AOTCODE A
000672,000618: # 2 AOTCODE +1 A
000673,000619: # 3 AOTCODE +2 A
000674,000620: # 72 1 CDUT WW
000675,000621: # 2 CDUS D
000676,000622: # 73 1 TANG WW
000677,000623: # 2 TANG +1 D
000678,000624: # 74 1 TTOGO L
000679,000625: # 2 YAW H
000680,000626: # 3 PITCH H
000681,000627: # 75 1 DIFFALT Q
000682,000628: # 2 T1TOT2 L
000683,000629: # 3 T2TOT3 L
000684,000630: # 76 1 ZDOTD S
000685,000631: # 2 RDOTD S
000686,000632: # 3 XRANGE Q
000687,000633: # 77 1 TTOGO L
000688,000634: # 2 YDOT S
000689,000635: # 78 1 DNRRANGE U
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Page 16
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000691,000637: # 2 DNRRDOT V
000692,000638: # 3 TTOTIG L
000693,000639: # 79 1 CURSOR D
000694,000640: # 2 SPIRAL D
000695,000641: # 3 POSCODE C
000696,000642: # 80 1 DATAGOOD C
000697,000643: # 2 OMEGAD H
000698,000644: # 81 1 DELVLVC S
000699,000645: # 2 DELVLVC +2 S
000700,000646: # 3 DELVLVC +4 S
000701,000647: # 82 1 DELVLVC S
000702,000648: # 2 DELVLVC +2 S
000703,000649: # 3 DELVLVC +4 S
000704,000650: # 83 1 DELVIMU S
000705,000651: # 2 DELVIMU +2 S
000706,000652: # 3 DELVIMU +4 S
000707,000653: # 84 1 DELVOV S
000708,000654: # 2 DELVOV +2 S
000709,000655: # 3 DELVOV +4 S
000710,000656: # 85 1 VGBODY S
000711,000657: # 2 VGBODY +2 S
000712,000658: # 3 VGBODY +4 S
000713,000659: # 86 1 DELVLVC S
000714,000660: # 2 DELVLVC +2 S
000715,000661: # 3 DELVLVC +4 S
000716,000662: # 87 1 AZ D
000717,000663: # 2 EL D
000718,000664: # 88 1 STARAD B
000719,000665: # 2 STARAD +2 B
000720,000666: # 3 STARAD +4 B
000721,000667: # 89 1 LANDLAT G
000722,000668: # 2 LANDLONG G
000723,000669: # 3 LANDALT JJ
000724,000670: # 90 1 RANGE JJ
000725,000671: # 2 RRATE S
000726,000672: # 3 RTHETA H
000727,000673: # 91 1 P21ALT Q (MEMORY/100 TO DIPLAY TENS N.M.)
000728,000674: # 2 P21VEL P
000729,000675: # 3 P21GAM H
000730,000676: # 92 1 THRDISP C
000731,000677: # 2 HDOTDISP S
000732,000678: # 3 HCALC1 RR
000733,000679: # 93 1 OGC G
000734,000680: # 2 OGC +2 G
000735,000681: # 3 OGC +4 G
000736,000682: # 94 SPARE
000737,000683: # 95 SPARE
000738,000684: # 96 SPARE
000739,000685: # 97 1 DSPTEM1 C
000740,000686: # 2 DSPTEM1 +1 C
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|
Page 17
|
000742,000688: # 3 DSPTEM1 +2 C
000743,000689: # 98 1 DSPTEM2 C
000744,000690: # 2 DSPTEM2 +1 B
000745,000691: # 3 DSPTEM2 +2 C
000746,000692: # 99 1 WWPOS XX
000747,000693: # 2 WWVEL YY
000748,000694: # 3 WWBIAS AAA
000749,000695:
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|
Page 18
|
000751,000697: # NOUN SCALES AND FORMATS
000752,000698:
000753,000699: # -SCALE TYPE- PRECISION
000754,000700: # UNITS DECIMAL FORMAT -- AGC FORMAT
000755,000701: # ------------ -------------- -- ----------
000756,000702:
000757,000703: # -A-
000758,000704: # OCTAL XXXXX SP OCTAL
000759,000705:
000760,000706: # -B- -14
000761,000707: # FRACTIONAL .XXXXX SP BIT 1 = 2 UNITS
000762,000708: # (MAX .99996)
000763,000709:
000764,000710: # -C-
000765,000711: # WHOLE XXXXX. SP BIT 1 = 1 UNIT
000766,000712: # (MAX 16383.)
000767,000713:
000768,000714: # -D- 15
000769,000715: # CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360/2 DEGREES
000770,000716: # (MAX 359.99) (USES 15 BITS FOR MAGNI-
000771,000717: # TUDE AND 2-S COMP.)
000772,000718:
000773,000719: # -E- 14
000774,000720: # ELEVATION DEGREES XX.XXX DEGREES SP BIT 1 = 90/2 DEGREES
000775,000721: # (MAX 89.999)
000776,000722:
000777,000723: # -F- 14
000778,000724: # DEGREES (180) XXX.XX DEGREES SP BIT 1 = 180/2 DEGREES
000779,000725: # (MAX 179.99)
000780,000726:
000781,000727: # -G-
000782,000728: # DP DEGREES(90) XX.XXX DEGREES DP BIT 1 OF LOW REGISTER =
000783,000729: # 28
000784,000730: # 360/2 DEGREES
000785,000731:
000786,000732: # -H-
000787,000733: # DP DEGREES (360) XXX.XX DEGREES DP BIT 1 OF LOW REGISTER =
000788,000734: # 28
000789,000735: # (MAX 359.99) 360/2 DEGREES
000790,000736:
|
|
Page 19
|
000792,000738: # -K-
000793,000739: # TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER =
000794,000740: # 000XX. MIN -2
000795,000741: # 0XX.XX SEC 10 SEC
000796,000742: # (DECIMAL ONLY.
000797,000743: # MAX MIN COMP=59
000798,000744: # MAX SEC COMP=59.99
000799,000745: # MAX CAPACITY=745 HRS
000800,000746: # 39 MINS
000801,000747: # 14.55 SECS.
000802,000748: # WHEN LOADING, ALL 3
000803,000749: # COMPONENTS MUST BE
000804,000750: # SUPPLIED.)
000805,000751:
000806,000752: # -L-
000807,000753: # TIME (MIN/SEC) XXBXX MIN/SEC DP BIT 1 OF LOW REGISTER =
000808,000754: # (B IS A BLANK -2
000809,000755: # POSITION, DECIMAL 10 SEC
000810,000756: # ONLY, DISPLAY OR
000811,000757: # MONITOR ONLY. CANNOT
000812,000758: # BE LOADED.
000813,000759: # MAX MIN COMP=59
000814,000760: # MAX SEC COMP=59
000815,000761: # VALUES GREATER THAN
000816,000762: # 59 MIN 59 SEC
000817,000763: # ARE DISPLAYED AS
000818,000764: # 59 MIN 59 SEC.)
000819,000765:
000820,000766: # -M- -2
000821,000767: # TIME (SEC) XXX.XX SEC SP BIT 1 = 10 SEC
000822,000768: # (MAX 163.83)
000823,000769:
000824,000770: # -N-
000825,000771: # TIME(SEC) DP XXX.XX SEC DP BIT 1 OF LOW REGISTER =
000826,000772: # -2
000827,000773: # 10 SEC
000828,000774:
000829,000775: # -P-
000830,000776: # VELOCITY 2 XXXXX. FEET/SEC DP BIT 1 OF HIGH REGISTER =
000831,000777: # (MAX 41994.) -7
000832,000778: # 2 METERS/CENTI-SEC
000833,000779:
000834,000780: # -Q-
000835,000781: # POSITION 4 XXXX.X NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
000836,000782: # 2 METERS
000837,000783:
000838,000784: # -S-
000839,000785: # VELOCITY 3 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
000840,000786: # -7
000841,000787: # 2 METERS/CENTI-SEC
000842,000788:
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|
Page 20
|
000844,000790: # -T- -2
000845,000791: # G XXX.XX G SP BIT 1 = 10 G
000846,000792: # (MAX 163.83)
000847,000793:
000848,000794: # -U-
000849,000795: # RENDEZVOUS XXX.XX NAUT MI SP USES 15 BITS FOR UNSIGNED
000850,000796: # RADAR RANGE (DECIMAL ONLY. MAGNITUDE.
000851,000797: # DISPLAY OR MONITOR BIT 1 = 9.38 FEET
000852,000798: # ONLY. CANNOT BE
000853,000799: # LOADED.)
000854,000800:
000855,000801: # -V-
000856,000802: # RENDEZVOUS XXXXX. FEET/SEC SP USES 15 BITS FOR UNSIGNED
000857,000803: # RADAR RANGE RATE (DECIMAL ONLY. MAGNITUDE.
000858,000804: # DISPLAY OR MONITOR BIT 1 = -.6278 FEET/SEC
000859,000805: # ONLY. CANNOT BE
000860,000806: # LOADED.
000861,000807: # BIAS OF 17000 COUNTS
000862,000808: # SUBTRACTED BEFORE
000863,000809: # DISPLAY.)
000864,000810:
000865,000811: # -W-
000866,000812: # LANDING RADAR XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000867,000813: # ALTITUDE WORD = 1.079 FEET
000868,000814:
000869,000815: # -X-
000870,000816: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000871,000817: # VELX WORD = -.6440 FEET/SEC
000872,000818:
000873,000819: # -Y-
000874,000820: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000875,000821: # VELY WORD = 1.212 FEET/SEC
000876,000822:
000877,000823: # -Z-
000878,000824: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000879,000825: # VELZ WORD = .8668 FEET/SEC
000880,000826:
000881,000827: # -AA-
000882,000828: # INITIAL/FINAL XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000883,000829: # ALTITUDE WORD = 2.345 FEET
000884,000830:
000885,000831: # -BB-
000886,000832: # ALTITUDE RATE XXXXX. FEET/SEC SP LOW ORDER BIT = .5
000887,000833: # (MAX 08191.) FEET/SEC
000888,000834:
000889,000835: # -CC-
000890,000836: # FORWARD/LATERAL XXXX.X FEET/SEC SP LOW ORDER BIT = .5571
000891,000837: # VELOCITY (MAX 09126.) FEET/SEC
000892,000838:
000893,000839: # -DD-
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|
Page 21
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000895,000841: # ROTATIONAL HAND XXXXX. DEG/SEC SP FRACTIONAL PART OF PI RAD
000896,000842: # CONTROLLER ANGULAR (MAX 00044.) 4 SEC
000897,000843: # RATES
000898,000844:
000899,000845: # -EE-
000900,000846: # OPTICAL TRACKER XXX.XX DEG. DP LOW ORDER BIT OF LOW ORDER
000901,000847: # AZIMUTH ANGLE 15
000902,000848: # WORD = 360/2 DEGREES
000903,000849:
000904,000850: # -JJ-
000905,000851: # POSITION5 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
000906,000852: # 2 METERS
000907,000853:
000908,000854: # -KK- 16
000909,000855: # WEIGHT2 XXXXX. LBS SP FRACTIONAL PART OF 2 KG
000910,000856:
000911,000857: # -NN-
000912,000858: # TRIM DEGREES 2 XXX.XX DEG SP BIT 1=.01SEC(TIME)
000913,000859: # (MAX 032.76)
000914,000860:
000915,000861: # -PP-
000916,000862: # 2 INTEGERS +XXBYY DP BIT 1 OF HIGH REGISTER =
000917,000863: # (B IS A BLANK 1 UNIT OF XX
000918,000864: # POSITION. DECIMAL BIT 1 OF LOW REGISTER =
000919,000865: # ONLY, DISPLAY OR 1 UNIT OF YY
000920,000866: # MONITOR ONLY. CANNOT (EACH REGISTER MUST
000921,000867: # BE LOADED.) CONTAIN A POSITIVE INTEGER
000922,000868: # (MAX 99B99) LESS THAN 100)
000923,000869:
000924,000870: # -QQ-
000925,000871: # POSITION7 XXXX.X NAUT MI DP BIT 1 OF LOW REGISTER =
000926,000872: # (MAX 9058.9) -4
000927,000873: # 2 METERS
000928,000874:
000929,000875: # -RR-
000930,000876: # COMPUTED ALTITUDE XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000931,000877: # -4
000932,000878: # 2 METERS
000933,000879:
000934,000880: # -SS-
000935,000881: # DP DEGREES XXXX.X DEGREES DP BIT 1 OF HIGH REGISTER =
000936,000882: # 1 DEGREE
000937,000883:
000938,000884: # -TT-
000939,000885: # LANDING RADAR +0000X CHANNEL 33,BIT 6=NOT POSIT. 1
000940,000886: # POSITION (DECIMAL ONLY. CHANNEL 33,BIT 7=NOT POSIT. 2
000941,000887: # DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
000942,000888: # ONLY. CANNOT BE X = 2 FOR LR POSITION 2
000943,000889: # LOADED.)
000944,000890:
000945,000891: # -WW- 15
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|
Page 22
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000947,000893: # 360-CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360 - (360/2 )
000948,000894: # (MAX 359.99) DEGREES
000949,000895: # (USES 15 BITS FOR MAGNI-
000950,000896: # TUDE AND 2-S COMP.)
000951,000897:
000952,000898: # -XX-
000953,000899: # POSITION 9 XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000954,000900: # -9
000955,000901: # 2 METERS
000956,000902:
000957,000903: # -YY-
000958,000904: # VELOCITY 4 XXXX.X FEET/SEC DP FRACTIONAL PART OF
000959,000905: # (MAX 328.0) METERS/CENTI-SEC
000960,000906:
000961,000907: # -ZZ-
000962,000908: # VELOCITY5 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
000963,000909: # -9
000964,000910: # 2 METERS/CENTI-SEC
000965,000911:
000966,000912: # -AAA-
000967,000913: # RADIANS XX.XXX RADIANS DP BIT 1 OF HIGH REGISTER =
000968,000914: # (MAX 31.999) -9
000969,000915: # 2 RADIANS
000970,000916:
000971,000917: # THAT-S ALL ON THE NOUNS.
000972,000918:
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000974,000920: # ALARM CODES FOR LUMINARY
000975,000921:
000976,000922: # *9 *18 *60 COLUMN
000977,000923:
000978,000924: # CODE * TYPE SET BY
000979,000925:
000980,000926: # 00107 MORE THAN 5 MARK PAIRS AOTMARK
000981,000927: # 00111 MARK MISSING AOTMARK
000982,000928: # 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
000983,000929: # 00113 NO INBITS AOTMARK
000984,000930: # 00114 MARK MADE BUT NOT DESIRED AOTMARK
000985,000931: # 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
000986,000932: # 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING
000987,000933: # 00206 + GIMBAL LOCK.
000988,000934: # 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
000989,000935: # 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51, P57
000990,000936: # 00211 COARSE ALIGN ERROR IMU MODE SWITCH
000991,000937: # 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH,T4RPT
000992,000938: # 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
000993,000939: # 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
000994,000940: # 00217 BAD RETURN FROM IMUSTALL P51,P52,P57
000995,000941: # 00220 IMU NOT ALIGNED - NO REFSMMAT R02,R47
000996,000942: # 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
000997,000943: # FINDCDUW
000998,000944: # 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
000999,000945: # 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
001000,000946: # 00405 TWO STARS NOT AVAILABLE P52
001001,000947: # 00421 W-MATRIX OVERFLOW INTEGRV
001002,000948: # 00501 P RADAR ANTENNA OUT OF LIMITS R23
001003,000949: # 00502 BAD RADAR GIMBAL ANGLE INPUT V41N72
001004,000950: # 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V41N72
001005,000951: # 00510 RADAR AUTO DESCRETE NOT PRESENT R25
001006,000952: # 00511 LR ANTENNA MOVED AND NOT REPOSITIONED SERVICER
001007,000953: # 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
001008,000954: # 00515 RR CDU FAIL DISCRETE PRESENT R25
001009,000955: # 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
001010,000956: # 00522 LANDING RADAR POSITION CHANGE R04
001011,000957: # 00523 LR ANTENNA DIDN'T ACHIEVE POSITION 2 V59 IN V60)
001012,000958: # 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
001013,000959: # 00526 RANGE GREATER THAN 400 NAUTICAL MILES P20
001014,000960: # 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21,R24
001015,000961: # LUNAR SURFACE
001016,000962: # OR VEHICLE MANEUVER REQUIRED R24 (20)
001017,000963: # 00530 P LOS NOT IN MODE2 COVERAGE R21
001018,000964: # ON LUNAR SURFACE AFTER 600 SECS.
001019,000965: # 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
001020,000966: # 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32,P72,
001021,000967: # 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32,P72,
001022,000968: # 00603 CSI TO CDH TIME LT TMIN12 P32,P72,P33,P73
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001024,000970: # 00604 CDH TO TPI TIME LT TMIN23 P32,P72,
001025,000971: # OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
001026,000972: # 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
001027,000973: # 00606 DV EXCEEDS MAXIMUM P32,P72,
001028,000974: # 00611 NO TIG FOR GIVEN ELEV ANGLE P34,P74
001029,000975: # 00701 ILLEGAL OPTION CODE SELECTED P57
001030,000976: # 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
001031,000977: # 01102 AGC SELF TEST ERROR SELF CHECK
001032,000978: # 01105 DOWNLINK TOO FAST T4RUPT
001033,000979: # 01106 UPLINK TOO FAST T4RUPT
001034,000980: # 01107 PHASE TABLE FAILURE. ASSUME RESTART
001035,000981: # ERASABLE MEMORY IS SUSPECT. RESTART
001036,000982: # 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
001037,000983: # 01406 BAD RETURN FROM ROOTPSRS DESCENT GUIDANCE EQS.
001038,000984: # 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
001039,000985: # .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
001040,000986: # VECTOR.) S40.8
001041,000987: # 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
001042,000988: # 01412 DESCENT IGNALG NOT CONVERGING P63
001043,000989: # 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
001044,000990: # 01600 OVERFLOW IN DRIFT TEST IMU 4
001045,000991: # 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
001046,000992: # 01601 IMU 4 (LEM)
001047,000993: # 01703 IGNITION TIME SLIPPED MIDTOAVE
001048,000994: # 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
001049,000995: # CONFIGURATION P40, P42
001050,000996: # 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
001051,000997: # 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
001052,000998: # 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
001053,000999: # 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
001054,001000: # 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
001055,001001: # 04777 ICDU , PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001056,001002: # 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
001057,001003: # 10777 IMU , PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001058,001004: # 13777 IMU , ICDU FAILS CAUSED THE ISS WARNING T4RUPT
001059,001005: # 14777 IMU,ICDU,PIPA FAILS CAUSED ISS WARNING T4RUPT
001060,001006:
001061,001007: # THE FOLLOWING CODES INDICATE THE MORE SERIOUS POODOO ABORTS THAT RESULT
001062,001008: # IN THE PROGRAM GOING TO ROO.
001063,001009:
001064,001010: # 20105 AOTMARK SYSTEM IN USE AOTMARK
001065,001011: # 20430 ACCELERATION OVERFLOW IN INTEGRATION ORBITAL INTEGRATION
001066,001012: # 20607 NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET, TIMERAD
001067,001013: # 21103 UNUSED CCS BRANCH EXECUTED ABORT
001068,001014: # 21204 WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
001069,001015: # CALLED WITH ZERO OR NEGATIVE DELTA-TIME
001070,001016: # 21302 SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
001071,001017: # 21406 BAD RETURN FROM ROOTPSRS IGNITION ALGORITHMN
001072,001018: # 21501 KEYBOARD AND DISPLAY ALARM DURING PINBALL
001073,001019: # INTERNAL USE(NVSUB).ABORT
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001075,001021: # THE FOLLOWING CODES INDICATE A BAILOUT ABORT THAT RESULTS IN A SOFTWARE
001076,001022: # RESTART
001077,001023: # 31104 DELAY ROUTINE BUSY EXEC
001078,001024: # 31201 EXECUTIVE OVERFLOW-NO VAC AREAS EXEC
001079,001025: # 31202 EXECUTIVE OVERFLOW-NO CORE SETS EXEC
001080,001026: # 31203 WAITLIST OVERFLOW-TOO MANY TASKS WAITLIST
001081,001027: # 31206 SECOND JOB ATTEMPTS TO GO TO SLEEP VIA PINBALL
001082,001028: # KEYBOARD AND DISPLAY PROGRAM
001083,001029: # 31207 NO VAC AREAS FOR MARKS AOTMARK
001084,001030: # 31210 TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
001085,001031: # 31211 ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
001086,001032: # 31502 TWO PRIO DISPLAYS WAITING DSP INTRFCE
001087,001033: # 32000 DAP STILL IN PROGRESS AT NEXT TIME5 RUPT DAP
001088,001034:
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001090,001036: # CHECKLIST CODES FOR LUMINARY
001091,001037:
001092,001038: # *9 *17 *26 *9 COLUMN
001093,001039:
001094,001040: # R1CODE ACTION TO BE EFFECTED PROGRAM
001095,001041:
001096,001042: # 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
001097,001043: # 00014 PROCEED DO IMU FINE ALIGN ROUTINE P51,P63,P57
001098,001044: # 00014 ENTER DO LANDING SITE DETERMINATION(N89DISP) P57OPTION2
001099,001045: # 00015 PERFORM CELESTIAL BODY ACQUISITION R51,P51
001100,001046: # 00062 SWITCH AGC POWER DOWN P06
001101,001047: # 00201 SWITCH RR MODE TO AUTOMATIC P20,P22,R04
001102,001048: # 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12,P42,P71
001103,001049: # ALSO THR CONT TO AUTO P40,P63,P70
001104,001050: # 00205 PERFORM MANUAL ACQUISITION OF RR R23
001105,001051: # 00500 SWITCH LR ANTENNA TO POSITION 1 P63
001106,001052:
001107,001053: # SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
001108,001054: # PERFORM DENOTES START OR END OF A TASK
001109,001055: # KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
001110,001056:
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001112,001058: # OPTION CODES FOR LUMINARY
001113,001059:
001114,001060: # THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
001115,001061: # CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
001116,001062: # ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
001117,001063:
001118,001064: # *9 *17 *52 *11 *25 COLUMN
001119,001065:
001120,001066: # OPTION
001121,001067: # CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
001122,001068:
001123,001069: # 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
001124,001070: # 4=LAND SITE
001125,001071: # 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
001126,001072: # 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
001127,001073: # 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
001128,001074: # 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
001129,001075: # 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
001130,001076: # 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
001131,001077: # 2=TWO BODIES 3=ONE BODY + G
001132,001078: # 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
001133,001079: # ORBIT TO PASS OVER LM
End of include-file ASSEMBLY_AND_OPERATION_INFORMATION.agc. Parent file is MAIN.agc