GAP: ASSEMBLE REVISION 001 OF AGC PROGRAM LMY99 BY NASA 2021112-061 16:27 JULY 14,1969Note that the date is the date of the printout, not the date of the program revision.
Source Code
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These source-code files were from the printout at the MIT Museum, with many thanks
to Deborah Douglas, the Museum's Curator of Science and Technology, for releasing
it to us. The printout was digitally photographed by Paul Fjeld. A team of
volunteers transcribed the source code manually from these images or, where
appropriate, modified already-transcribed but similar source Luminary 131 (Apollo 13)
source code to agree with the images from the printout. Note that the page images
presented online are of reduced quality, and that higher-quality images
are available. Report any conversion errors or legibility
problems in page images to info@sandroid.org.
Notations on the program listing read, in part:GAP: ASSEMBLE REVISION 001 OF AGC PROGRAM LMY99 BY NASA 2021112-061 16:27 JULY 14,1969Note that the date is the date of the printout, not the date of the program revision. |
000081,000002: ## Copyright: Public domain.
000082,000003: ## Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
000083,000004: ## Purpose: Part of the source code for Luminary 1A build 099.
000084,000005: ## It is part of the source code for the Lunar Module's (LM)
000085,000006: ## Apollo Guidance Computer (AGC), for Apollo 11.
000086,000007: ##
000087,000008: ## Assembler: yaYUL
000088,000009: ## Contact: Jim Lawton <jim.lawton@gmail.com>
000089,000010: ## Website: www.ibiblio.org/apollo.
000090,000011: ## Pages: 001-027
000091,000012: ## Mod history: 2009-05-16 JVL Transcribed from page images.
000092,000013: ## 2016-12-11 RSB Proofed text comments with octopus/ProoferComments
000093,000014: ## and corrected the errors found.
000094,000015: ## 2017-01-04 MAS A few typos found during Luminary 69 transcription.
000095,000016: ## 2017-01-25 RSB Back-ported a typo-fix found while proofing Luminary 69.
000096,000017: ## 2017-03-14 RSB Comment-text fixes identified in 5-way
000097,000018: ## side-by-side diff of Luminary 69/99/116/131/210.
000098,000019: ## 2017-08-01 MAS Removed an asterisk indicating a changed line that
000099,000020: ## was incorrectly included as part of a comment.
000100,000021:
000101,000022: ## This source code has been transcribed or otherwise adapted from digitized
000102,000023: ## images of a hardcopy from the MIT Museum. The digitization was performed
000103,000024: ## by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many
000104,000025: ## thanks to both. The images (with suitable reduction in storage size and
000105,000026: ## consequent reduction in image quality as well) are available online at
000106,000027: ## www.ibiblio.org/apollo. If for some reason you find that the images are
000107,000028: ## illegible, contact me at info@sandroid.org about getting access to the
000108,000029: ## (much) higher-quality images which Paul actually created.
000109,000030: ##
000110,000031: ## Notations on the hardcopy document read, in part:
000111,000032: ##
000112,000033: ## Assemble revision 001 of AGC program LMY99 by NASA 2021112-061
000113,000034: ## 16:27 JULY 14, 1969
000114,000035:
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Page 1 |
000116,000037:
000117,000038: # THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
000118,000039: # THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
000119,000040:
000120,000041: # GUIDANCE SYSTEM OPERATIONS PLAN
000121,000042: # FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
000122,000043: # USING PROGRAM LUMINARY
000123,000044:
000124,000045: # THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
000125,000046: # TECHNOLOGY 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS UNDER PROJECT 55-238-70, SPONSORED BY THE MANNED
000126,000047: # SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065.
000127,000048:
000128,000049: # THIS PROGRAM IS REFERRED TO AS LUMINARY 1A
000129,000050:
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Page 2 |
000131,000052:
000132,000053: # TABLE OF LOG CARDS
000133,000054: # ASSEMBLY AND OPERATION INFORMATION
000134,000055: # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
000135,000056: # CONTROLLED CONSTANTS
000136,000057: # INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
000137,000058: # FLAGWORD ASSIGNMENTS
000138,000059: # SUBROUTINE CALLS
000139,000060:
000140,000061: # TABLE OF SUBROUTINE LOG SECTIONS
000141,000062: # LUMERASE
000142,000063: # ERASABLE ASSIGNMENTS
000143,000064: # LNYAIDE
000144,000065: # INTERRUPT LEAD INS
000145,000066: # T4RUPT PROGRAM
000146,000067: # RCS FAILURE MONITOR
000147,000068: # DOWNLINK LISTS
000148,000069: # AGS INITIALIZATION
000149,000070: # FRESH START AND RESTART
000150,000071: # RESTART TABLES
000151,000072: # AOTMARK
000152,000073: # EXTENDED VERBS
000153,000074: # PINBALL NOUN TABLES
000154,000075: # LEM GEOMETRY
000155,000076: # IMU COMPENSATION PACKAGE
000156,000077: # R63
000157,000078: # ATTITUDE MANEUVER ROUTINE
000158,000079: # GIMBAL LOCK AVOIDANCE
000159,000080: # KALCMANU STEERING
000160,000081: # SYSTEM TEST STANDARD LEAD INS
000161,000082: # IMU PERFORMANCE TESTS 2
000162,000083: # IMU PERFORMANCE TESTS 4
000163,000084: # PINBALL GAMES BUTTONS AND LIGHTS
000164,000085: # R60,R62
000165,000086: # S-BAND ANTENNA FOR LM
000166,000087: # LEMP20S
000167,000088: # RADAR LEADIN ROUTINES
000168,000089: # P20-P25
000169,000090: # LEMP30S
000170,000091: # P30,P37
000171,000092: # P32-P35, P72-P75
000172,000093: # GENERAL LAMBERT AIMPOINT GUIDANCE
000173,000094: # KISSING
000174,000095: # GROUND TRACKING DETERMINATION PROGRAM - P21
000175,000096: # P34-P35, P74-P75
000176,000097: # R31
000177,000098: # P76
000178,000099: # R30
000179,000100: # STABLE ORBIT - P38-P39
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Page 3 |
000181,000102: # FLY
000182,000103: # BURN, BABY, BURN -- MASTER IGNITION ROUTINE
000183,000104: # P40-P47
000184,000105: # THE LUNAR LANDING
000185,000106: # THROTTLE CONTROL ROUTINES
000186,000107: # LUNAR LANDING GUIDANCE EQUATIONS
000187,000108: # P70-P71
000188,000109: # P12
000189,000110: # ASCENT GUIDANCE
000190,000111: # SERVICER
000191,000112: # LANDING ANALOG DISPLAYS
000192,000113: # FINDCDUW - GUIDAP INTERFACE
000193,000114: # LEMP50S
000194,000115: # P51-P53
000195,000116: # LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
000196,000117: # SKIPPER
000197,000118: # DOWN-TELEMETRY PROGRAM
000198,000119: # INTER-BANK COMMUNICATION
000199,000120: # INTERPRETER
000200,000121: # FIXED-FIXED CONSTANT POOL
000201,000122: # INTERPRETIVE CONSTANTS
000202,000123: # SINGLE PRECISION SUBROUTINES
000203,000124: # EXECUTIVE
000204,000125: # WAITLIST
000205,000126: # LATITUDE LONGITUDE SUBROUTINES
000206,000127: # PLANETARY INERTIAL ORIENTATION
000207,000128: # MEASUREMENT INCORPORATION
000208,000129: # CONIC SUBROUTINES
000209,000130: # INTEGRATION INITIALIZATION
000210,000131: # ORBITAL INTEGRATION
000211,000132: # INFLIGHT ALIGNMENT ROUTINES
000212,000133: # POWERED FLIGHT SUBROUTINES
000213,000134: # TIME OF FREE FALL
000214,000135: # AGC BLOCK TWO SELF-CHECK
000215,000136: # PHASE TABLE MAINTENANCE
000216,000137: # RESTARTS ROUTINE
000217,000138: # IMU MODE SWITCHING ROUTINES
000218,000139: # KEYRUPT, UPRUPT
000219,000140: # DISPLAY INTERFACE ROUTINES
000220,000141: # SERVICE ROUTINES
000221,000142: # ALARM AND ABORT
000222,000143: # UPDATE PROGRAM
000223,000144: # RTB OP CODES
000224,000145: # LMDAP
000225,000146: # T6-RUPT PROGRAMS
000226,000147: # DAP INTERFACE SUBROUTINES
000227,000148: # DAPIDLER PROGRAM
000228,000149: # P-AXIS RCS AUTOPILOT
000229,000150: # Q,R-AXIS RCS AUTOPILOT
000230,000151: # TJET LAW
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Page 4 |
000232,000153: # KALMAN FILTER
000233,000154: # TRIM GIMBAL CONTROL SYSTEM
000234,000155: # AOSTASK AND AOSJOB
000235,000156: # SPS BACK-UP RCS CONTROL
000236,000157:
000237,000158: # SYMBOL TABLE LISTING
000238,000159: # UNREFERENCED SYMBOL LISTING
000239,000160: # ERASABLE & EQUALS CROSS-REFERENCE TABLE
000240,000161: # SUMMARY OF SYMBOL TABLE LISTINGS
000241,000162: # MEMORY TYPE & AVAILABLITY DISPLAY
000242,000163: # COUNT TABLE
000243,000164: # PARAGRAPHS GENERATED FOR THIS ASSEMBLY
000244,000165: # OCTAL LISTING
000245,000166: # OCCUPIED LOCATIONS TABLE
000246,000167: # SUBROS CALLED & PROGRAM STATUS
000247,000168:
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Page 5 |
000249,000170: # VERB LIST FOR LUMINARY
000250,000171:
000251,000172: # REGULAR VERBS
000252,000173:
000253,000174: # 00 NOT IN USE
000254,000175: # 01 DISPLAY OCTAL COMP 1 IN R1
000255,000176: # 02 DISPLAY OCTAL COMP 2 IN R1
000256,000177: # 03 DISPLAY OCTAL COMP 3 IN R1
000257,000178: # 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
000258,000179: # 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
000259,000180: # 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000260,000181: # 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
000261,000182: # 08
000262,000183: # 09
000263,000184: # 10
000264,000185: # 11 MONITOR OCTAL COMP 1 IN R1
000265,000186: # 12 MONITOR OCTAL COMP 2 IN R1
000266,000187: # 13 MONITOR OCTAL COMP 3 IN R1
000267,000188: # 14 MONITOR OCTAL COMP 1,2 IN R1,R2
000268,000189: # 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
000269,000190: # 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000270,000191: # 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
000271,000192: # 18
000272,000193: # 19
000273,000194: # 20
000274,000195: # 21 LOAD COMPONENT 1 INTO R1
000275,000196: # 22 LOAD COMPONENT 2 INTO R2
000276,000197: # 23 LOAD COMPONENT 3 INTO R3
000277,000198: # 24 LOAD COMPONENT 1,2 INTO R1,R2
000278,000199: # 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
000279,000200: # 26
000280,000201: # 27 DISPLAY FIXED MEMORY
000281,000202: # 28
000282,000203: # 29
000283,000204: # 30 REQUEST EXECUTIVE
000284,000205: # 31 REQUEST WAITLIST
000285,000206: # 32 RECYCLE PROGRAM
000286,000207: # 33 PROCEED WITHOUT DSKY INPUTS
000287,000208: # 34 TERMINATE FUNCTION
000288,000209: # 35 TEST LIGHTS
000289,000210: # 36 REQUEST FRESH START
000290,000211: # 37 CHANGE PROGRAM (MAJOR MODE)
000291,000212: # 38
000292,000213: # 39
000293,000214:
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Page 6 |
000295,000216: # EXTENDED VERBS
000296,000217:
000297,000218: # 40 ZERO CDU-S
000298,000219: # 41 COARSE ALIGN CDU-S
000299,000220: # 42 FINE ALIGN IMU
000300,000221: # 43 LOAD IMU ATT ERROR METERS
000301,000222: # 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
000302,000223: # 45
000303,000224: # 46
000304,000225: # 47 INITIALIZE AGS (R47)
000305,000226: # 48 REQUEST DAP DATA LOAD ROUTINE (R03)
000306,000227: # 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
000307,000228: # 50 PLEASE PERFORM
000308,000229: # 51
000309,000230: # 52 MARK X-RETICLE
000310,000231: # 53 MARK Y-RETICLE
000311,000232: # 54 MARK X OR Y-RETICLE
000312,000233: # 55 INCREMENT AGC TIME (DECIMAL)
000313,000234: # 56 TERMINATE TRACKING (P20 + P25)
000314,000235: # 57 PERMIT LANDING RADAR UPDATES
000315,000236: # 58 INHIBIT LANDING RADAR UPDATES
000316,000237: # 59
000317,000238: # 60 COMMAND LR TO POSITION 2.
000318,000239: # 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
000319,000240: # 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
000320,000241: # 63 SAMPLE RADAR ONCE PER SECOND (R04).
000321,000242: # 64 REQUEST S-BAND ANTENNA ROUTINE (R05)
000322,000243: # 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
000323,000244: # 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
000324,000245: # 67 DISPLAY W MATRIX
000325,000246: # 68
000326,000247: # 69 CAUSE RESTART
000327,000248: # 70 UPDATE LIFTOFF TIME
000328,000249: # 71 UNIVERSAL UPDATE-BLOCK ADR
000329,000250: # 72 UNIVERSAL UPDATE-SINGLE ADR
000330,000251: # 73 UPDATE AGC TIME (OCTAL)
000331,000252: # 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
000332,000253: # 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
000333,000254: # 76 MINIMUM IMPULSE COMMAND MODE
000334,000255: # 77 RATE COMMAND AND ATTITUDE HOLD MODE
000335,000256: # 78 LR SPURIOUS RETURN TEST START (R77)
000336,000257: # 79 LR SPURIOUS RETURN TEST STOP
000337,000258: # 80 UPDATE LEM STATE VECTOR
000338,000259: # 81 UPDATE CSM STATE VECTOR
000339,000260: # 82 REQUEST ORBIT PARAM DISPLAY (R30)
000340,000261: # 83 REQUEST REND PARAM DISPLAY (R31)
000341,000262: # 84
000342,000263: # 85 DISPLAY RR LOS AZ AND ELEV
000343,000264: # 86
000344,000265: # 87
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000346,000267: # 88
000347,000268: # 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
000348,000269: # 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
000349,000270: # 91 DISPLAY BANK SUM
000350,000271: # 92 OPERATE IMU PERFORMANCE TEST (P07)
000351,000272: # 93 ENABLE W MATRIX INITIALIZATION
000352,000273: # 94
000353,000274: # 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
000354,000275: # 96 INTERRUPT INTEGRATION AND GO TO POO
000355,000276: # 97 PERFORM ENGINE FAIL PROCEDURE
000356,000277: # 98
000357,000278: # 99 PLEASE ENABLE ENGINE
000358,000279:
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000360,000281: # IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
000361,000282: # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
000362,000283: # SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
000363,000284: # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23
000364,000285: # MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
000365,000286: # ABOVE SCALE TYPES.
000366,000287:
000367,000288: # THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
000368,000289: # EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
000369,000290:
000370,000291: # NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000371,000292: # 00 NOT IN USE
000372,000293: # 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH
000373,000294: # 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH
000374,000295: # 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP XXX.XX DEG FOR EACH
000375,000296: # 04 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000376,000297: # 05 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000377,000298: # 06 OPTION CODE 3COMP OCTAL ONLY FOR EACH
000378,000299: # LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
000379,000300: # 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
000380,000301: # ONES FOR BITS TO BE MODIFIED
000381,000302: # 1 TO SET OR 0 TO RESET SELECTED BITS
000382,000303: # 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
000383,000304: # 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
000384,000305: # 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
000385,000306: # 11 TIG OF CSI 3COMP 00XXX. HRS DEC ONLY
000386,000307: # 000XX. MIN MUST LOAD 3 COMPS
000387,000308: # 0XX.XX SEC
000388,000309: # 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
000389,000310: # (USED BY EXTENDED VERBS ONLY)
000390,000311: # 13 TIG OF CDH 3COMP 00XXX. HRS DEC ONLY
000391,000312: # 000XX. MIN MUST LOAD 3 COMPS
000392,000313: # 0XX.XX SEC
000393,000314: # 14 CHECKLIST 3COMP XXXXX. FOR EACH
000394,000315: # (USED BY EXTENDED VERBS ONLY)
000395,000316: # (NOUN 25 IS PASTED AFTER DISPLAY)
000396,000317: # 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
000397,000318: # 16 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000398,000319: # (USED BY EXTENDED VERBS ONLY) 000XX. MIN MUST LOAD 3 COMPS
000399,000320: # 0XX.XX SEC
000400,000321: # 17 SPARE
000401,000322: # 18 AUTO MANEUVER BALL ANGLES 3COMP XXX.XX DEG FOR EACH
000402,000323: # 19 SPARE
000403,000324: # 20 ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000404,000325: # 21 PIPAS 3COMP XXXXX. PULSES FOR EACH
000405,000326: # 22 NEW ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000406,000327: # 23 SPARE
000407,000328: # 24 DELTA TIME FOR AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000408,000329: # 000XX. MIN MUST LOAD 3 COMPS
000409,000330: # 0XX.XX SEC
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000411,000332: # 25 CHECKLIST 3COMP XXXXX. FOR EACH
000412,000333: # (USED WITH PLEASE PERFORM ONLY)
000413,000334: # 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
000414,000335: # 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX.
000415,000336: # 28 SPARE
000416,000337: # 29 SPARE
000417,000338: # 30 SPARE
000418,000339: # 31 SPARE
000419,000340: # 32 TIME FROM PERIGEE 3COMP 00XXX. HRS DEC ONLY
000420,000341: # 000XX. MIN MUST LOAD 3 COMPS
000421,000342: # 0XX.XX SEC
000422,000343: # 33 TIME OF IGNITION 3COMP 00XXX. HRS DEC ONLY
000423,000344: # 000XX. MIN MUST LOAD 3 COMPS
000424,000345: # 0XX.XX SEC
000425,000346: # 34 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000426,000347: # 000XX. MIN MUST LOAD 3 COMPS
000427,000348: # 0XX.XX SEC
000428,000349: # 35 TIME FROM EVENT 3COMP 00XXX. HRS DEC ONLY
000429,000350: # 000XX. MIN MUST LOAD 3 COMPS
000430,000351: # 0XX.XX SEC
000431,000352: # 36 TIME OF AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000432,000353: # 000XX. MIN MUST LOAD 3 COMPS
000433,000354: # 0XX.XX SEC
000434,000355: # 37 TIG OF TPI 3COMP 00XXX. HRS DEC ONLY
000435,000356: # 000XX. MIN MUST LOAD 3 COMPS
000436,000357: # 0XX.XX SEC
000437,000358: # 38 TIME OF STATE BEING INTEGRATED 3COMP 00XXX. HRS DEC ONLY
000438,000359: # 000XX. MIN MUST LOAD 3 COMPS
000439,000360: # 0XX.XX SEC
000440,000361: # 39 SPARE
000441,000362:
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Page 10 |
000443,000364: # MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000444,000365: # 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000445,000366: # VG, XXXX.X FT/SEC
000446,000367: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000447,000368: # 41 TARGET AZIMUTH, 2COMP XXX.XX DEG (FOR SYSTEM TEST)
000448,000369: # ELEVATION XX.XXX DEG
000449,000370: # 42 APOGEE, 3COMP XXXX.X NAUT MI DEC ONLY
000450,000371: # PERIGEE, XXXX.X NAUT MI
000451,000372: # DELTA V (REQUIRED) XXXX.X FT/SEC
000452,000373: # 43 LATITUDE, 3COMP XXX.XX DEG DEC ONLY
000453,000374: # LONGITUDE, XXX.XX DEG
000454,000375: # ALTITUDE XXXX.X NAUT MI
000455,000376: # 44 APOGEE, 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000456,000377: # PERIGEE, XXXX.X NAUT MI
000457,000378: # TFF XXBXX MIN/SEC
000458,000379: # 45 MARKS, 3COMP XXXXX. NO LOAD, DEC ONLY
000459,000380: # TFI OF NEXT BURN XXBXX MIN/SEC
000460,000381: # MGA XXX.XX DEG
000461,000382: # 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
000462,000383: # 47 LEM WEIGHT, 2COMP XXXXX. LBS DEC ONLY
000463,000384: # CSM WEIGHT XXXXX. LBS
000464,000385: # 48 GIMBAL PITCH TRIM, 2COMP XXX.XX DEG DEC ONLY
000465,000386: # GIMBAL ROLL TRIM XXX.XX DEG
000466,000387: # 49 DELTA R, 3COMP XXXX.X NAUT MI DEC ONLY
000467,000388: # DELTA V, XXXX.X FT/SEC
000468,000389: # RADAR DATA SOURCE CODE XXXXX.
000469,000390: # 50 SPARE
000470,000391: # 51 S-BAND ANTENNA ANGLES PITCH 2COMP XXX.XX DEG DEC ONLY
000471,000392: # YAW XXX.XX DEG
000472,000393: # 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG
000473,000394: # 53 SPARE
000474,000395: # 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
000475,000396: # RANGE RATE, XXXX.X FT/SEC
000476,000397: # THETA XXX.XX DEG
000477,000398: # 55 NO. OF APSIDAL CROSSINGS 3COMP XXXXX. DEC ONLY
000478,000399: # ELEVATION ANGLE XXX.XX DEG
000479,000400: # CENTRAL ANGLE OF PASSIVE VEHICLE XXX.XX DEG
000480,000401: # 56 RR LOS AZIMUTH 2COMP XXX.XX DEG
000481,000402: # ELEVATION XXX.XX DEG
000482,000403: # 57 DELTA R 1COMP XXXX.X NAUT MI DEC ONLY
000483,000404: # 58 PERIGEE ALT (POST TPI) 3COMP XXXX.X NAUT MI DEC ONLY
000484,000405: # DELTA V TPI XXXX.X FT/SEC
000485,000406: # DELTA V TPF XXXX.X FT/SEC
000486,000407: # 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY
000487,000408: # 60 HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000488,000409: # ALTITUDE RATE XXXX.X FT/SEC
000489,000410: # COMPUTED ALTITUDE XXXXX. FEET
000490,000411: # 61 TIME TO GO IN BRAKING PHASE 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000491,000412: # TIME FROM IGNITION XXBXX MIN/SEC
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000493,000414: # CROSS RANGE DISTANCE XXXX.X NAUT MI
000494,000415: # 62 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC NO LOAD, DEC ONLY
000495,000416: # TIME FROM IGNITION XXBXX MIN/SEC
000496,000417: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000497,000418: # 63 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000498,000419: # ALTITUDE RATE XXXX.X FT/SEC
000499,000420: # COMPUTED ALTITUDE XXXXX. FEET
000500,000421: # 64 TIME LEFT FOR REDESIGNATION- LPD ANGLE 3COMP XXBXX NO LOAD, DEC ONLY
000501,000422: # ALTITUDE RATE XXXX.X FT/SEC
000502,000423: # COMPUTED ALTITUDE XXXXX. FEET
000503,000424: # 65 SAMPLED AGC TIME 3COMP 00XXX. HRS DEC ONLY
000504,000425: # (FETCHED IN INTERRUPT) 000XX. MIN MUST LOAD 3 COMPS
000505,000426: # 0XX.XX SEC
000506,000427: # 66 LR RANGE 2COMP XXXXX. FEET NO LOAD, DEC ONLY
000507,000428: # POSITION +0000X
000508,000429: # 67 LRVX 3COMP XXXXX. FT/SEC
000509,000430: # LRVY XXXXX. FT/SEC
000510,000431: # LRVZ XXXXX. FT/SEC
000511,000432: # 68 SLANT RANGE TO LANDING SITE 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000512,000433: # TIME TO GO IN BRAKING PHASE XXBXX MIN/SEC
000513,000434: # LR ALTITUDE - COMPUTED ALTITUDE XXXXX. FEET
000514,000435: # 69 SPARE
000515,000436: # 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000516,000437: # 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000517,000438: # 72 RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000518,000439: # SHAFT ANGLE XXX.XX DEG
000519,000440: # 73 NEW RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000520,000441: # SHAFT ANGLE XXX.XX DEG
000521,000442: # 74 TIME FROM IGNITION 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000522,000443: # YAW AFTER VEHICLE RISE XXX.XX DEG
000523,000444: # PITCH AFTER VEHICLE RISE XXX.XX DEG
000524,000445: # 75 DELTA ALTITUDE CDH 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000525,000446: # DELTA TIME (CDH-CSI OR TPI-CDH) XXBXX MIN/SEC
000526,000447: # DELTA TIME (TPI-CDH OR TPI-NOMTPI) XXBXX MIN/SEC
000527,000448: # 76 DESIRED HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000528,000449: # DESIRED RADIAL VELOCITY XXXX.X FT/SEC
000529,000450: # CROSS-RANGE DISTANCE XXXX.X NAUT MI
000530,000451: # 77 TIME TO ENGINE CUTOFF 2COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000531,000452: # VELOCITY NORMAL TO CSM PLANE XXXX.X FT/SEC
000532,000453: # 78 RR RANGE 2COMP XXX.XX NAUT MI
000533,000454: # RANGE RATE XXXXX. FT/SEC
000534,000455: # 79 CURSOR ANGLE 3COMP XXX.XX DEG DEC ONLY
000535,000456: # SPIRAL ANGLE XXX.XX DEG
000536,000457: # POSITION CODE XXXXX.
000537,000458: # 80 DATA INDICATOR, 2COMP XXXXX.
000538,000459: # OMEGA XXX.XX DEG
000539,000460: # 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
|
|
Page 12 |
000541,000462: # 82 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000542,000463: # 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000543,000464: # 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000544,000465: # 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000545,000466: # 86 VG (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000546,000467: # 87 BACKUP OPTICS LOS AZIMUTH 2COMP XXX.XX DEG
000547,000468: # ELEVATION XXX.XX DEG
000548,000469: # 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY
000549,000470: # 89 LANDMARK LATITUDE 3COMP XX.XXX DEG DEC ONLY
000550,000471: # LONGITUDE/2 XX.XXX DEC
000551,000472: # ALTITUDE XXX.XX NAUT MI
000552,000473: # 90 Y 3COMP XXX.XX NM DEC ONLY
000553,000474: # Y DOT XXXX.X FPS
000554,000475: # PSI XXX.XX DEG
000555,000476: # 91 ALTITUDE 3COMP XXXXXB. NAUT MI
000556,000477: # VELOCITY XXXXX. FT/SEC
000557,000478: # FLIGHT PATH ANGLE XXX.XX DEG
000558,000479: # 92 SPARE
000559,000480: # 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
000560,000481: # 94 SPARE
000561,000482: # 95 SPARE
000562,000483: # 96 SPARE
000563,000484: # 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH
000564,000485: # 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX.
000565,000486: # .XXXXX
000566,000487: # XXXXX.
000567,000488: # 99 RMS IN POSITION 3COMP XXXXX. FT DEC ONLY
000568,000489: # RMS IN VELOCITY XXXX.X FT/SEC
000569,000490: # RMS IN BIAS XX.XXX RADIANS
000570,000491:
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Page 13 |
000572,000493: # REGISTERS AND SCALING FOR NORMAL NOUNS
000573,000494:
000574,000495: # NOUN REGISTER SCALE TYPE
000575,000496: # 00 NOT IN USE
000576,000497: # 01 SPECIFY ADDRESS B
000577,000498: # 02 SPECIFY ADDRESS C
000578,000499: # 03 SPECIFY ADDRESS D
000579,000500: # 04 DSPTEM1 H
000580,000501: # 05 DSPTEM1 H
000581,000502: # 06 OPTION1 A
000582,000503: # 07 XREG A
000583,000504: # 08 ALMCADR A
000584,000505: # 09 FAILREG A
000585,000506: # 10 SPECIFY CHANNEL A
000586,000507: # 11 TCSI K
000587,000508: # 12 OPTIONX A
000588,000509: # 13 TCDH K
000589,000510: # 14 DSPTEMX C
000590,000511: # 15 INCREMENT ADDRESS A
000591,000512: # 16 DSPTEMX C
000592,000513: # 17 SPARE
000593,000514: # 18 FDAIX D
000594,000515: # 19 SPARE
000595,000516: # 20 CDUX D
000596,000517: # 21 PIPAX C
000597,000518: # 22 THETAD D
000598,000519: # 23 SPARE
000599,000520: # 24 DSPTEM2 +1 K
000600,000521: # 25 DSPTEM1 C
000601,000522: # 26 DSPTEM1 A
000602,000523: # 27 SMODE C
000603,000524: # 28 SPARE
000604,000525: # 29 SPARE
000605,000526: # 30 SPARE
000606,000527: # 31 SPARE
000607,000528: # 32 -TPER K
000608,000529: # 33 TIG K
000609,000530: # 34 DSPTEM1 K
000610,000531: # 35 TTOGO K
000611,000532: # 36 TIME2 K
000612,000533: # 37 TTPI K
000613,000534: # 38 TET K
000614,000535: # 39 SPARE
000615,000536:
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|
Page 14 |
000617,000538: # REGISTERS AND SCALING FOR MIXED NOUNS
000618,000539:
000619,000540: # NOUN COMP REGISTER SCALE TYPE
000620,000541: # 40 1 TTOGO L
000621,000542: # 2 VGDISP S
000622,000543: # 3 DVTOTAL S
000623,000544: # 41 1 DSPTEM1 D
000624,000545: # 2 DSPTEM1 +1 E
000625,000546: # 42 1 HAPO Q
000626,000547: # 2 HPER Q
000627,000548: # 3 VGDISP S
000628,000549: # 43 1 LAT H
000629,000550: # 2 LONG H
000630,000551: # 3 ALT Q
000631,000552: # 44 1 HAPOX Q
000632,000553: # 2 HPERX Q
000633,000554: # 3 TFF L
000634,000555: # 45 1 TRKMKCNT C
000635,000556: # 2 TTOGO L
000636,000557: # 3 +MGA H
000637,000558: # 46 1 DAPDATR1 A
000638,000559: # 47 1 LEMMASS KK
000639,000560: # 2 CSMMASS KK
000640,000561: # 48 1 PITTIME NN
000641,000562: # 2 ROLLTIME NN
000642,000563: # 49 1 R22DISP Q
000643,000564: # 2 R22DISP +2 S
000644,000565: # 3 WHCHREAD C
000645,000566: # 50 SPARE
000646,000567: # 51 1 ALPHASB H
000647,000568: # 2 BETASB H
000648,000569: # 52 1 ACTCENT H
000649,000570: # 53 SPARE
000650,000571: # 54 1 RANGE JJ
000651,000572: # 2 RRATE S
000652,000573: # 3 RTHETA H
000653,000574: # 55 1 NN C
000654,000575: # 2 ELEV H
000655,000576: # 3 CENTANG H
000656,000577: # 56 1 RR-AZ H
000657,000578: # 2 RR-ELEV H
000658,000579: # 57 1 DELTAR Q
000659,000580: # 58 1 POSTTPI Q
000660,000581: # 2 DELVTPI S
000661,000582: # 3 DELVTPF S
000662,000583: # 59 1 DVLOS S
000663,000584: # 2 DVLOS +2 S
000664,000585: # 3 DVLOS +4 S
000665,000586: # 60 1 VHORIZ S
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|
Page 15 |
000667,000588: # 2 HDOTDISP S
000668,000589: # 3 HCALC RR
000669,000590: # 61 1 TTFDISP L
000670,000591: # 2 TTOGO L
000671,000592: # 3 OUTOFPLN QQ
000672,000593: # 62 1 ABVEL S
000673,000594: # 2 TTOGO L
000674,000595: # 3 DVTOTAL S
000675,000596: # 63 1 ABVEL S
000676,000597: # 2 HDOTDISP S
000677,000598: # 3 HCALC1 RR
000678,000599: # 64 1 FUNNYDSP PP
000679,000600: # 2 HDOTDISP S
000680,000601: # 3 HCALC RR
000681,000602: # 65 1 SAMPTIME K
000682,000603: # 2 SAMPTIME K
000683,000604: # 3 SAMPTIME K
000684,000605: # 66 1 RSTACK +6 W
000685,000606: # 2 CHANNEL 33 TT
000686,000607: # 67 1 RSTACK X
000687,000608: # 2 RSTACK +2 Y
000688,000609: # 3 RSTACK +4 Z
000689,000610: # 68 1 RANGEDSP QQ
000690,000611: # 2 TTFDISP L
000691,000612: # 3 DELTAH RR
000692,000613: # 69 SPARE
000693,000614: # 70 1 AOTCODE A
000694,000615: # 2 AOTCODE +1 A
000695,000616: # 3 AOTCODE +2 A
000696,000617: # 71 1 AOTCODE A
000697,000618: # 2 AOTCODE +1 A
000698,000619: # 3 AOTCODE +2 A
000699,000620: # 72 1 CDUT WW
000700,000621: # 2 CDUS D
000701,000622: # 73 1 TANG WW
000702,000623: # 2 TANG +1 D
000703,000624: # 74 1 TTOGO L
000704,000625: # 2 YAW H
000705,000626: # 3 PITCH H
000706,000627: # 75 1 DIFFALT Q
000707,000628: # 2 T1TOT2 L
000708,000629: # 3 T2TOT3 L
000709,000630: # 76 1 ZDOTD S
000710,000631: # 2 RDOTD S
000711,000632: # 3 XRANGE Q
000712,000633: # 77 1 TTOGO L
000713,000634: # 2 YDOT S
000714,000635: # 78 1 RSTACK U
000715,000636: # 2 RSTACK +2 V
000716,000637: # 79 1 CURSOR D
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|
Page 16 |
000718,000639: # 2 SPIRAL D
000719,000640: # 3 POSCODE C
000720,000641: # 80 1 DATAGOOD C
000721,000642: # 2 OMEGAD H
000722,000643: # 81 1 DELVLVC S
000723,000644: # 2 DELVLVC +2 S
000724,000645: # 3 DELVLVC +4 S
000725,000646: # 82 1 DELVLVC S
000726,000647: # 2 DELVLVC +2 S
000727,000648: # 3 DELVLVC +4 S
000728,000649: # 83 1 DELVIMU S
000729,000650: # 2 DELVIMU +2 S
000730,000651: # 3 DELVIMU +4 S
000731,000652: # 84 1 DELVOV S
000732,000653: # 2 DELVOV +2 S
000733,000654: # 3 DELVOV +4 S
000734,000655: # 85 1 VGBODY S
000735,000656: # 2 VGBODY +2 S
000736,000657: # 3 VGBODY +4 S
000737,000658: # 86 1 DELVLVC S
000738,000659: # 2 DELVLVC +2 S
000739,000660: # 3 DELVLVC +4 S
000740,000661: # 87 1 AZ D
000741,000662: # 2 EL D
000742,000663: # 88 1 STARAD B
000743,000664: # 2 STARAD +2 B
000744,000665: # 3 STARAD +4 B
000745,000666: # 89 1 LANDLAT G
000746,000667: # 2 LANDLONG G
000747,000668: # 3 LANDALT JJ
000748,000669: # 90 1 RANGE JJ
000749,000670: # 2 RRATE S
000750,000671: # 3 RTHETA H
000751,000672: # 91 1 P21ALT Q (MEMORY/100 TO DIPLAY TENS N.M.)
000752,000673: # 2 P21VEL P
000753,000674: # 3 P21GAM H
000754,000675: # 92 SPARE
000755,000676: # 93 1 OGC G
000756,000677: # 2 OGC +2 G
000757,000678: # 3 OGC +4 G
000758,000679: # 94 SPARE
000759,000680: # 95 SPARE
000760,000681: # 96 SPARE
000761,000682: # 97 1 DSPTEM1 C
000762,000683: # 2 DSPTEM1 +1 C
000763,000684: # 3 DSPTEM1 +2 C
000764,000685: # 98 1 DSPTEM2 C
000765,000686: # 2 DSPTEM2 +1 B
000766,000687: # 3 DSPTEM2 +2 C
000767,000688: # 99 1 WWPOS XX
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|
Page 17 |
000769,000690: # 2 WWVEL YY
000770,000691: # 3 WWBIAS AAA
|
|
Page 18 |
000772,000693: # NOUN SCALES AND FORMATS
000773,000694:
000774,000695: # -SCALE TYPE- PRECISION
000775,000696: # UNITS DECIMAL FORMAT -- AGC FORMAT
000776,000697: # ------------ -------------- -- ----------
000777,000698:
000778,000699: # -A-
000779,000700: # OCTAL XXXXX SP OCTAL
000780,000701:
000781,000702: # -B- -14
000782,000703: # FRACTIONAL .XXXXX SP BIT 1 = 2 UNITS
000783,000704: # (MAX .99996)
000784,000705:
000785,000706: # -C-
000786,000707: # WHOLE XXXXX. SP BIT 1 = 1 UNIT
000787,000708: # (MAX 16383.)
000788,000709:
000789,000710: # -D- 15
000790,000711: # CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360/2 DEGREES
000791,000712: # (MAX 359.99) (USES 15 BITS FOR MAGNI-
000792,000713: # TUDE AND 2-S COMP.)
000793,000714:
000794,000715: # -E- 14
000795,000716: # ELEVATION DEGREES XX.XXX DEGREES SP BIT 1 = 90/2 DEGREES
000796,000717: # (MAX 89.999)
000797,000718:
000798,000719: # -F- 14
000799,000720: # DEGREES (180) XXX.XX DEGREES SP BIT 1 = 180/2 DEGREES
000800,000721: # (MAX 179.99)
000801,000722:
000802,000723: # -G-
000803,000724: # DP DEGREES (90) XX.XXX DEGREES DP BIT 1 OF LOW REGISTER =
000804,000725: # 28
000805,000726: # 360/2 DEGREES
000806,000727:
000807,000728: # -H-
000808,000729: # DP DEGREES (360) XXX.XX DEGREES DP BIT 1 OF LOW REGISTER =
000809,000730: # 28
000810,000731: # (MAX 359.99) 360/2 DEGREES
000811,000732:
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|
Page 19 |
000813,000734: # -K-
000814,000735: # TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER =
000815,000736: # 000XX. MIN -2
000816,000737: # 0XX.XX SEC 10 SEC
000817,000738: # (DECIMAL ONLY.
000818,000739: # MAX MIN COMP=59
000819,000740: # MAX SEC COMP=59.99
000820,000741: # MAX CAPACITY=745 HRS
000821,000742: # 39 MINS
000822,000743: # 14.55 SECS.
000823,000744: # WHEN LOADING, ALL 3
000824,000745: # COMPONENTS MUST BE
000825,000746: # SUPPLIED.)
000826,000747:
000827,000748: # -L-
000828,000749: # TIME (MIN/SEC) XXBXX MIN/SEC DP BIT 1 OF LOW REGISTER =
000829,000750: # (B IS A BLANK -2
000830,000751: # POSITION, DECIMAL 10 SEC
000831,000752: # ONLY, DISPLAY OR
000832,000753: # MONITOR ONLY. CANNOT
000833,000754: # BE LOADED.
000834,000755: # MAX MIN COMP=59
000835,000756: # MAX SEC COMP=59
000836,000757: # VALUES GREATER THAN
000837,000758: # 59 MIN 59 SEC
000838,000759: # ARE DISPLAYED AS
000839,000760: # 59 MIN 59 SEC.)
000840,000761:
000841,000762: # -M- -2
000842,000763: # TIME (SEC) XXX.XX SEC SP BIT 1 = 10 SEC
000843,000764: # (MAX 163.83)
000844,000765:
000845,000766: # -N-
000846,000767: # TIME(SEC) DP XXX.XX SEC DP BIT 1 OF LOW REGISTER =
000847,000768: # -2
000848,000769: # 10 SEC
000849,000770:
000850,000771: # -P-
000851,000772: # VELOCITY 2 XXXXX. FEET/SEC DP BIT 1 OF HIGH REGISTER =
000852,000773: # (MAX 41994.) -7
000853,000774: # 2 METERS/CENTI-SEC
000854,000775:
000855,000776: # -Q-
000856,000777: # POSITION 4 XXXX.X NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
000857,000778: # 2 METERS
000858,000779:
000859,000780: # -S-
000860,000781: # VELOCITY 3 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
000861,000782: # -7
000862,000783: # 2 METERS/CENTI-SEC
000863,000784:
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|
Page 20 |
000865,000786: # -T- -2
000866,000787: # G XXX.XX G SP BIT 1 = 10 G
000867,000788: # (MAX 163.83)
000868,000789:
000869,000790: # -U-
000870,000791: # RENDEZVOUS XXX.XX NAUT MI DP LOW ORDER BIT OF LOW ORDER
000871,000792: # RADAR RANGE WORD = 9.38 FEET
000872,000793:
000873,000794: # -V-
000874,000795: # RENDEZVOUS XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000875,000796: # RADAR RANGE RATE WORD = -.6278 FEET/SEC
000876,000797:
000877,000798: # -W-
000878,000799: # LANDING RADAR XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000879,000800: # ALTITUDE WORD = 1.079 FEET
000880,000801:
000881,000802: # -X-
000882,000803: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000883,000804: # VELX WORD = -.6440 FEET/SEC
000884,000805:
000885,000806: # -Y-
000886,000807: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000887,000808: # VELY WORD = 1.212 FEET/SEC
000888,000809:
000889,000810: # -Z-
000890,000811: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000891,000812: # VELZ WORD = .8668 FEET/SEC
000892,000813:
000893,000814: # -AA-
000894,000815: # INITIAL/FINAL XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000895,000816: # ALTITUDE WORD = 2.345 FEET
000896,000817:
000897,000818: # -BB-
000898,000819: # ALTITUDE RATE XXXXX. FEET/SEC SP LOW ORDER BIT = .5
000899,000820: # (MAX 08191.) FEET/SEC
000900,000821:
000901,000822: # -CC-
000902,000823: # FORWARD/LATERAL XXXXX. FEET/SEC SP LOW ORDER BIT = .5571
000903,000824: # VELOCITY (MAX 09126.) FEET/SEC
000904,000825:
000905,000826: # -DD-
000906,000827: # ROTATIONAL HAND XXXXX. DEG/SEC SP FRACTIONAL PART OF PI RAD
000907,000828: # CONTROLLER ANGULAR (MAX 00044.) 4 SEC
000908,000829: # RATES
000909,000830:
000910,000831: # -EE-
000911,000832: # OPTICAL TRACKER XXX.XX DEG. DP LOW ORDER BIT OF LOW ORDER
000912,000833: # AZIMUTH ANGLE 15
000913,000834: # WORD = 360/2 DEGREES
000914,000835:
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|
Page 21 |
000916,000837:
000917,000838: # -JJ-
000918,000839: # POSITION5 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
000919,000840: # 2 METERS
000920,000841:
000921,000842: # -KK- 16
000922,000843: # WEIGHT2 XXXXX. LBS SP FRACTIONAL PART OF 2 KG
000923,000844:
000924,000845: # -NN-
000925,000846: # TRIM DEGREES 2 XXX.XX DEG SP BIT 1=.01 SEC(TIME)
000926,000847: # (MAX 032.76)
000927,000848:
000928,000849: # -PP-
000929,000850: # 2 INTEGERS +XXBYY DP BIT 1 OF HIGH REGISTER =
000930,000851: # (B IS A BLANK 1 UNIT OF XX
000931,000852: # POSITION. DECIMAL BIT 1 OF LOW REGISTER =
000932,000853: # ONLY, DISPLAY OR 1 UNIT OF YY
000933,000854: # MONITOR ONLY. CANNOT (EACH REGISTER MUST
000934,000855: # BE LOADED.) CONTAIN A POSITIVE INTEGER
000935,000856: # (MAX 99B99) LESS THAN 100)
000936,000857:
000937,000858: # -QQ-
000938,000859: # POSITION7 XXXX.X NAUT MI DP BIT 1 OF LOW REGISTER =
000939,000860: # (MAX 9058.9) -4
000940,000861: # 2 METERS
000941,000862:
000942,000863: # -RR-
000943,000864: # COMPUTED ALTITUDE XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000944,000865: # -4
000945,000866: # 2 METERS
000946,000867:
000947,000868: # -SS-
000948,000869: # DP DEGREES XXXX.X DEGREES DP BIT 1 OF HIGH REGISTER =
000949,000870: # 1 DEGREE
000950,000871:
000951,000872: # -TT-
000952,000873: # LANDING RADAR +0000X CHANNEL 33, BIT 6 = NOT POSIT. 1
000953,000874: # POSITION (DECIMAL ONLY. CHANNEL 33, BIT 7 = NOT POSIT. 2
000954,000875: # DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
000955,000876: # ONLY. CANNOT BE X = 2 FOR LR POSITION 2
000956,000877: # LOADED.)
000957,000878:
000958,000879: # -WW- 15
000959,000880: # 360-CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360 - (360/2 )
000960,000881: # (MAX 359.99) DEGREES
000961,000882: # (USES 15 BITS FOR MAGNI-
000962,000883: # TUDE AND 2-S COMP.)
000963,000884:
000964,000885: # -XX-
000965,000886: # POSITION 9 XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000966,000887: # -9
000967,000888: # 2 METERS
000968,000889:
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|
Page 22 |
000970,000891:
000971,000892: # -YY-
000972,000893: # VELOCITY 4 XXXX.X FEET/SEC DP FRACTIONAL PART OF
000973,000894: # (MAX 328.0) METERS/CENTI-SEC
000974,000895:
000975,000896: # -AAA-
000976,000897: # RADIANS XX.XXX RADIANS DP BIT 1 OF HIGH REGISTER =
000977,000898: # (MAX 31.999) -9
000978,000899: # 2 RADIANS
000979,000900:
000980,000901:
000981,000902: # THAT-S ALL ON THE NOUNS.
000982,000903:
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|
Page 23 |
000984,000905: # ALARM CODES FOR LUMINARY
000985,000906:
000986,000907: # *9 *18 *60 COLUMN
000987,000908:
000988,000909: # CODE * TYPE SET BY
000989,000910:
000990,000911: # 00105 ** AOTMARK SYSTEM IN USE
000991,000912: # 00107 MORE THAN 5 MARK PAIRS AOTMARK
000992,000913: # 00111 MARK MISSING AOTMARK
000993,000914: # 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
000994,000915: # 00113 NO INBITS AOTMARK
000995,000916: # 00114 MARK MADE BUT NOT DESIRED AOTMARK
000996,000917: # 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
000997,000918: # 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING
000998,000919: # 00206 + GIMBAL LOCK.
000999,000920: # 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
001000,000921: # 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51, P57
001001,000922: # 00211 COARSE ALIGN ERROR IMU MODE SWITCH
001002,000923: # 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH, T4RPT
001003,000924: # 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
001004,000925: # 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
001005,000926: # 00217 BAD RETURN FROM IMUSTALL P51, P52, P57
001006,000927: # 00220 IMU NOT ALIGNED - NO REFSMMAT R02, R47
001007,000928: # 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
001008,000929: # FINDCDUW
001009,000930: # 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
001010,000931: # 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
001011,000932: # 00405 TWO STARS NOT AVAILABLE P52
001012,000933: # 00421 W-MATRIX OVERFLOW INTEGRV
001013,000934: # 00430 ** ACCELERATION OVERFLOW IN INTEGRATION ORBITAL INTEGRATION
001014,000935: # 00501 P RADAR ANTENNA OUT OF LIMITS R23
001015,000936: # 00502 BAD RADAR GIMBAL ANGLE INPUT V41N72
001016,000937: # 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V41N72
001017,000938: # 00510 RADAR AUTO DESCRETE NOT PRESENT R25
001018,000939: # 00511 LR NOT IN POSITION 2 OR REPOSITIONING SERVICER
001019,000940: # 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
001020,000941: # 00515 RR CDU FAIL DISCRETE PRESENT R25
001021,000942: # 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
001022,000943: # 00521 COULD NOT READ RADAR P20
001023,000944: # 00522 LANDING RADAR POSITION CHANGE RADAR READ
001024,000945: # 00523 P LR ANTENNA DIDN'T ACHIEVE POSITION 2 SERVICER, V60 (NON-P IN V60)
001025,000946: # 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
001026,000947: # 00526 P RANGE GREATER THAN 400 NAUT. MILES P20, P22
001027,000948: # 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21, R24
001028,000949: # LUNAR SURFACE
001029,000950: # OR VEHICLE MANEUVER REQUIRED R24 (20)
001030,000951: # 00530 P LOS NOT IN MODE2 COVERAGE R21
001031,000952: # ON LUNAR SURFACE AFTER 600 SECS.
001032,000953: # 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
001033,000954: # 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32, P72,
001034,000955:
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001036,000957:
001037,000958: # 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32, P72,
001038,000959: # 00603 CSI TO CDH TIME LT TMIN12 P32, P72, P33, P73
001039,000960: # 00604 CDH TO TPI TIME LT TMIN23 P32, P72,
001040,000961: # OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
001041,000962: # 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
001042,000963: # 00606 DV EXCEEDS MAXIMUM P32,P72,
001043,000964: # 00607 ** NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET, TIMERAD
001044,000965: # 00611 NO TIG FOR GIVEN ELEV ANGLE P34, P74
001045,000966: # 00701 ILLEGAL OPTION CODE SELECTED P57
001046,000967: # 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
001047,000968: # 01102 AGC SELF TEST ERROR SELF CHECK
001048,000969: # 01103 ** UNUSED CCS BRANCH EXECUTED ABORT
001049,000970: # 01104 * DELAY ROUTINE BUSY EXEC
001050,000971: # 01105 DOWNLINK TOO FAST T4RUPT
001051,000972: # 01106 UPLINK TOO FAST T4RUPT
001052,000973: # 01107 PHASE TABLE FAILURE. ASSUME RESTART
001053,000974: # ERASABLE MEMORY IS SUSPECT. RESTART
001054,000975: # 01201 * EXECUTIVE OVERFLOW - NO VAC AREAS EXEC
001055,000976: # 01202 * EXECUTIVE OVERFLOW - NO CORE SETS EXEC
001056,000977: # 01203 * WAITLIST OVERFLOW - TOO MANY TASKS WAITLIST
001057,000978: # 01204 ** WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
001058,000979: # CALLED WITH ZERO OR NEGATIVE DELTA-TIME
001059,000980: # 01206 ** SECOND JOB ATTEMPTS TO GO TO SLEEP PINBALL
001060,000981: # 01206 VIA KYBD AND DISPLAY PROGRAM
001061,000982: # 01207 * NO VAC AREAS FOR MARKS AOTMARK
001062,000983: # 01210 * TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
001063,000984: # 01211 * ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
001064,000985: # 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
001065,000986: # 01302 ** SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
001066,000987: # 01406 BAD RETURN FROM ROOTPSRS DESCENT GUIDANCE EQS.
001067,000988: # 01406 ** BAD RETURN FROM ROOTPSRS IGNITION ALGORITHM
001068,000989:
001069,000990: # NOTE: 1406 IS A POODOO DURING THE IGNITION ALGORITHM
001070,000991: # AND AN ALARM DURING THE ACTUAL GUIDANCE PHASE.
001071,000992:
001072,000993: # 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
001073,000994: # .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
001074,000995: # VECTOR.) S40.8
001075,000996: # 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
001076,000997: # 01412 DESCENT IGNALG NOT CONVERGING P63
001077,000998: # 01501 ** KEYBOARD AND DISPLAY ALARM DURING PINBALL
001078,000999: # 01501 INTERNAL USE (NVSUB). ABORT
001079,001000: # 01502 ** ILLEGAL FLASHING DISPLAY GOPLAY
001080,001001: # 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
001081,001002: # 01600 OVERFLOW IN DRIFT TEST IMU 4
001082,001003: # 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
001083,001004: # 01601 IMU 4 (LEM)
001084,001005: # 01703 IGNITION TIME SLIPPED MIDTOAVE
001085,001006: # 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
001086,001007: # CONFIGURATION P40, P42
001087,001008:
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001089,001010:
001090,001011: # 02000 * DAP STILL IN PROGRESS AT NEXT TIME5 RUPT DAP
001091,001012: # 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
001092,001013: # 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
001093,001014: # 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
001094,001015: # 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
001095,001016: # 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
001096,001017: # 04777 ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001097,001018: # 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
001098,001019: # 10777 IMU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001099,001020: # 13777 IMU, ICDU FAILS CAUSED THE ISS WARNING T4RUPT
001100,001021: # 14777 IMU, ICDU, PIPA FAILS CAUSED THE ISSWNING T4RUPT
001101,001022:
001102,001023: # * INDICATES AN ABORT CODE THAT RESULTS IN A SOFTWARE RESTART.
001103,001024:
001104,001025: # ** INDICATES A MORE SERIOUS ABORT CODE THAT RESULTS IN THE
001105,001026: # PROGRAM GOING TO R00.
001106,001027:
001107,001028: # P INDICATES A PRIORITY ALARM.
001108,001029:
001109,001030: # ALL OTHERS ARE NON-ABORTIVE
001110,001031:
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001112,001033:
001113,001034: # CHECKLIST CODES FOR LUMINARY
001114,001035:
001115,001036: # *9 *17 *26 *9 COLUMN
001116,001037:
001117,001038: # R1CODE ACTION TO BE EFFECTED PROGRAM
001118,001039:
001119,001040: # 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
001120,001041: # 00014 PROCEED DO IMU FINE ALIGN ROUTINE P51, P63, P57
001121,001042: # 00014 ENTER DO LANDING SITE DETERMINATION (N89DISP) P57OPTION2
001122,001043: # 00015 PERFORM CELESTIAL BODY ACQUISITION R51, P51
001123,001044: # 00062 SWITCH AGC POWER DOWN P06
001124,001045: # 00201 SWITCH RR MODE TO AUTOMATIC P20, P22, R04
001125,001046: # 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12, P42, P71
001126,001047: # ALSO THR CONT TO AUTO P40, P63, P70
001127,001048: # 00205 PERFORM MANUAL ACQUISITION OF RR R23
001128,001049: # 00500 SWITCH LR ANTENNA TO POSITION 1 P63
001129,001050:
001130,001051: # SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
001131,001052: # PERFORM DENOTES START OR END OF A TASK
001132,001053: # KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
001133,001054:
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001135,001056: # OPTION CODES FOR LUMINARY
001136,001057:
001137,001058: # THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
001138,001059: # CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
001139,001060: # ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
001140,001061:
001141,001062: # *9 *17 *52 *11 *25 COLUMN
001142,001063:
001143,001064: # OPTION
001144,001065: # CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
001145,001066:
001146,001067: # 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
001147,001068: # 4=LAND SITE
001148,001069: # 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
001149,001070: # 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
001150,001071: # 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
001151,001072: # 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
001152,001073: # 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
001153,001074: # 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
001154,001075: # 2=TWO BODIES 3=ONE BODY + G
001155,001076: # 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
001156,001077: # ORBIT TO PASS OVER LM
001157,001078:
End of include-file ASSEMBLY_AND_OPERATION_INFORMATION.agc. Parent file is MAIN.agc