Source Code
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This is a reconstruction of the AGC program Luminary 99 Rev 0. It was the third release
of the Lunar Module flight software targeted for use in Apollo 11, after Luminary 96 and 97.
A bug (which had been around since at least Apollo 10, Luminary 69) was
discovered in Rev 0 shortly before the Apollo 11 flight, resulting in a last minute
revision into Rev 1,
which is what actually flew rather than
the Rev 0 presented here. A hardcopy of Rev 0 is known to
exist — it belonged to AGC developer Allan Klumpp for many years — but
unfortunately the Virtual AGC Project has not had access to that hardcopy. Thus
the code you see here had been reconstructed (we believe accurately) rather than
transcribed. The first step of the reconstruction of the Rev 0 source code was
the transcription of the Rev 1 source code from a hardcopy in the MIT Museum collection.
The process of reverting the active portion of the source code (i.e., other than
program comments) from Rev 1 to Rev 0 was very minor, consisting
only of moving the position of the STARTSB1 label in
FRESH START AND RESTART. Allan had previously given
us the checksums of the memory banks of Rev 0, and we have verified the program presented here has checksums
identical to all banks of Allan's listing of Rev 0. The notations on Allan's Rev 0 program listing read,
in part:GAP: ASSEMBLE REVISION 099 OF AGC PROGRAM LUMINARY BY NASA 2021112-051 A single program comment is known to differ between Rev 0 and Rev 1, but these are harder to reconstruct and verify than changes to the active portion of the code. Thus it is possible that there are additional differences between the program comments in Rev 0 and Rev 1 that are unknown to us, and therefore are not reflected in the code presented here. |
000081,000002: ## Copyright: Public domain.
000082,000003: ## Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
000083,000004: ## Purpose: Part of the reconstructed source code for LMY99 Rev 0,
000084,000005: ## otherwise known as Luminary Rev 99, the third release
000085,000006: ## of the Apollo Guidance Computer (AGC) software for Apollo 11.
000086,000007: ## It differs from LMY99 Rev 1 (the flown version) only in the
000087,000008: ## placement of a single label. The corrections shown here have
000088,000009: ## been verified to have the same bank checksums as AGC developer
000089,000010: ## Allan Klumpp's copy of Luminary Rev 99, and so are believed
000090,000011: ## to be accurate. This file is intended to be a faithful
000091,000012: ## recreation, except that the code format has been changed to
000092,000013: ## conform to the requirements of the yaYUL assembler rather than
000093,000014: ## the original YUL assembler.
000094,000015: ##
000095,000016: ## Assembler: yaYUL
000096,000017: ## Contact: Jim Lawton <jim.lawton@gmail.com>
000097,000018: ## Website: www.ibiblio.org/apollo.
000098,000019: ## Pages: 001-027
000099,000020: ## Mod history: 2009-05-16 JVL Transcribed from page images.
000100,000021: ## 2016-12-11 RSB Proofed text comments with octopus/ProoferComments
000101,000022: ## and corrected the errors found.
000102,000023: ## 2017-01-04 MAS A few typos found during Luminary 69 transcription.
000103,000024: ## 2017-01-25 RSB Back-ported a typo-fix found while proofing Luminary 69.
000104,000025: ## 2017-03-14 RSB Comment-text fixes identified in 5-way
000105,000026: ## side-by-side diff of Luminary 69/99/116/131/210.
000106,000027: ## 2017-08-01 MAS Created from LMY99 Rev 1, and modified to make
000107,000028: ## equivalent to LMY99 Rev 0 / Luminary Rev 99.
000108,000029:
000109,000030: ## This source code has been transcribed or otherwise adapted from
000110,000031: ## digitized images of a hardcopy from the MIT Museum. The digitization
000111,000032: ## was performed by Paul Fjeld, and arranged for by Deborah Douglas of
000112,000033: ## the Museum. Many thanks to both. The images (with suitable reduction
000113,000034: ## in storage size and consequent reduction in image quality as well) are
000114,000035: ## available online at www.ibiblio.org/apollo. If for some reason you
000115,000036: ## find that the images are illegible, contact me at info@sandroid.org
000116,000037: ## about getting access to the (much) higher-quality images which Paul
000117,000038: ## actually created.
000118,000039: ##
000119,000040: ## The code has been modified to match LMY99 Revision 0, otherwise
000120,000041: ## known as Luminary Revision 99, the Apollo 11 software release preceeding
000121,000042: ## the listing from which it was transcribed. It has been verified to
000122,000043: ## contain the same bank checksums as AGC developer Allan Klumpp's listing
000123,000044: ## of Luminary Revision 99 (for which we do not have scans).
000124,000045: ##
000125,000046: ## Notations on Allan Klumpp's listing read, in part:
000126,000047: ##
000127,000048: ## ASSEMBLE REVISION 099 OF AGC PROGRAM LUMINARY BY NASA 2021112-51
000128,000049:
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Page 1 |
000130,000051:
000131,000052: # THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
000132,000053: # THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
000133,000054:
000134,000055: # GUIDANCE SYSTEM OPERATIONS PLAN
000135,000056: # FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
000136,000057: # USING PROGRAM LUMINARY
000137,000058:
000138,000059: # THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
000139,000060: # TECHNOLOGY 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS UNDER PROJECT 55-238-70, SPONSORED BY THE MANNED
000140,000061: # SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065.
000141,000062:
000142,000063: # THIS PROGRAM IS REFERRED TO AS LUMINARY 1A
000143,000064:
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Page 2 |
000145,000066:
000146,000067: # TABLE OF LOG CARDS
000147,000068: # ASSEMBLY AND OPERATION INFORMATION
000148,000069: # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
000149,000070: # CONTROLLED CONSTANTS
000150,000071: # INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
000151,000072: # FLAGWORD ASSIGNMENTS
000152,000073: # SUBROUTINE CALLS
000153,000074:
000154,000075: # TABLE OF SUBROUTINE LOG SECTIONS
000155,000076: # LUMERASE
000156,000077: # ERASABLE ASSIGNMENTS
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The following comment line reads "LNYAIDE" in LMY99 Rev 1. |
000158,000079: # LEMONAID
000159,000080: # INTERRUPT LEAD INS
000160,000081: # T4RUPT PROGRAM
000161,000082: # RCS FAILURE MONITOR
000162,000083: # DOWNLINK LISTS
000163,000084: # AGS INITIALIZATION
000164,000085: # FRESH START AND RESTART
000165,000086: # RESTART TABLES
000166,000087: # AOTMARK
000167,000088: # EXTENDED VERBS
000168,000089: # PINBALL NOUN TABLES
000169,000090: # LEM GEOMETRY
000170,000091: # IMU COMPENSATION PACKAGE
000171,000092: # R63
000172,000093: # ATTITUDE MANEUVER ROUTINE
000173,000094: # GIMBAL LOCK AVOIDANCE
000174,000095: # KALCMANU STEERING
000175,000096: # SYSTEM TEST STANDARD LEAD INS
000176,000097: # IMU PERFORMANCE TESTS 2
000177,000098: # IMU PERFORMANCE TESTS 4
000178,000099: # PINBALL GAMES BUTTONS AND LIGHTS
000179,000100: # R60,R62
000180,000101: # S-BAND ANTENNA FOR LM
000181,000102: # LEMP20S
000182,000103: # RADAR LEADIN ROUTINES
000183,000104: # P20-P25
000184,000105: # LEMP30S
000185,000106: # P30,P37
000186,000107: # P32-P35, P72-P75
000187,000108: # GENERAL LAMBERT AIMPOINT GUIDANCE
000188,000109: # KISSING
000189,000110: # GROUND TRACKING DETERMINATION PROGRAM - P21
000190,000111: # P34-P35, P74-P75
000191,000112: # R31
000192,000113: # P76
000193,000114: # R30
000194,000115: # STABLE ORBIT - P38-P39
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Page 3 |
000196,000117: # FLY
000197,000118: # BURN, BABY, BURN -- MASTER IGNITION ROUTINE
000198,000119: # P40-P47
000199,000120: # THE LUNAR LANDING
000200,000121: # THROTTLE CONTROL ROUTINES
000201,000122: # LUNAR LANDING GUIDANCE EQUATIONS
000202,000123: # P70-P71
000203,000124: # P12
000204,000125: # ASCENT GUIDANCE
000205,000126: # SERVICER
000206,000127: # LANDING ANALOG DISPLAYS
000207,000128: # FINDCDUW - GUIDAP INTERFACE
000208,000129: # LEMP50S
000209,000130: # P51-P53
000210,000131: # LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
000211,000132: # SKIPPER
000212,000133: # DOWN-TELEMETRY PROGRAM
000213,000134: # INTER-BANK COMMUNICATION
000214,000135: # INTERPRETER
000215,000136: # FIXED-FIXED CONSTANT POOL
000216,000137: # INTERPRETIVE CONSTANTS
000217,000138: # SINGLE PRECISION SUBROUTINES
000218,000139: # EXECUTIVE
000219,000140: # WAITLIST
000220,000141: # LATITUDE LONGITUDE SUBROUTINES
000221,000142: # PLANETARY INERTIAL ORIENTATION
000222,000143: # MEASUREMENT INCORPORATION
000223,000144: # CONIC SUBROUTINES
000224,000145: # INTEGRATION INITIALIZATION
000225,000146: # ORBITAL INTEGRATION
000226,000147: # INFLIGHT ALIGNMENT ROUTINES
000227,000148: # POWERED FLIGHT SUBROUTINES
000228,000149: # TIME OF FREE FALL
000229,000150: # AGC BLOCK TWO SELF-CHECK
000230,000151: # PHASE TABLE MAINTENANCE
000231,000152: # RESTARTS ROUTINE
000232,000153: # IMU MODE SWITCHING ROUTINES
000233,000154: # KEYRUPT, UPRUPT
000234,000155: # DISPLAY INTERFACE ROUTINES
000235,000156: # SERVICE ROUTINES
000236,000157: # ALARM AND ABORT
000237,000158: # UPDATE PROGRAM
000238,000159: # RTB OP CODES
000239,000160: # LMDAP
000240,000161: # T6-RUPT PROGRAMS
000241,000162: # DAP INTERFACE SUBROUTINES
000242,000163: # DAPIDLER PROGRAM
000243,000164: # P-AXIS RCS AUTOPILOT
000244,000165: # Q,R-AXIS RCS AUTOPILOT
000245,000166: # TJET LAW
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Page 4 |
000247,000168: # KALMAN FILTER
000248,000169: # TRIM GIMBAL CONTROL SYSTEM
000249,000170: # AOSTASK AND AOSJOB
000250,000171: # SPS BACK-UP RCS CONTROL
000251,000172:
000252,000173: # SYMBOL TABLE LISTING
000253,000174: # UNREFERENCED SYMBOL LISTING
000254,000175: # ERASABLE & EQUALS CROSS-REFERENCE TABLE
000255,000176: # SUMMARY OF SYMBOL TABLE LISTINGS
000256,000177: # MEMORY TYPE & AVAILABLITY DISPLAY
000257,000178: # COUNT TABLE
000258,000179: # PARAGRAPHS GENERATED FOR THIS ASSEMBLY
000259,000180: # OCTAL LISTING
000260,000181: # OCCUPIED LOCATIONS TABLE
000261,000182: # SUBROS CALLED & PROGRAM STATUS
000262,000183:
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Page 5 |
000264,000185: # VERB LIST FOR LUMINARY
000265,000186:
000266,000187: # REGULAR VERBS
000267,000188:
000268,000189: # 00 NOT IN USE
000269,000190: # 01 DISPLAY OCTAL COMP 1 IN R1
000270,000191: # 02 DISPLAY OCTAL COMP 2 IN R1
000271,000192: # 03 DISPLAY OCTAL COMP 3 IN R1
000272,000193: # 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
000273,000194: # 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
000274,000195: # 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000275,000196: # 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
000276,000197: # 08
000277,000198: # 09
000278,000199: # 10
000279,000200: # 11 MONITOR OCTAL COMP 1 IN R1
000280,000201: # 12 MONITOR OCTAL COMP 2 IN R1
000281,000202: # 13 MONITOR OCTAL COMP 3 IN R1
000282,000203: # 14 MONITOR OCTAL COMP 1,2 IN R1,R2
000283,000204: # 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
000284,000205: # 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000285,000206: # 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
000286,000207: # 18
000287,000208: # 19
000288,000209: # 20
000289,000210: # 21 LOAD COMPONENT 1 INTO R1
000290,000211: # 22 LOAD COMPONENT 2 INTO R2
000291,000212: # 23 LOAD COMPONENT 3 INTO R3
000292,000213: # 24 LOAD COMPONENT 1,2 INTO R1,R2
000293,000214: # 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
000294,000215: # 26
000295,000216: # 27 DISPLAY FIXED MEMORY
000296,000217: # 28
000297,000218: # 29
000298,000219: # 30 REQUEST EXECUTIVE
000299,000220: # 31 REQUEST WAITLIST
000300,000221: # 32 RECYCLE PROGRAM
000301,000222: # 33 PROCEED WITHOUT DSKY INPUTS
000302,000223: # 34 TERMINATE FUNCTION
000303,000224: # 35 TEST LIGHTS
000304,000225: # 36 REQUEST FRESH START
000305,000226: # 37 CHANGE PROGRAM (MAJOR MODE)
000306,000227: # 38
000307,000228: # 39
000308,000229:
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Page 6 |
000310,000231: # EXTENDED VERBS
000311,000232:
000312,000233: # 40 ZERO CDU-S
000313,000234: # 41 COARSE ALIGN CDU-S
000314,000235: # 42 FINE ALIGN IMU
000315,000236: # 43 LOAD IMU ATT ERROR METERS
000316,000237: # 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
000317,000238: # 45
000318,000239: # 46
000319,000240: # 47 INITIALIZE AGS (R47)
000320,000241: # 48 REQUEST DAP DATA LOAD ROUTINE (R03)
000321,000242: # 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
000322,000243: # 50 PLEASE PERFORM
000323,000244: # 51
000324,000245: # 52 MARK X-RETICLE
000325,000246: # 53 MARK Y-RETICLE
000326,000247: # 54 MARK X OR Y-RETICLE
000327,000248: # 55 INCREMENT AGC TIME (DECIMAL)
000328,000249: # 56 TERMINATE TRACKING (P20 + P25)
000329,000250: # 57 PERMIT LANDING RADAR UPDATES
000330,000251: # 58 INHIBIT LANDING RADAR UPDATES
000331,000252: # 59
000332,000253: # 60 COMMAND LR TO POSITION 2.
000333,000254: # 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
000334,000255: # 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
000335,000256: # 63 SAMPLE RADAR ONCE PER SECOND (R04).
000336,000257: # 64 REQUEST S-BAND ANTENNA ROUTINE (R05)
000337,000258: # 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
000338,000259: # 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
000339,000260: # 67 DISPLAY W MATRIX
000340,000261: # 68
000341,000262: # 69 CAUSE RESTART
000342,000263: # 70 UPDATE LIFTOFF TIME
000343,000264: # 71 UNIVERSAL UPDATE-BLOCK ADR
000344,000265: # 72 UNIVERSAL UPDATE-SINGLE ADR
000345,000266: # 73 UPDATE AGC TIME (OCTAL)
000346,000267: # 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
000347,000268: # 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
000348,000269: # 76 MINIMUM IMPULSE COMMAND MODE
000349,000270: # 77 RATE COMMAND AND ATTITUDE HOLD MODE
000350,000271: # 78 LR SPURIOUS RETURN TEST START (R77)
000351,000272: # 79 LR SPURIOUS RETURN TEST STOP
000352,000273: # 80 UPDATE LEM STATE VECTOR
000353,000274: # 81 UPDATE CSM STATE VECTOR
000354,000275: # 82 REQUEST ORBIT PARAM DISPLAY (R30)
000355,000276: # 83 REQUEST REND PARAM DISPLAY (R31)
000356,000277: # 84
000357,000278: # 85 DISPLAY RR LOS AZ AND ELEV
000358,000279: # 86
000359,000280: # 87
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Page 7 |
000361,000282: # 88
000362,000283: # 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
000363,000284: # 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
000364,000285: # 91 DISPLAY BANK SUM
000365,000286: # 92 OPERATE IMU PERFORMANCE TEST (P07)
000366,000287: # 93 ENABLE W MATRIX INITIALIZATION
000367,000288: # 94
000368,000289: # 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
000369,000290: # 96 INTERRUPT INTEGRATION AND GO TO POO
000370,000291: # 97 PERFORM ENGINE FAIL PROCEDURE
000371,000292: # 98
000372,000293: # 99 PLEASE ENABLE ENGINE
000373,000294:
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Page 8 |
000375,000296: # IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
000376,000297: # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
000377,000298: # SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
000378,000299: # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23
000379,000300: # MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
000380,000301: # ABOVE SCALE TYPES.
000381,000302:
000382,000303: # THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
000383,000304: # EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
000384,000305:
000385,000306: # NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000386,000307: # 00 NOT IN USE
000387,000308: # 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH
000388,000309: # 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH
000389,000310: # 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP XXX.XX DEG FOR EACH
000390,000311: # 04 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000391,000312: # 05 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000392,000313: # 06 OPTION CODE 3COMP OCTAL ONLY FOR EACH
000393,000314: # LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
000394,000315: # 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
000395,000316: # ONES FOR BITS TO BE MODIFIED
000396,000317: # 1 TO SET OR 0 TO RESET SELECTED BITS
000397,000318: # 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
000398,000319: # 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
000399,000320: # 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
000400,000321: # 11 TIG OF CSI 3COMP 00XXX. HRS DEC ONLY
000401,000322: # 000XX. MIN MUST LOAD 3 COMPS
000402,000323: # 0XX.XX SEC
000403,000324: # 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
000404,000325: # (USED BY EXTENDED VERBS ONLY)
000405,000326: # 13 TIG OF CDH 3COMP 00XXX. HRS DEC ONLY
000406,000327: # 000XX. MIN MUST LOAD 3 COMPS
000407,000328: # 0XX.XX SEC
000408,000329: # 14 CHECKLIST 3COMP XXXXX. FOR EACH
000409,000330: # (USED BY EXTENDED VERBS ONLY)
000410,000331: # (NOUN 25 IS PASTED AFTER DISPLAY)
000411,000332: # 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
000412,000333: # 16 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000413,000334: # (USED BY EXTENDED VERBS ONLY) 000XX. MIN MUST LOAD 3 COMPS
000414,000335: # 0XX.XX SEC
000415,000336: # 17 SPARE
000416,000337: # 18 AUTO MANEUVER BALL ANGLES 3COMP XXX.XX DEG FOR EACH
000417,000338: # 19 SPARE
000418,000339: # 20 ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000419,000340: # 21 PIPAS 3COMP XXXXX. PULSES FOR EACH
000420,000341: # 22 NEW ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000421,000342: # 23 SPARE
000422,000343: # 24 DELTA TIME FOR AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000423,000344: # 000XX. MIN MUST LOAD 3 COMPS
000424,000345: # 0XX.XX SEC
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Page 9 |
000426,000347: # 25 CHECKLIST 3COMP XXXXX. FOR EACH
000427,000348: # (USED WITH PLEASE PERFORM ONLY)
000428,000349: # 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
000429,000350: # 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX.
000430,000351: # 28 SPARE
000431,000352: # 29 SPARE
000432,000353: # 30 SPARE
000433,000354: # 31 SPARE
000434,000355: # 32 TIME FROM PERIGEE 3COMP 00XXX. HRS DEC ONLY
000435,000356: # 000XX. MIN MUST LOAD 3 COMPS
000436,000357: # 0XX.XX SEC
000437,000358: # 33 TIME OF IGNITION 3COMP 00XXX. HRS DEC ONLY
000438,000359: # 000XX. MIN MUST LOAD 3 COMPS
000439,000360: # 0XX.XX SEC
000440,000361: # 34 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000441,000362: # 000XX. MIN MUST LOAD 3 COMPS
000442,000363: # 0XX.XX SEC
000443,000364: # 35 TIME FROM EVENT 3COMP 00XXX. HRS DEC ONLY
000444,000365: # 000XX. MIN MUST LOAD 3 COMPS
000445,000366: # 0XX.XX SEC
000446,000367: # 36 TIME OF AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000447,000368: # 000XX. MIN MUST LOAD 3 COMPS
000448,000369: # 0XX.XX SEC
000449,000370: # 37 TIG OF TPI 3COMP 00XXX. HRS DEC ONLY
000450,000371: # 000XX. MIN MUST LOAD 3 COMPS
000451,000372: # 0XX.XX SEC
000452,000373: # 38 TIME OF STATE BEING INTEGRATED 3COMP 00XXX. HRS DEC ONLY
000453,000374: # 000XX. MIN MUST LOAD 3 COMPS
000454,000375: # 0XX.XX SEC
000455,000376: # 39 SPARE
000456,000377:
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Page 10 |
000458,000379: # MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000459,000380: # 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000460,000381: # VG, XXXX.X FT/SEC
000461,000382: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000462,000383: # 41 TARGET AZIMUTH, 2COMP XXX.XX DEG (FOR SYSTEM TEST)
000463,000384: # ELEVATION XX.XXX DEG
000464,000385: # 42 APOGEE, 3COMP XXXX.X NAUT MI DEC ONLY
000465,000386: # PERIGEE, XXXX.X NAUT MI
000466,000387: # DELTA V (REQUIRED) XXXX.X FT/SEC
000467,000388: # 43 LATITUDE, 3COMP XXX.XX DEG DEC ONLY
000468,000389: # LONGITUDE, XXX.XX DEG
000469,000390: # ALTITUDE XXXX.X NAUT MI
000470,000391: # 44 APOGEE, 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000471,000392: # PERIGEE, XXXX.X NAUT MI
000472,000393: # TFF XXBXX MIN/SEC
000473,000394: # 45 MARKS, 3COMP XXXXX. NO LOAD, DEC ONLY
000474,000395: # TFI OF NEXT BURN XXBXX MIN/SEC
000475,000396: # MGA XXX.XX DEG
000476,000397: # 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
000477,000398: # 47 LEM WEIGHT, 2COMP XXXXX. LBS DEC ONLY
000478,000399: # CSM WEIGHT XXXXX. LBS
000479,000400: # 48 GIMBAL PITCH TRIM, 2COMP XXX.XX DEG DEC ONLY
000480,000401: # GIMBAL ROLL TRIM XXX.XX DEG
000481,000402: # 49 DELTA R, 3COMP XXXX.X NAUT MI DEC ONLY
000482,000403: # DELTA V, XXXX.X FT/SEC
000483,000404: # RADAR DATA SOURCE CODE XXXXX.
000484,000405: # 50 SPARE
000485,000406: # 51 S-BAND ANTENNA ANGLES PITCH 2COMP XXX.XX DEG DEC ONLY
000486,000407: # YAW XXX.XX DEG
000487,000408: # 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG
000488,000409: # 53 SPARE
000489,000410: # 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
000490,000411: # RANGE RATE, XXXX.X FT/SEC
000491,000412: # THETA XXX.XX DEG
000492,000413: # 55 NO. OF APSIDAL CROSSINGS 3COMP XXXXX. DEC ONLY
000493,000414: # ELEVATION ANGLE XXX.XX DEG
000494,000415: # CENTRAL ANGLE OF PASSIVE VEHICLE XXX.XX DEG
000495,000416: # 56 RR LOS AZIMUTH 2COMP XXX.XX DEG
000496,000417: # ELEVATION XXX.XX DEG
000497,000418: # 57 DELTA R 1COMP XXXX.X NAUT MI DEC ONLY
000498,000419: # 58 PERIGEE ALT (POST TPI) 3COMP XXXX.X NAUT MI DEC ONLY
000499,000420: # DELTA V TPI XXXX.X FT/SEC
000500,000421: # DELTA V TPF XXXX.X FT/SEC
000501,000422: # 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY
000502,000423: # 60 HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000503,000424: # ALTITUDE RATE XXXX.X FT/SEC
000504,000425: # COMPUTED ALTITUDE XXXXX. FEET
000505,000426: # 61 TIME TO GO IN BRAKING PHASE 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000506,000427: # TIME FROM IGNITION XXBXX MIN/SEC
|
|
Page 11 |
000508,000429: # CROSS RANGE DISTANCE XXXX.X NAUT MI
000509,000430: # 62 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC NO LOAD, DEC ONLY
000510,000431: # TIME FROM IGNITION XXBXX MIN/SEC
000511,000432: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000512,000433: # 63 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000513,000434: # ALTITUDE RATE XXXX.X FT/SEC
000514,000435: # COMPUTED ALTITUDE XXXXX. FEET
000515,000436: # 64 TIME LEFT FOR REDESIGNATION- LPD ANGLE 3COMP XXBXX NO LOAD, DEC ONLY
000516,000437: # ALTITUDE RATE XXXX.X FT/SEC
000517,000438: # COMPUTED ALTITUDE XXXXX. FEET
000518,000439: # 65 SAMPLED AGC TIME 3COMP 00XXX. HRS DEC ONLY
000519,000440: # (FETCHED IN INTERRUPT) 000XX. MIN MUST LOAD 3 COMPS
000520,000441: # 0XX.XX SEC
000521,000442: # 66 LR RANGE 2COMP XXXXX. FEET NO LOAD, DEC ONLY
000522,000443: # POSITION +0000X
000523,000444: # 67 LRVX 3COMP XXXXX. FT/SEC
000524,000445: # LRVY XXXXX. FT/SEC
000525,000446: # LRVZ XXXXX. FT/SEC
000526,000447: # 68 SLANT RANGE TO LANDING SITE 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000527,000448: # TIME TO GO IN BRAKING PHASE XXBXX MIN/SEC
000528,000449: # LR ALTITUDE - COMPUTED ALTITUDE XXXXX. FEET
000529,000450: # 69 SPARE
000530,000451: # 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000531,000452: # 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000532,000453: # 72 RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000533,000454: # SHAFT ANGLE XXX.XX DEG
000534,000455: # 73 NEW RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000535,000456: # SHAFT ANGLE XXX.XX DEG
000536,000457: # 74 TIME FROM IGNITION 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000537,000458: # YAW AFTER VEHICLE RISE XXX.XX DEG
000538,000459: # PITCH AFTER VEHICLE RISE XXX.XX DEG
000539,000460: # 75 DELTA ALTITUDE CDH 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000540,000461: # DELTA TIME (CDH-CSI OR TPI-CDH) XXBXX MIN/SEC
000541,000462: # DELTA TIME (TPI-CDH OR TPI-NOMTPI) XXBXX MIN/SEC
000542,000463: # 76 DESIRED HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000543,000464: # DESIRED RADIAL VELOCITY XXXX.X FT/SEC
000544,000465: # CROSS-RANGE DISTANCE XXXX.X NAUT MI
000545,000466: # 77 TIME TO ENGINE CUTOFF 2COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000546,000467: # VELOCITY NORMAL TO CSM PLANE XXXX.X FT/SEC
000547,000468: # 78 RR RANGE 2COMP XXX.XX NAUT MI
000548,000469: # RANGE RATE XXXXX. FT/SEC
000549,000470: # 79 CURSOR ANGLE 3COMP XXX.XX DEG DEC ONLY
000550,000471: # SPIRAL ANGLE XXX.XX DEG
000551,000472: # POSITION CODE XXXXX.
000552,000473: # 80 DATA INDICATOR, 2COMP XXXXX.
000553,000474: # OMEGA XXX.XX DEG
000554,000475: # 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
|
|
Page 12 |
000556,000477: # 82 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000557,000478: # 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000558,000479: # 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000559,000480: # 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000560,000481: # 86 VG (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000561,000482: # 87 BACKUP OPTICS LOS AZIMUTH 2COMP XXX.XX DEG
000562,000483: # ELEVATION XXX.XX DEG
000563,000484: # 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY
000564,000485: # 89 LANDMARK LATITUDE 3COMP XX.XXX DEG DEC ONLY
000565,000486: # LONGITUDE/2 XX.XXX DEC
000566,000487: # ALTITUDE XXX.XX NAUT MI
000567,000488: # 90 Y 3COMP XXX.XX NM DEC ONLY
000568,000489: # Y DOT XXXX.X FPS
000569,000490: # PSI XXX.XX DEG
000570,000491: # 91 ALTITUDE 3COMP XXXXXB. NAUT MI
000571,000492: # VELOCITY XXXXX. FT/SEC
000572,000493: # FLIGHT PATH ANGLE XXX.XX DEG
000573,000494: # 92 SPARE
000574,000495: # 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
000575,000496: # 94 SPARE
000576,000497: # 95 SPARE
000577,000498: # 96 SPARE
000578,000499: # 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH
000579,000500: # 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX.
000580,000501: # .XXXXX
000581,000502: # XXXXX.
000582,000503: # 99 RMS IN POSITION 3COMP XXXXX. FT DEC ONLY
000583,000504: # RMS IN VELOCITY XXXX.X FT/SEC
000584,000505: # RMS IN BIAS XX.XXX RADIANS
000585,000506:
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Page 13 |
000587,000508: # REGISTERS AND SCALING FOR NORMAL NOUNS
000588,000509:
000589,000510: # NOUN REGISTER SCALE TYPE
000590,000511: # 00 NOT IN USE
000591,000512: # 01 SPECIFY ADDRESS B
000592,000513: # 02 SPECIFY ADDRESS C
000593,000514: # 03 SPECIFY ADDRESS D
000594,000515: # 04 DSPTEM1 H
000595,000516: # 05 DSPTEM1 H
000596,000517: # 06 OPTION1 A
000597,000518: # 07 XREG A
000598,000519: # 08 ALMCADR A
000599,000520: # 09 FAILREG A
000600,000521: # 10 SPECIFY CHANNEL A
000601,000522: # 11 TCSI K
000602,000523: # 12 OPTIONX A
000603,000524: # 13 TCDH K
000604,000525: # 14 DSPTEMX C
000605,000526: # 15 INCREMENT ADDRESS A
000606,000527: # 16 DSPTEMX C
000607,000528: # 17 SPARE
000608,000529: # 18 FDAIX D
000609,000530: # 19 SPARE
000610,000531: # 20 CDUX D
000611,000532: # 21 PIPAX C
000612,000533: # 22 THETAD D
000613,000534: # 23 SPARE
000614,000535: # 24 DSPTEM2 +1 K
000615,000536: # 25 DSPTEM1 C
000616,000537: # 26 DSPTEM1 A
000617,000538: # 27 SMODE C
000618,000539: # 28 SPARE
000619,000540: # 29 SPARE
000620,000541: # 30 SPARE
000621,000542: # 31 SPARE
000622,000543: # 32 -TPER K
000623,000544: # 33 TIG K
000624,000545: # 34 DSPTEM1 K
000625,000546: # 35 TTOGO K
000626,000547: # 36 TIME2 K
000627,000548: # 37 TTPI K
000628,000549: # 38 TET K
000629,000550: # 39 SPARE
000630,000551:
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|
Page 14 |
000632,000553: # REGISTERS AND SCALING FOR MIXED NOUNS
000633,000554:
000634,000555: # NOUN COMP REGISTER SCALE TYPE
000635,000556: # 40 1 TTOGO L
000636,000557: # 2 VGDISP S
000637,000558: # 3 DVTOTAL S
000638,000559: # 41 1 DSPTEM1 D
000639,000560: # 2 DSPTEM1 +1 E
000640,000561: # 42 1 HAPO Q
000641,000562: # 2 HPER Q
000642,000563: # 3 VGDISP S
000643,000564: # 43 1 LAT H
000644,000565: # 2 LONG H
000645,000566: # 3 ALT Q
000646,000567: # 44 1 HAPOX Q
000647,000568: # 2 HPERX Q
000648,000569: # 3 TFF L
000649,000570: # 45 1 TRKMKCNT C
000650,000571: # 2 TTOGO L
000651,000572: # 3 +MGA H
000652,000573: # 46 1 DAPDATR1 A
000653,000574: # 47 1 LEMMASS KK
000654,000575: # 2 CSMMASS KK
000655,000576: # 48 1 PITTIME NN
000656,000577: # 2 ROLLTIME NN
000657,000578: # 49 1 R22DISP Q
000658,000579: # 2 R22DISP +2 S
000659,000580: # 3 WHCHREAD C
000660,000581: # 50 SPARE
000661,000582: # 51 1 ALPHASB H
000662,000583: # 2 BETASB H
000663,000584: # 52 1 ACTCENT H
000664,000585: # 53 SPARE
000665,000586: # 54 1 RANGE JJ
000666,000587: # 2 RRATE S
000667,000588: # 3 RTHETA H
000668,000589: # 55 1 NN C
000669,000590: # 2 ELEV H
000670,000591: # 3 CENTANG H
000671,000592: # 56 1 RR-AZ H
000672,000593: # 2 RR-ELEV H
000673,000594: # 57 1 DELTAR Q
000674,000595: # 58 1 POSTTPI Q
000675,000596: # 2 DELVTPI S
000676,000597: # 3 DELVTPF S
000677,000598: # 59 1 DVLOS S
000678,000599: # 2 DVLOS +2 S
000679,000600: # 3 DVLOS +4 S
000680,000601: # 60 1 VHORIZ S
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|
Page 15 |
000682,000603: # 2 HDOTDISP S
000683,000604: # 3 HCALC RR
000684,000605: # 61 1 TTFDISP L
000685,000606: # 2 TTOGO L
000686,000607: # 3 OUTOFPLN QQ
000687,000608: # 62 1 ABVEL S
000688,000609: # 2 TTOGO L
000689,000610: # 3 DVTOTAL S
000690,000611: # 63 1 ABVEL S
000691,000612: # 2 HDOTDISP S
000692,000613: # 3 HCALC1 RR
000693,000614: # 64 1 FUNNYDSP PP
000694,000615: # 2 HDOTDISP S
000695,000616: # 3 HCALC RR
000696,000617: # 65 1 SAMPTIME K
000697,000618: # 2 SAMPTIME K
000698,000619: # 3 SAMPTIME K
000699,000620: # 66 1 RSTACK +6 W
000700,000621: # 2 CHANNEL 33 TT
000701,000622: # 67 1 RSTACK X
000702,000623: # 2 RSTACK +2 Y
000703,000624: # 3 RSTACK +4 Z
000704,000625: # 68 1 RANGEDSP QQ
000705,000626: # 2 TTFDISP L
000706,000627: # 3 DELTAH RR
000707,000628: # 69 SPARE
000708,000629: # 70 1 AOTCODE A
000709,000630: # 2 AOTCODE +1 A
000710,000631: # 3 AOTCODE +2 A
000711,000632: # 71 1 AOTCODE A
000712,000633: # 2 AOTCODE +1 A
000713,000634: # 3 AOTCODE +2 A
000714,000635: # 72 1 CDUT WW
000715,000636: # 2 CDUS D
000716,000637: # 73 1 TANG WW
000717,000638: # 2 TANG +1 D
000718,000639: # 74 1 TTOGO L
000719,000640: # 2 YAW H
000720,000641: # 3 PITCH H
000721,000642: # 75 1 DIFFALT Q
000722,000643: # 2 T1TOT2 L
000723,000644: # 3 T2TOT3 L
000724,000645: # 76 1 ZDOTD S
000725,000646: # 2 RDOTD S
000726,000647: # 3 XRANGE Q
000727,000648: # 77 1 TTOGO L
000728,000649: # 2 YDOT S
000729,000650: # 78 1 RSTACK U
000730,000651: # 2 RSTACK +2 V
000731,000652: # 79 1 CURSOR D
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|
Page 16 |
000733,000654: # 2 SPIRAL D
000734,000655: # 3 POSCODE C
000735,000656: # 80 1 DATAGOOD C
000736,000657: # 2 OMEGAD H
000737,000658: # 81 1 DELVLVC S
000738,000659: # 2 DELVLVC +2 S
000739,000660: # 3 DELVLVC +4 S
000740,000661: # 82 1 DELVLVC S
000741,000662: # 2 DELVLVC +2 S
000742,000663: # 3 DELVLVC +4 S
000743,000664: # 83 1 DELVIMU S
000744,000665: # 2 DELVIMU +2 S
000745,000666: # 3 DELVIMU +4 S
000746,000667: # 84 1 DELVOV S
000747,000668: # 2 DELVOV +2 S
000748,000669: # 3 DELVOV +4 S
000749,000670: # 85 1 VGBODY S
000750,000671: # 2 VGBODY +2 S
000751,000672: # 3 VGBODY +4 S
000752,000673: # 86 1 DELVLVC S
000753,000674: # 2 DELVLVC +2 S
000754,000675: # 3 DELVLVC +4 S
000755,000676: # 87 1 AZ D
000756,000677: # 2 EL D
000757,000678: # 88 1 STARAD B
000758,000679: # 2 STARAD +2 B
000759,000680: # 3 STARAD +4 B
000760,000681: # 89 1 LANDLAT G
000761,000682: # 2 LANDLONG G
000762,000683: # 3 LANDALT JJ
000763,000684: # 90 1 RANGE JJ
000764,000685: # 2 RRATE S
000765,000686: # 3 RTHETA H
000766,000687: # 91 1 P21ALT Q (MEMORY/100 TO DIPLAY TENS N.M.)
000767,000688: # 2 P21VEL P
000768,000689: # 3 P21GAM H
000769,000690: # 92 SPARE
000770,000691: # 93 1 OGC G
000771,000692: # 2 OGC +2 G
000772,000693: # 3 OGC +4 G
000773,000694: # 94 SPARE
000774,000695: # 95 SPARE
000775,000696: # 96 SPARE
000776,000697: # 97 1 DSPTEM1 C
000777,000698: # 2 DSPTEM1 +1 C
000778,000699: # 3 DSPTEM1 +2 C
000779,000700: # 98 1 DSPTEM2 C
000780,000701: # 2 DSPTEM2 +1 B
000781,000702: # 3 DSPTEM2 +2 C
000782,000703: # 99 1 WWPOS XX
|
|
Page 17 |
000784,000705: # 2 WWVEL YY
000785,000706: # 3 WWBIAS AAA
|
|
Page 18 |
000787,000708: # NOUN SCALES AND FORMATS
000788,000709:
000789,000710: # -SCALE TYPE- PRECISION
000790,000711: # UNITS DECIMAL FORMAT -- AGC FORMAT
000791,000712: # ------------ -------------- -- ----------
000792,000713:
000793,000714: # -A-
000794,000715: # OCTAL XXXXX SP OCTAL
000795,000716:
000796,000717: # -B- -14
000797,000718: # FRACTIONAL .XXXXX SP BIT 1 = 2 UNITS
000798,000719: # (MAX .99996)
000799,000720:
000800,000721: # -C-
000801,000722: # WHOLE XXXXX. SP BIT 1 = 1 UNIT
000802,000723: # (MAX 16383.)
000803,000724:
000804,000725: # -D- 15
000805,000726: # CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360/2 DEGREES
000806,000727: # (MAX 359.99) (USES 15 BITS FOR MAGNI-
000807,000728: # TUDE AND 2-S COMP.)
000808,000729:
000809,000730: # -E- 14
000810,000731: # ELEVATION DEGREES XX.XXX DEGREES SP BIT 1 = 90/2 DEGREES
000811,000732: # (MAX 89.999)
000812,000733:
000813,000734: # -F- 14
000814,000735: # DEGREES (180) XXX.XX DEGREES SP BIT 1 = 180/2 DEGREES
000815,000736: # (MAX 179.99)
000816,000737:
000817,000738: # -G-
000818,000739: # DP DEGREES (90) XX.XXX DEGREES DP BIT 1 OF LOW REGISTER =
000819,000740: # 28
000820,000741: # 360/2 DEGREES
000821,000742:
000822,000743: # -H-
000823,000744: # DP DEGREES (360) XXX.XX DEGREES DP BIT 1 OF LOW REGISTER =
000824,000745: # 28
000825,000746: # (MAX 359.99) 360/2 DEGREES
000826,000747:
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|
Page 19 |
000828,000749: # -K-
000829,000750: # TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER =
000830,000751: # 000XX. MIN -2
000831,000752: # 0XX.XX SEC 10 SEC
000832,000753: # (DECIMAL ONLY.
000833,000754: # MAX MIN COMP=59
000834,000755: # MAX SEC COMP=59.99
000835,000756: # MAX CAPACITY=745 HRS
000836,000757: # 39 MINS
000837,000758: # 14.55 SECS.
000838,000759: # WHEN LOADING, ALL 3
000839,000760: # COMPONENTS MUST BE
000840,000761: # SUPPLIED.)
000841,000762:
000842,000763: # -L-
000843,000764: # TIME (MIN/SEC) XXBXX MIN/SEC DP BIT 1 OF LOW REGISTER =
000844,000765: # (B IS A BLANK -2
000845,000766: # POSITION, DECIMAL 10 SEC
000846,000767: # ONLY, DISPLAY OR
000847,000768: # MONITOR ONLY. CANNOT
000848,000769: # BE LOADED.
000849,000770: # MAX MIN COMP=59
000850,000771: # MAX SEC COMP=59
000851,000772: # VALUES GREATER THAN
000852,000773: # 59 MIN 59 SEC
000853,000774: # ARE DISPLAYED AS
000854,000775: # 59 MIN 59 SEC.)
000855,000776:
000856,000777: # -M- -2
000857,000778: # TIME (SEC) XXX.XX SEC SP BIT 1 = 10 SEC
000858,000779: # (MAX 163.83)
000859,000780:
000860,000781: # -N-
000861,000782: # TIME(SEC) DP XXX.XX SEC DP BIT 1 OF LOW REGISTER =
000862,000783: # -2
000863,000784: # 10 SEC
000864,000785:
000865,000786: # -P-
000866,000787: # VELOCITY 2 XXXXX. FEET/SEC DP BIT 1 OF HIGH REGISTER =
000867,000788: # (MAX 41994.) -7
000868,000789: # 2 METERS/CENTI-SEC
000869,000790:
000870,000791: # -Q-
000871,000792: # POSITION 4 XXXX.X NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
000872,000793: # 2 METERS
000873,000794:
000874,000795: # -S-
000875,000796: # VELOCITY 3 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
000876,000797: # -7
000877,000798: # 2 METERS/CENTI-SEC
000878,000799:
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|
Page 20 |
000880,000801: # -T- -2
000881,000802: # G XXX.XX G SP BIT 1 = 10 G
000882,000803: # (MAX 163.83)
000883,000804:
000884,000805: # -U-
000885,000806: # RENDEZVOUS XXX.XX NAUT MI DP LOW ORDER BIT OF LOW ORDER
000886,000807: # RADAR RANGE WORD = 9.38 FEET
000887,000808:
000888,000809: # -V-
000889,000810: # RENDEZVOUS XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000890,000811: # RADAR RANGE RATE WORD = -.6278 FEET/SEC
000891,000812:
000892,000813: # -W-
000893,000814: # LANDING RADAR XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000894,000815: # ALTITUDE WORD = 1.079 FEET
000895,000816:
000896,000817: # -X-
000897,000818: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000898,000819: # VELX WORD = -.6440 FEET/SEC
000899,000820:
000900,000821: # -Y-
000901,000822: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000902,000823: # VELY WORD = 1.212 FEET/SEC
000903,000824:
000904,000825: # -Z-
000905,000826: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000906,000827: # VELZ WORD = .8668 FEET/SEC
000907,000828:
000908,000829: # -AA-
000909,000830: # INITIAL/FINAL XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000910,000831: # ALTITUDE WORD = 2.345 FEET
000911,000832:
000912,000833: # -BB-
000913,000834: # ALTITUDE RATE XXXXX. FEET/SEC SP LOW ORDER BIT = .5
000914,000835: # (MAX 08191.) FEET/SEC
000915,000836:
000916,000837: # -CC-
000917,000838: # FORWARD/LATERAL XXXXX. FEET/SEC SP LOW ORDER BIT = .5571
000918,000839: # VELOCITY (MAX 09126.) FEET/SEC
000919,000840:
000920,000841: # -DD-
000921,000842: # ROTATIONAL HAND XXXXX. DEG/SEC SP FRACTIONAL PART OF PI RAD
000922,000843: # CONTROLLER ANGULAR (MAX 00044.) 4 SEC
000923,000844: # RATES
000924,000845:
000925,000846: # -EE-
000926,000847: # OPTICAL TRACKER XXX.XX DEG. DP LOW ORDER BIT OF LOW ORDER
000927,000848: # AZIMUTH ANGLE 15
000928,000849: # WORD = 360/2 DEGREES
000929,000850:
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|
Page 21 |
000931,000852:
000932,000853: # -JJ-
000933,000854: # POSITION5 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
000934,000855: # 2 METERS
000935,000856:
000936,000857: # -KK- 16
000937,000858: # WEIGHT2 XXXXX. LBS SP FRACTIONAL PART OF 2 KG
000938,000859:
000939,000860: # -NN-
000940,000861: # TRIM DEGREES 2 XXX.XX DEG SP BIT 1=.01 SEC(TIME)
000941,000862: # (MAX 032.76)
000942,000863:
000943,000864: # -PP-
000944,000865: # 2 INTEGERS +XXBYY DP BIT 1 OF HIGH REGISTER =
000945,000866: # (B IS A BLANK 1 UNIT OF XX
000946,000867: # POSITION. DECIMAL BIT 1 OF LOW REGISTER =
000947,000868: # ONLY, DISPLAY OR 1 UNIT OF YY
000948,000869: # MONITOR ONLY. CANNOT (EACH REGISTER MUST
000949,000870: # BE LOADED.) CONTAIN A POSITIVE INTEGER
000950,000871: # (MAX 99B99) LESS THAN 100)
000951,000872:
000952,000873: # -QQ-
000953,000874: # POSITION7 XXXX.X NAUT MI DP BIT 1 OF LOW REGISTER =
000954,000875: # (MAX 9058.9) -4
000955,000876: # 2 METERS
000956,000877:
000957,000878: # -RR-
000958,000879: # COMPUTED ALTITUDE XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000959,000880: # -4
000960,000881: # 2 METERS
000961,000882:
000962,000883: # -SS-
000963,000884: # DP DEGREES XXXX.X DEGREES DP BIT 1 OF HIGH REGISTER =
000964,000885: # 1 DEGREE
000965,000886:
000966,000887: # -TT-
000967,000888: # LANDING RADAR +0000X CHANNEL 33, BIT 6 = NOT POSIT. 1
000968,000889: # POSITION (DECIMAL ONLY. CHANNEL 33, BIT 7 = NOT POSIT. 2
000969,000890: # DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
000970,000891: # ONLY. CANNOT BE X = 2 FOR LR POSITION 2
000971,000892: # LOADED.)
000972,000893:
000973,000894: # -WW- 15
000974,000895: # 360-CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360 - (360/2 )
000975,000896: # (MAX 359.99) DEGREES
000976,000897: # (USES 15 BITS FOR MAGNI-
000977,000898: # TUDE AND 2-S COMP.)
000978,000899:
000979,000900: # -XX-
000980,000901: # POSITION 9 XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000981,000902: # -9
000982,000903: # 2 METERS
000983,000904:
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000985,000906:
000986,000907: # -YY-
000987,000908: # VELOCITY 4 XXXX.X FEET/SEC DP FRACTIONAL PART OF
000988,000909: # (MAX 328.0) METERS/CENTI-SEC
000989,000910:
000990,000911: # -AAA-
000991,000912: # RADIANS XX.XXX RADIANS DP BIT 1 OF HIGH REGISTER =
000992,000913: # (MAX 31.999) -9
000993,000914: # 2 RADIANS
000994,000915:
000995,000916:
000996,000917: # THAT-S ALL ON THE NOUNS.
000997,000918:
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000999,000920: # ALARM CODES FOR LUMINARY
001000,000921:
001001,000922: # *9 *18 *60 COLUMN
001002,000923:
001003,000924: # CODE * TYPE SET BY
001004,000925:
001005,000926: # 00105 ** AOTMARK SYSTEM IN USE
001006,000927: # 00107 MORE THAN 5 MARK PAIRS AOTMARK
001007,000928: # 00111 MARK MISSING AOTMARK
001008,000929: # 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
001009,000930: # 00113 NO INBITS AOTMARK
001010,000931: # 00114 MARK MADE BUT NOT DESIRED AOTMARK
001011,000932: # 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
001012,000933: # 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING
001013,000934: # 00206 + GIMBAL LOCK.
001014,000935: # 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
001015,000936: # 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51, P57
001016,000937: # 00211 COARSE ALIGN ERROR IMU MODE SWITCH
001017,000938: # 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH, T4RPT
001018,000939: # 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
001019,000940: # 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
001020,000941: # 00217 BAD RETURN FROM IMUSTALL P51, P52, P57
001021,000942: # 00220 IMU NOT ALIGNED - NO REFSMMAT R02, R47
001022,000943: # 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
001023,000944: # FINDCDUW
001024,000945: # 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
001025,000946: # 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
001026,000947: # 00405 TWO STARS NOT AVAILABLE P52
001027,000948: # 00421 W-MATRIX OVERFLOW INTEGRV
001028,000949: # 00430 ** ACCELERATION OVERFLOW IN INTEGRATION ORBITAL INTEGRATION
001029,000950: # 00501 P RADAR ANTENNA OUT OF LIMITS R23
001030,000951: # 00502 BAD RADAR GIMBAL ANGLE INPUT V41N72
001031,000952: # 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V41N72
001032,000953: # 00510 RADAR AUTO DESCRETE NOT PRESENT R25
001033,000954: # 00511 LR NOT IN POSITION 2 OR REPOSITIONING SERVICER
001034,000955: # 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
001035,000956: # 00515 RR CDU FAIL DISCRETE PRESENT R25
001036,000957: # 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
001037,000958: # 00521 COULD NOT READ RADAR P20
001038,000959: # 00522 LANDING RADAR POSITION CHANGE RADAR READ
001039,000960: # 00523 P LR ANTENNA DIDN'T ACHIEVE POSITION 2 SERVICER, V60 (NON-P IN V60)
001040,000961: # 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
001041,000962: # 00526 P RANGE GREATER THAN 400 NAUT. MILES P20, P22
001042,000963: # 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21, R24
001043,000964: # LUNAR SURFACE
001044,000965: # OR VEHICLE MANEUVER REQUIRED R24 (20)
001045,000966: # 00530 P LOS NOT IN MODE2 COVERAGE R21
001046,000967: # ON LUNAR SURFACE AFTER 600 SECS.
001047,000968: # 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
001048,000969: # 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32, P72,
001049,000970:
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001051,000972:
001052,000973: # 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32, P72,
001053,000974: # 00603 CSI TO CDH TIME LT TMIN12 P32, P72, P33, P73
001054,000975: # 00604 CDH TO TPI TIME LT TMIN23 P32, P72,
001055,000976: # OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
001056,000977: # 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
001057,000978: # 00606 DV EXCEEDS MAXIMUM P32,P72,
001058,000979: # 00607 ** NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET, TIMERAD
001059,000980: # 00611 NO TIG FOR GIVEN ELEV ANGLE P34, P74
001060,000981: # 00701 ILLEGAL OPTION CODE SELECTED P57
001061,000982: # 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
001062,000983: # 01102 AGC SELF TEST ERROR SELF CHECK
001063,000984: # 01103 ** UNUSED CCS BRANCH EXECUTED ABORT
001064,000985: # 01104 * DELAY ROUTINE BUSY EXEC
001065,000986: # 01105 DOWNLINK TOO FAST T4RUPT
001066,000987: # 01106 UPLINK TOO FAST T4RUPT
001067,000988: # 01107 PHASE TABLE FAILURE. ASSUME RESTART
001068,000989: # ERASABLE MEMORY IS SUSPECT. RESTART
001069,000990: # 01201 * EXECUTIVE OVERFLOW - NO VAC AREAS EXEC
001070,000991: # 01202 * EXECUTIVE OVERFLOW - NO CORE SETS EXEC
001071,000992: # 01203 * WAITLIST OVERFLOW - TOO MANY TASKS WAITLIST
001072,000993: # 01204 ** WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
001073,000994: # CALLED WITH ZERO OR NEGATIVE DELTA-TIME
001074,000995: # 01206 ** SECOND JOB ATTEMPTS TO GO TO SLEEP PINBALL
001075,000996: # 01206 VIA KYBD AND DISPLAY PROGRAM
001076,000997: # 01207 * NO VAC AREAS FOR MARKS AOTMARK
001077,000998: # 01210 * TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
001078,000999: # 01211 * ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
001079,001000: # 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
001080,001001: # 01302 ** SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
001081,001002: # 01406 BAD RETURN FROM ROOTPSRS DESCENT GUIDANCE EQS.
001082,001003: # 01406 ** BAD RETURN FROM ROOTPSRS IGNITION ALGORITHM
001083,001004:
001084,001005: # NOTE: 1406 IS A POODOO DURING THE IGNITION ALGORITHM
001085,001006: # AND AN ALARM DURING THE ACTUAL GUIDANCE PHASE.
001086,001007:
001087,001008: # 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
001088,001009: # .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
001089,001010: # VECTOR.) S40.8
001090,001011: # 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
001091,001012: # 01412 DESCENT IGNALG NOT CONVERGING P63
001092,001013: # 01501 ** KEYBOARD AND DISPLAY ALARM DURING PINBALL
001093,001014: # 01501 INTERNAL USE (NVSUB). ABORT
001094,001015: # 01502 ** ILLEGAL FLASHING DISPLAY GOPLAY
001095,001016: # 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
001096,001017: # 01600 OVERFLOW IN DRIFT TEST IMU 4
001097,001018: # 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
001098,001019: # 01601 IMU 4 (LEM)
001099,001020: # 01703 IGNITION TIME SLIPPED MIDTOAVE
001100,001021: # 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
001101,001022: # CONFIGURATION P40, P42
001102,001023:
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001104,001025:
001105,001026: # 02000 * DAP STILL IN PROGRESS AT NEXT TIME5 RUPT DAP
001106,001027: # 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
001107,001028: # 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
001108,001029: # 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
001109,001030: # 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
001110,001031: # 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
001111,001032: # 04777 ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001112,001033: # 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
001113,001034: # 10777 IMU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001114,001035: # 13777 IMU, ICDU FAILS CAUSED THE ISS WARNING T4RUPT
001115,001036: # 14777 IMU, ICDU, PIPA FAILS CAUSED THE ISSWNING T4RUPT
001116,001037:
001117,001038: # * INDICATES AN ABORT CODE THAT RESULTS IN A SOFTWARE RESTART.
001118,001039:
001119,001040: # ** INDICATES A MORE SERIOUS ABORT CODE THAT RESULTS IN THE
001120,001041: # PROGRAM GOING TO R00.
001121,001042:
001122,001043: # P INDICATES A PRIORITY ALARM.
001123,001044:
001124,001045: # ALL OTHERS ARE NON-ABORTIVE
001125,001046:
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001127,001048:
001128,001049: # CHECKLIST CODES FOR LUMINARY
001129,001050:
001130,001051: # *9 *17 *26 *9 COLUMN
001131,001052:
001132,001053: # R1CODE ACTION TO BE EFFECTED PROGRAM
001133,001054:
001134,001055: # 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
001135,001056: # 00014 PROCEED DO IMU FINE ALIGN ROUTINE P51, P63, P57
001136,001057: # 00014 ENTER DO LANDING SITE DETERMINATION (N89DISP) P57OPTION2
001137,001058: # 00015 PERFORM CELESTIAL BODY ACQUISITION R51, P51
001138,001059: # 00062 SWITCH AGC POWER DOWN P06
001139,001060: # 00201 SWITCH RR MODE TO AUTOMATIC P20, P22, R04
001140,001061: # 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12, P42, P71
001141,001062: # ALSO THR CONT TO AUTO P40, P63, P70
001142,001063: # 00205 PERFORM MANUAL ACQUISITION OF RR R23
001143,001064: # 00500 SWITCH LR ANTENNA TO POSITION 1 P63
001144,001065:
001145,001066: # SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
001146,001067: # PERFORM DENOTES START OR END OF A TASK
001147,001068: # KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
001148,001069:
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001150,001071: # OPTION CODES FOR LUMINARY
001151,001072:
001152,001073: # THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
001153,001074: # CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
001154,001075: # ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
001155,001076:
001156,001077: # *9 *17 *52 *11 *25 COLUMN
001157,001078:
001158,001079: # OPTION
001159,001080: # CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
001160,001081:
001161,001082: # 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
001162,001083: # 4=LAND SITE
001163,001084: # 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
001164,001085: # 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
001165,001086: # 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
001166,001087: # 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
001167,001088: # 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
001168,001089: # 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
001169,001090: # 2=TWO BODIES 3=ONE BODY + G
001170,001091: # 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
001171,001092: # ORBIT TO PASS OVER LM
001172,001093:
End of include-file ASSEMBLY_AND_OPERATION_INFORMATION.agc. Parent file is MAIN.agc