Source Code
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These source-code files are part of a reconstructed copy of Luminary 98, a
development version of the Apollo 11 Lunar Module (LM) Apollo Guidance Computer
(AGC) software.
The reconstruction began with source code of Luminary 99 revision 1 previously
transcribed from a digitized copy of that program. The code was then updated
by undoing changes described in original Luminary memo 85, using asterisks
indicating changed lines in the listing as a guide. While no listing of this
version is known to exist, nor are the memory-bank checksums available,
the reconstruction is believed to be correct because it was an an intermediate
step in reconstructing Luminary 97 whose reconstruction was
verified by matching memory-bank checksums to those listed in drawing 2021152G.
Note that page numbers in the reconstructed code match those on the Luminary 099
revision 001 printout, although the added code would likely have changed page
numbers for a real Luminary 98 listing.
Comments from the original source code are prefixed with a single '#' symbol,
whereas comments added later are prefixed by "##" or "###". Report any errors
noted by creating an
issue report at the Virtual AGC
project's GitHub repository.
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000019,000002: ## Copyright: Public domain.
000020,000003: ## Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
000021,000004: ## Purpose: A section of Luminary revision 98.
000022,000005: ## It is part of the reconstructed source code for the a
000023,000006: ## development version of the flight software for the Lunar
000024,000007: ## Module's (LM) Apollo Guidance Computer (AGC) for Apollo 11.
000025,000008: ## The code has been recreated from a copy of Luminary 99
000026,000009: ## revision 001, using asterisks indicating changed lines in
000027,000010: ## the listing and Luminary Memo #85, which lists changes between
000028,000011: ## Luminary 98 and 99.
000029,000012: ## Reference: pp. 1-27
000030,000013: ## Assembler: yaYUL
000031,000014: ## Contact: Ron Burkey <info@sandroid.org>.
000032,000015: ## Website: www.ibiblio.org/apollo/index.html
000033,000016: ## Mod history: 2019-07-28 MAS Created from Luminary 99.
000034,000017:
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Page 1
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000036,000019:
000037,000020: # THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
000038,000021: # THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
000039,000022:
000040,000023: # GUIDANCE SYSTEM OPERATIONS PLAN
000041,000024: # FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
000042,000025: # USING PROGRAM LUMINARY
000043,000026:
000044,000027: # THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
000045,000028: # TECHNOLOGY 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS UNDER PROJECT 55-238-70, SPONSORED BY THE MANNED
000046,000029: # SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065.
000047,000030:
000048,000031: # THIS PROGRAM IS REFERRED TO AS LUMINARY 1A
000049,000032:
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Page 2
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000051,000034:
000052,000035: # TABLE OF LOG CARDS
000053,000036: # ASSEMBLY AND OPERATION INFORMATION
000054,000037: # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
000055,000038: # CONTROLLED CONSTANTS
000056,000039: # INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
000057,000040: # FLAGWORD ASSIGNMENTS
000058,000041: # SUBROUTINE CALLS
000059,000042:
000060,000043: # TABLE OF SUBROUTINE LOG SECTIONS
000061,000044: # LUMERASE
000062,000045: # ERASABLE ASSIGNMENTS
000063,000046: # LEMONAID
000064,000047: # INTERRUPT LEAD INS
000065,000048: # T4RUPT PROGRAM
000066,000049: # RCS FAILURE MONITOR
000067,000050: # DOWNLINK LISTS
000068,000051: # AGS INITIALIZATION
000069,000052: # FRESH START AND RESTART
000070,000053: # RESTART TABLES
000071,000054: # AOTMARK
000072,000055: # EXTENDED VERBS
000073,000056: # PINBALL NOUN TABLES
000074,000057: # LEM GEOMETRY
000075,000058: # IMU COMPENSATION PACKAGE
000076,000059: # R63
000077,000060: # ATTITUDE MANEUVER ROUTINE
000078,000061: # GIMBAL LOCK AVOIDANCE
000079,000062: # KALCMANU STEERING
000080,000063: # SYSTEM TEST STANDARD LEAD INS
000081,000064: # IMU PERFORMANCE TESTS 2
000082,000065: # IMU PERFORMANCE TESTS 4
000083,000066: # PINBALL GAMES BUTTONS AND LIGHTS
000084,000067: # R60,R62
000085,000068: # S-BAND ANTENNA FOR LM
000086,000069: # LEMP20S
000087,000070: # RADAR LEADIN ROUTINES
000088,000071: # P20-P25
000089,000072: # LEMP30S
000090,000073: # P30,P37
000091,000074: # P32-P35, P72-P75
000092,000075: # GENERAL LAMBERT AIMPOINT GUIDANCE
000093,000076: # KISSING
000094,000077: # GROUND TRACKING DETERMINATION PROGRAM - P21
000095,000078: # P34-P35, P74-P75
000096,000079: # R31
000097,000080: # P76
000098,000081: # R30
000099,000082: # STABLE ORBIT - P38-P39
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Page 3
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000101,000084: # FLY
000102,000085: # BURN, BABY, BURN -- MASTER IGNITION ROUTINE
000103,000086: # P40-P47
000104,000087: # THE LUNAR LANDING
000105,000088: # THROTTLE CONTROL ROUTINES
000106,000089: # LUNAR LANDING GUIDANCE EQUATIONS
000107,000090: # P70-P71
000108,000091: # P12
000109,000092: # ASCENT GUIDANCE
000110,000093: # SERVICER
000111,000094: # LANDING ANALOG DISPLAYS
000112,000095: # FINDCDUW - GUIDAP INTERFACE
000113,000096: # LEMP50S
000114,000097: # P51-P53
000115,000098: # LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
000116,000099: # SKIPPER
000117,000100: # DOWN-TELEMETRY PROGRAM
000118,000101: # INTER-BANK COMMUNICATION
000119,000102: # INTERPRETER
000120,000103: # FIXED-FIXED CONSTANT POOL
000121,000104: # INTERPRETIVE CONSTANTS
000122,000105: # SINGLE PRECISION SUBROUTINES
000123,000106: # EXECUTIVE
000124,000107: # WAITLIST
000125,000108: # LATITUDE LONGITUDE SUBROUTINES
000126,000109: # PLANETARY INERTIAL ORIENTATION
000127,000110: # MEASUREMENT INCORPORATION
000128,000111: # CONIC SUBROUTINES
000129,000112: # INTEGRATION INITIALIZATION
000130,000113: # ORBITAL INTEGRATION
000131,000114: # INFLIGHT ALIGNMENT ROUTINES
000132,000115: # POWERED FLIGHT SUBROUTINES
000133,000116: # TIME OF FREE FALL
000134,000117: # AGC BLOCK TWO SELF-CHECK
000135,000118: # PHASE TABLE MAINTENANCE
000136,000119: # RESTARTS ROUTINE
000137,000120: # IMU MODE SWITCHING ROUTINES
000138,000121: # KEYRUPT, UPRUPT
000139,000122: # DISPLAY INTERFACE ROUTINES
000140,000123: # SERVICE ROUTINES
000141,000124: # ALARM AND ABORT
000142,000125: # UPDATE PROGRAM
000143,000126: # RTB OP CODES
000144,000127: # LMDAP
000145,000128: # T6-RUPT PROGRAMS
000146,000129: # DAP INTERFACE SUBROUTINES
000147,000130: # DAPIDLER PROGRAM
000148,000131: # P-AXIS RCS AUTOPILOT
000149,000132: # Q,R-AXIS RCS AUTOPILOT
000150,000133: # TJET LAW
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Page 4
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000152,000135: # KALMAN FILTER
000153,000136: # TRIM GIMBAL CONTROL SYSTEM
000154,000137: # AOSTASK AND AOSJOB
000155,000138: # SPS BACK-UP RCS CONTROL
000156,000139:
000157,000140: # SYMBOL TABLE LISTING
000158,000141: # UNREFERENCED SYMBOL LISTING
000159,000142: # ERASABLE & EQUALS CROSS-REFERENCE TABLE
000160,000143: # SUMMARY OF SYMBOL TABLE LISTINGS
000161,000144: # MEMORY TYPE & AVAILABLITY DISPLAY
000162,000145: # COUNT TABLE
000163,000146: # PARAGRAPHS GENERATED FOR THIS ASSEMBLY
000164,000147: # OCTAL LISTING
000165,000148: # OCCUPIED LOCATIONS TABLE
000166,000149: # SUBROS CALLED & PROGRAM STATUS
000167,000150:
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Page 5
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000169,000152: # VERB LIST FOR LUMINARY
000170,000153:
000171,000154: # REGULAR VERBS
000172,000155:
000173,000156: # 00 NOT IN USE
000174,000157: # 01 DISPLAY OCTAL COMP 1 IN R1
000175,000158: # 02 DISPLAY OCTAL COMP 2 IN R1
000176,000159: # 03 DISPLAY OCTAL COMP 3 IN R1
000177,000160: # 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
000178,000161: # 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
000179,000162: # 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000180,000163: # 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
000181,000164: # 08
000182,000165: # 09
000183,000166: # 10
000184,000167: # 11 MONITOR OCTAL COMP 1 IN R1
000185,000168: # 12 MONITOR OCTAL COMP 2 IN R1
000186,000169: # 13 MONITOR OCTAL COMP 3 IN R1
000187,000170: # 14 MONITOR OCTAL COMP 1,2 IN R1,R2
000188,000171: # 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
000189,000172: # 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000190,000173: # 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
000191,000174: # 18
000192,000175: # 19
000193,000176: # 20
000194,000177: # 21 LOAD COMPONENT 1 INTO R1
000195,000178: # 22 LOAD COMPONENT 2 INTO R2
000196,000179: # 23 LOAD COMPONENT 3 INTO R3
000197,000180: # 24 LOAD COMPONENT 1,2 INTO R1,R2
000198,000181: # 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
000199,000182: # 26
000200,000183: # 27 DISPLAY FIXED MEMORY
000201,000184: # 28
000202,000185: # 29
000203,000186: # 30 REQUEST EXECUTIVE
000204,000187: # 31 REQUEST WAITLIST
000205,000188: # 32 RECYCLE PROGRAM
000206,000189: # 33 PROCEED WITHOUT DSKY INPUTS
000207,000190: # 34 TERMINATE FUNCTION
000208,000191: # 35 TEST LIGHTS
000209,000192: # 36 REQUEST FRESH START
000210,000193: # 37 CHANGE PROGRAM (MAJOR MODE)
000211,000194: # 38
000212,000195: # 39
000213,000196:
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Page 6
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000215,000198: # EXTENDED VERBS
000216,000199:
000217,000200: # 40 ZERO CDU-S
000218,000201: # 41 COARSE ALIGN CDU-S
000219,000202: # 42 FINE ALIGN IMU
000220,000203: # 43 LOAD IMU ATT ERROR METERS
000221,000204: # 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
000222,000205: # 45
000223,000206: # 46
000224,000207: # 47 INITIALIZE AGS (R47)
000225,000208: # 48 REQUEST DAP DATA LOAD ROUTINE (R03)
000226,000209: # 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
000227,000210: # 50 PLEASE PERFORM
000228,000211: # 51
000229,000212: # 52 MARK X-RETICLE
000230,000213: # 53 MARK Y-RETICLE
000231,000214: # 54 MARK X OR Y-RETICLE
000232,000215: # 55 INCREMENT AGC TIME (DECIMAL)
000233,000216: # 56 TERMINATE TRACKING (P20 + P25)
000234,000217: # 57 PERMIT LANDING RADAR UPDATES
000235,000218: # 58 INHIBIT LANDING RADAR UPDATES
000236,000219: # 59
000237,000220: # 60 COMMAND LR TO POSITION 2.
000238,000221: # 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
000239,000222: # 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
000240,000223: # 63 SAMPLE RADAR ONCE PER SECOND (R04).
000241,000224: # 64 REQUEST S-BAND ANTENNA ROUTINE (R05)
000242,000225: # 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
000243,000226: # 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
000244,000227: # 67 DISPLAY W MATRIX
000245,000228: # 68
000246,000229: # 69 CAUSE RESTART
000247,000230: # 70 UPDATE LIFTOFF TIME
000248,000231: # 71 UNIVERSAL UPDATE-BLOCK ADR
000249,000232: # 72 UNIVERSAL UPDATE-SINGLE ADR
000250,000233: # 73 UPDATE AGC TIME (OCTAL)
000251,000234: # 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
000252,000235: # 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
000253,000236: # 76 MINIMUM IMPULSE COMMAND MODE
000254,000237: # 77 RATE COMMAND AND ATTITUDE HOLD MODE
000255,000238: # 78 LR SPURIOUS RETURN TEST START (R77)
000256,000239: # 79 LR SPURIOUS RETURN TEST STOP
000257,000240: # 80 UPDATE LEM STATE VECTOR
000258,000241: # 81 UPDATE CSM STATE VECTOR
000259,000242: # 82 REQUEST ORBIT PARAM DISPLAY (R30)
000260,000243: # 83 REQUEST REND PARAM DISPLAY (R31)
000261,000244: # 84
000262,000245: # 85 DISPLAY RR LOS AZ AND ELEV
000263,000246: # 86
000264,000247: # 87
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Page 7
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000266,000249: # 88
000267,000250: # 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
000268,000251: # 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
000269,000252: # 91 DISPLAY BANK SUM
000270,000253: # 92 OPERATE IMU PERFORMANCE TEST (P07)
000271,000254: # 93 ENABLE W MATRIX INITIALIZATION
000272,000255: # 94
000273,000256: # 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
000274,000257: # 96 INTERRUPT INTEGRATION AND GO TO POO
000275,000258: # 97 PERFORM ENGINE FAIL PROCEDURE
000276,000259: # 98
000277,000260: # 99 PLEASE ENABLE ENGINE
000278,000261:
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Page 8
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000280,000263: # IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
000281,000264: # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
000282,000265: # SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
000283,000266: # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23
000284,000267: # MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
000285,000268: # ABOVE SCALE TYPES.
000286,000269:
000287,000270: # THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
000288,000271: # EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
000289,000272:
000290,000273: # NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000291,000274: # 00 NOT IN USE
000292,000275: # 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH
000293,000276: # 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH
000294,000277: # 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP XXX.XX DEG FOR EACH
000295,000278: # 04 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000296,000279: # 05 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000297,000280: # 06 OPTION CODE 3COMP OCTAL ONLY FOR EACH
000298,000281: # LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
000299,000282: # 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
000300,000283: # ONES FOR BITS TO BE MODIFIED
000301,000284: # 1 TO SET OR 0 TO RESET SELECTED BITS
000302,000285: # 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
000303,000286: # 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
000304,000287: # 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
000305,000288: # 11 TIG OF CSI 3COMP 00XXX. HRS DEC ONLY
000306,000289: # 000XX. MIN MUST LOAD 3 COMPS
000307,000290: # 0XX.XX SEC
000308,000291: # 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
000309,000292: # (USED BY EXTENDED VERBS ONLY)
000310,000293: # 13 TIG OF CDH 3COMP 00XXX. HRS DEC ONLY
000311,000294: # 000XX. MIN MUST LOAD 3 COMPS
000312,000295: # 0XX.XX SEC
000313,000296: # 14 CHECKLIST 3COMP XXXXX. FOR EACH
000314,000297: # (USED BY EXTENDED VERBS ONLY)
000315,000298: # (NOUN 25 IS PASTED AFTER DISPLAY)
000316,000299: # 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
000317,000300: # 16 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000318,000301: # (USED BY EXTENDED VERBS ONLY) 000XX. MIN MUST LOAD 3 COMPS
000319,000302: # 0XX.XX SEC
000320,000303: # 17 SPARE
000321,000304: # 18 AUTO MANEUVER BALL ANGLES 3COMP XXX.XX DEG FOR EACH
000322,000305: # 19 SPARE
000323,000306: # 20 ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000324,000307: # 21 PIPAS 3COMP XXXXX. PULSES FOR EACH
000325,000308: # 22 NEW ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000326,000309: # 23 SPARE
000327,000310: # 24 DELTA TIME FOR AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000328,000311: # 000XX. MIN MUST LOAD 3 COMPS
000329,000312: # 0XX.XX SEC
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Page 9
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000331,000314: # 25 CHECKLIST 3COMP XXXXX. FOR EACH
000332,000315: # (USED WITH PLEASE PERFORM ONLY)
000333,000316: # 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
000334,000317: # 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX.
000335,000318: # 28 SPARE
000336,000319: # 29 SPARE
000337,000320: # 30 SPARE
000338,000321: # 31 SPARE
000339,000322: # 32 TIME FROM PERIGEE 3COMP 00XXX. HRS DEC ONLY
000340,000323: # 000XX. MIN MUST LOAD 3 COMPS
000341,000324: # 0XX.XX SEC
000342,000325: # 33 TIME OF IGNITION 3COMP 00XXX. HRS DEC ONLY
000343,000326: # 000XX. MIN MUST LOAD 3 COMPS
000344,000327: # 0XX.XX SEC
000345,000328: # 34 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000346,000329: # 000XX. MIN MUST LOAD 3 COMPS
000347,000330: # 0XX.XX SEC
000348,000331: # 35 TIME FROM EVENT 3COMP 00XXX. HRS DEC ONLY
000349,000332: # 000XX. MIN MUST LOAD 3 COMPS
000350,000333: # 0XX.XX SEC
000351,000334: # 36 TIME OF AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000352,000335: # 000XX. MIN MUST LOAD 3 COMPS
000353,000336: # 0XX.XX SEC
000354,000337: # 37 TIG OF TPI 3COMP 00XXX. HRS DEC ONLY
000355,000338: # 000XX. MIN MUST LOAD 3 COMPS
000356,000339: # 0XX.XX SEC
000357,000340: # 38 TIME OF STATE BEING INTEGRATED 3COMP 00XXX. HRS DEC ONLY
000358,000341: # 000XX. MIN MUST LOAD 3 COMPS
000359,000342: # 0XX.XX SEC
000360,000343: # 39 SPARE
000361,000344:
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Page 10
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000363,000346: # MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000364,000347: # 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000365,000348: # VG, XXXX.X FT/SEC
000366,000349: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000367,000350: # 41 TARGET AZIMUTH, 2COMP XXX.XX DEG (FOR SYSTEM TEST)
000368,000351: # ELEVATION XX.XXX DEG
000369,000352: # 42 APOGEE, 3COMP XXXX.X NAUT MI DEC ONLY
000370,000353: # PERIGEE, XXXX.X NAUT MI
000371,000354: # DELTA V (REQUIRED) XXXX.X FT/SEC
000372,000355: # 43 LATITUDE, 3COMP XXX.XX DEG DEC ONLY
000373,000356: # LONGITUDE, XXX.XX DEG
000374,000357: # ALTITUDE XXXX.X NAUT MI
000375,000358: # 44 APOGEE, 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000376,000359: # PERIGEE, XXXX.X NAUT MI
000377,000360: # TFF XXBXX MIN/SEC
000378,000361: # 45 MARKS, 3COMP XXXXX. NO LOAD, DEC ONLY
000379,000362: # TFI OF NEXT BURN XXBXX MIN/SEC
000380,000363: # MGA XXX.XX DEG
000381,000364: # 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
000382,000365: # 47 LEM WEIGHT, 2COMP XXXXX. LBS DEC ONLY
000383,000366: # CSM WEIGHT XXXXX. LBS
000384,000367: # 48 GIMBAL PITCH TRIM, 2COMP XXX.XX DEG DEC ONLY
000385,000368: # GIMBAL ROLL TRIM XXX.XX DEG
000386,000369: # 49 DELTA R, 3COMP XXXX.X NAUT MI DEC ONLY
000387,000370: # DELTA V, XXXX.X FT/SEC
000388,000371: # RADAR DATA SOURCE CODE XXXXX.
000389,000372: # 50 SPARE
000390,000373: # 51 S-BAND ANTENNA ANGLES PITCH 2COMP XXX.XX DEG DEC ONLY
000391,000374: # YAW XXX.XX DEG
000392,000375: # 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG
000393,000376: # 53 SPARE
000394,000377: # 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
000395,000378: # RANGE RATE, XXXX.X FT/SEC
000396,000379: # THETA XXX.XX DEG
000397,000380: # 55 NO. OF APSIDAL CROSSINGS 3COMP XXXXX. DEC ONLY
000398,000381: # ELEVATION ANGLE XXX.XX DEG
000399,000382: # CENTRAL ANGLE OF PASSIVE VEHICLE XXX.XX DEG
000400,000383: # 56 RR LOS AZIMUTH 2COMP XXX.XX DEG
000401,000384: # ELEVATION XXX.XX DEG
000402,000385: # 57 DELTA R 1COMP XXXX.X NAUT MI DEC ONLY
000403,000386: # 58 PERIGEE ALT (POST TPI) 3COMP XXXX.X NAUT MI DEC ONLY
000404,000387: # DELTA V TPI XXXX.X FT/SEC
000405,000388: # DELTA V TPF XXXX.X FT/SEC
000406,000389: # 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY
000407,000390: # 60 HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000408,000391: # ALTITUDE RATE XXXX.X FT/SEC
000409,000392: # COMPUTED ALTITUDE XXXXX. FEET
000410,000393: # 61 TIME TO GO IN BRAKING PHASE 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000411,000394: # TIME FROM IGNITION XXBXX MIN/SEC
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Page 11
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000413,000396: # CROSS RANGE DISTANCE XXXX.X NAUT MI
000414,000397: # 62 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC NO LOAD, DEC ONLY
000415,000398: # TIME FROM IGNITION XXBXX MIN/SEC
000416,000399: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000417,000400: # 63 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000418,000401: # ALTITUDE RATE XXXX.X FT/SEC
000419,000402: # COMPUTED ALTITUDE XXXXX. FEET
000420,000403: # 64 TIME LEFT FOR REDESIGNATION- LPD ANGLE 3COMP XXBXX NO LOAD, DEC ONLY
000421,000404: # ALTITUDE RATE XXXX.X FT/SEC
000422,000405: # COMPUTED ALTITUDE XXXXX. FEET
000423,000406: # 65 SAMPLED AGC TIME 3COMP 00XXX. HRS DEC ONLY
000424,000407: # (FETCHED IN INTERRUPT) 000XX. MIN MUST LOAD 3 COMPS
000425,000408: # 0XX.XX SEC
000426,000409: # 66 LR RANGE 2COMP XXXXX. FEET NO LOAD, DEC ONLY
000427,000410: # POSITION +0000X
000428,000411: # 67 LRVX 3COMP XXXXX. FT/SEC
000429,000412: # LRVY XXXXX. FT/SEC
000430,000413: # LRVZ XXXXX. FT/SEC
000431,000414: # 68 SLANT RANGE TO LANDING SITE 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000432,000415: # TIME TO GO IN BRAKING PHASE XXBXX MIN/SEC
000433,000416: # LR ALTITUDE - COMPUTED ALTITUDE XXXXX. FEET
000434,000417: # 69 SPARE
000435,000418: # 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000436,000419: # 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000437,000420: # 72 RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000438,000421: # SHAFT ANGLE XXX.XX DEG
000439,000422: # 73 NEW RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000440,000423: # SHAFT ANGLE XXX.XX DEG
000441,000424: # 74 TIME FROM IGNITION 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000442,000425: # YAW AFTER VEHICLE RISE XXX.XX DEG
000443,000426: # PITCH AFTER VEHICLE RISE XXX.XX DEG
000444,000427: # 75 DELTA ALTITUDE CDH 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000445,000428: # DELTA TIME (CDH-CSI OR TPI-CDH) XXBXX MIN/SEC
000446,000429: # DELTA TIME (TPI-CDH OR TPI-NOMTPI) XXBXX MIN/SEC
000447,000430: # 76 DESIRED HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000448,000431: # DESIRED RADIAL VELOCITY XXXX.X FT/SEC
000449,000432: # CROSS-RANGE DISTANCE XXXX.X NAUT MI
000450,000433: # 77 TIME TO ENGINE CUTOFF 2COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000451,000434: # VELOCITY NORMAL TO CSM PLANE XXXX.X FT/SEC
000452,000435: # 78 RR RANGE 2COMP XXX.XX NAUT MI
000453,000436: # RANGE RATE XXXXX. FT/SEC
000454,000437: # 79 CURSOR ANGLE 3COMP XXX.XX DEG DEC ONLY
000455,000438: # SPIRAL ANGLE XXX.XX DEG
000456,000439: # POSITION CODE XXXXX.
000457,000440: # 80 DATA INDICATOR, 2COMP XXXXX.
000458,000441: # OMEGA XXX.XX DEG
000459,000442: # 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
|
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Page 12
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000461,000444: # 82 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000462,000445: # 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000463,000446: # 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000464,000447: # 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000465,000448: # 86 VG (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000466,000449: # 87 BACKUP OPTICS LOS AZIMUTH 2COMP XXX.XX DEG
000467,000450: # ELEVATION XXX.XX DEG
000468,000451: # 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY
000469,000452: # 89 LANDMARK LATITUDE 3COMP XX.XXX DEG DEC ONLY
000470,000453: # LONGITUDE/2 XX.XXX DEC
000471,000454: # ALTITUDE XXX.XX NAUT MI
000472,000455: # 90 Y 3COMP XXX.XX NM DEC ONLY
000473,000456: # Y DOT XXXX.X FPS
000474,000457: # PSI XXX.XX DEG
000475,000458: # 91 ALTITUDE 3COMP XXXXXB. NAUT MI
000476,000459: # VELOCITY XXXXX. FT/SEC
000477,000460: # FLIGHT PATH ANGLE XXX.XX DEG
000478,000461: # 92 SPARE
000479,000462: # 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
000480,000463: # 94 SPARE
000481,000464: # 95 SPARE
000482,000465: # 96 SPARE
000483,000466: # 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH
000484,000467: # 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX.
000485,000468: # .XXXXX
000486,000469: # XXXXX.
000487,000470: # 99 RMS IN POSITION 3COMP XXXXX. FT DEC ONLY
000488,000471: # RMS IN VELOCITY XXXX.X FT/SEC
000489,000472: # RMS IN BIAS XX.XXX RADIANS
000490,000473:
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Page 13
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000492,000475: # REGISTERS AND SCALING FOR NORMAL NOUNS
000493,000476:
000494,000477: # NOUN REGISTER SCALE TYPE
000495,000478: # 00 NOT IN USE
000496,000479: # 01 SPECIFY ADDRESS B
000497,000480: # 02 SPECIFY ADDRESS C
000498,000481: # 03 SPECIFY ADDRESS D
000499,000482: # 04 DSPTEM1 H
000500,000483: # 05 DSPTEM1 H
000501,000484: # 06 OPTION1 A
000502,000485: # 07 XREG A
000503,000486: # 08 ALMCADR A
000504,000487: # 09 FAILREG A
000505,000488: # 10 SPECIFY CHANNEL A
000506,000489: # 11 TCSI K
000507,000490: # 12 OPTIONX A
000508,000491: # 13 TCDH K
000509,000492: # 14 DSPTEMX C
000510,000493: # 15 INCREMENT ADDRESS A
000511,000494: # 16 DSPTEMX C
000512,000495: # 17 SPARE
000513,000496: # 18 FDAIX D
000514,000497: # 19 SPARE
000515,000498: # 20 CDUX D
000516,000499: # 21 PIPAX C
000517,000500: # 22 THETAD D
000518,000501: # 23 SPARE
000519,000502: # 24 DSPTEM2 +1 K
000520,000503: # 25 DSPTEM1 C
000521,000504: # 26 DSPTEM1 A
000522,000505: # 27 SMODE C
000523,000506: # 28 SPARE
000524,000507: # 29 SPARE
000525,000508: # 30 SPARE
000526,000509: # 31 SPARE
000527,000510: # 32 -TPER K
000528,000511: # 33 TIG K
000529,000512: # 34 DSPTEM1 K
000530,000513: # 35 TTOGO K
000531,000514: # 36 TIME2 K
000532,000515: # 37 TTPI K
000533,000516: # 38 TET K
000534,000517: # 39 SPARE
000535,000518:
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Page 14
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000537,000520: # REGISTERS AND SCALING FOR MIXED NOUNS
000538,000521:
000539,000522: # NOUN COMP REGISTER SCALE TYPE
000540,000523: # 40 1 TTOGO L
000541,000524: # 2 VGDISP S
000542,000525: # 3 DVTOTAL S
000543,000526: # 41 1 DSPTEM1 D
000544,000527: # 2 DSPTEM1 +1 E
000545,000528: # 42 1 HAPO Q
000546,000529: # 2 HPER Q
000547,000530: # 3 VGDISP S
000548,000531: # 43 1 LAT H
000549,000532: # 2 LONG H
000550,000533: # 3 ALT Q
000551,000534: # 44 1 HAPOX Q
000552,000535: # 2 HPERX Q
000553,000536: # 3 TFF L
000554,000537: # 45 1 TRKMKCNT C
000555,000538: # 2 TTOGO L
000556,000539: # 3 +MGA H
000557,000540: # 46 1 DAPDATR1 A
000558,000541: # 47 1 LEMMASS KK
000559,000542: # 2 CSMMASS KK
000560,000543: # 48 1 PITTIME NN
000561,000544: # 2 ROLLTIME NN
000562,000545: # 49 1 R22DISP Q
000563,000546: # 2 R22DISP +2 S
000564,000547: # 3 WHCHREAD C
000565,000548: # 50 SPARE
000566,000549: # 51 1 ALPHASB H
000567,000550: # 2 BETASB H
000568,000551: # 52 1 ACTCENT H
000569,000552: # 53 SPARE
000570,000553: # 54 1 RANGE JJ
000571,000554: # 2 RRATE S
000572,000555: # 3 RTHETA H
000573,000556: # 55 1 NN C
000574,000557: # 2 ELEV H
000575,000558: # 3 CENTANG H
000576,000559: # 56 1 RR-AZ H
000577,000560: # 2 RR-ELEV H
000578,000561: # 57 1 DELTAR Q
000579,000562: # 58 1 POSTTPI Q
000580,000563: # 2 DELVTPI S
000581,000564: # 3 DELVTPF S
000582,000565: # 59 1 DVLOS S
000583,000566: # 2 DVLOS +2 S
000584,000567: # 3 DVLOS +4 S
000585,000568: # 60 1 VHORIZ S
|
|
Page 15
|
000587,000570: # 2 HDOTDISP S
000588,000571: # 3 HCALC RR
000589,000572: # 61 1 TTFDISP L
000590,000573: # 2 TTOGO L
000591,000574: # 3 OUTOFPLN QQ
000592,000575: # 62 1 ABVEL S
000593,000576: # 2 TTOGO L
000594,000577: # 3 DVTOTAL S
000595,000578: # 63 1 ABVEL S
000596,000579: # 2 HDOTDISP S
000597,000580: # 3 HCALC1 RR
000598,000581: # 64 1 FUNNYDSP PP
000599,000582: # 2 HDOTDISP S
000600,000583: # 3 HCALC RR
000601,000584: # 65 1 SAMPTIME K
000602,000585: # 2 SAMPTIME K
000603,000586: # 3 SAMPTIME K
000604,000587: # 66 1 RSTACK +6 W
000605,000588: # 2 CHANNEL 33 TT
000606,000589: # 67 1 RSTACK X
000607,000590: # 2 RSTACK +2 Y
000608,000591: # 3 RSTACK +4 Z
000609,000592: # 68 1 RANGEDSP QQ
000610,000593: # 2 TTFDISP L
000611,000594: # 3 DELTAH RR
000612,000595: # 69 SPARE
000613,000596: # 70 1 AOTCODE A
000614,000597: # 2 AOTCODE +1 A
000615,000598: # 3 AOTCODE +2 A
000616,000599: # 71 1 AOTCODE A
000617,000600: # 2 AOTCODE +1 A
000618,000601: # 3 AOTCODE +2 A
000619,000602: # 72 1 CDUT WW
000620,000603: # 2 CDUS D
000621,000604: # 73 1 TANG WW
000622,000605: # 2 TANG +1 D
000623,000606: # 74 1 TTOGO L
000624,000607: # 2 YAW H
000625,000608: # 3 PITCH H
000626,000609: # 75 1 DIFFALT Q
000627,000610: # 2 T1TOT2 L
000628,000611: # 3 T2TOT3 L
000629,000612: # 76 1 ZDOTD S
000630,000613: # 2 RDOTD S
000631,000614: # 3 XRANGE Q
000632,000615: # 77 1 TTOGO L
000633,000616: # 2 YDOT S
000634,000617: # 78 1 RSTACK U
000635,000618: # 2 RSTACK +2 V
000636,000619: # 79 1 CURSOR D
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|
Page 16
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000638,000621: # 2 SPIRAL D
000639,000622: # 3 POSCODE C
000640,000623: # 80 1 DATAGOOD C
000641,000624: # 2 OMEGAD H
000642,000625: # 81 1 DELVLVC S
000643,000626: # 2 DELVLVC +2 S
000644,000627: # 3 DELVLVC +4 S
000645,000628: # 82 1 DELVLVC S
000646,000629: # 2 DELVLVC +2 S
000647,000630: # 3 DELVLVC +4 S
000648,000631: # 83 1 DELVIMU S
000649,000632: # 2 DELVIMU +2 S
000650,000633: # 3 DELVIMU +4 S
000651,000634: # 84 1 DELVOV S
000652,000635: # 2 DELVOV +2 S
000653,000636: # 3 DELVOV +4 S
000654,000637: # 85 1 VGBODY S
000655,000638: # 2 VGBODY +2 S
000656,000639: # 3 VGBODY +4 S
000657,000640: # 86 1 DELVLVC S
000658,000641: # 2 DELVLVC +2 S
000659,000642: # 3 DELVLVC +4 S
000660,000643: # 87 1 AZ D
000661,000644: # 2 EL D
000662,000645: # 88 1 STARAD B
000663,000646: # 2 STARAD +2 B
000664,000647: # 3 STARAD +4 B
000665,000648: # 89 1 LANDLAT G
000666,000649: # 2 LANDLONG G
000667,000650: # 3 LANDALT JJ
000668,000651: # 90 1 RANGE JJ
000669,000652: # 2 RRATE S
000670,000653: # 3 RTHETA H
000671,000654: # 91 1 P21ALT Q (MEMORY/100 TO DIPLAY TENS N.M.)
000672,000655: # 2 P21VEL P
000673,000656: # 3 P21GAM H
000674,000657: # 92 SPARE
000675,000658: # 93 1 OGC G
000676,000659: # 2 OGC +2 G
000677,000660: # 3 OGC +4 G
000678,000661: # 94 SPARE
000679,000662: # 95 SPARE
000680,000663: # 96 SPARE
000681,000664: # 97 1 DSPTEM1 C
000682,000665: # 2 DSPTEM1 +1 C
000683,000666: # 3 DSPTEM1 +2 C
000684,000667: # 98 1 DSPTEM2 C
000685,000668: # 2 DSPTEM2 +1 B
000686,000669: # 3 DSPTEM2 +2 C
000687,000670: # 99 1 WWPOS XX
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Page 17
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000689,000672: # 2 WWVEL YY
000690,000673: # 3 WWBIAS AAA
|
|
Page 18
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000692,000675: # NOUN SCALES AND FORMATS
000693,000676:
000694,000677: # -SCALE TYPE- PRECISION
000695,000678: # UNITS DECIMAL FORMAT -- AGC FORMAT
000696,000679: # ------------ -------------- -- ----------
000697,000680:
000698,000681: # -A-
000699,000682: # OCTAL XXXXX SP OCTAL
000700,000683:
000701,000684: # -B- -14
000702,000685: # FRACTIONAL .XXXXX SP BIT 1 = 2 UNITS
000703,000686: # (MAX .99996)
000704,000687:
000705,000688: # -C-
000706,000689: # WHOLE XXXXX. SP BIT 1 = 1 UNIT
000707,000690: # (MAX 16383.)
000708,000691:
000709,000692: # -D- 15
000710,000693: # CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360/2 DEGREES
000711,000694: # (MAX 359.99) (USES 15 BITS FOR MAGNI-
000712,000695: # TUDE AND 2-S COMP.)
000713,000696:
000714,000697: # -E- 14
000715,000698: # ELEVATION DEGREES XX.XXX DEGREES SP BIT 1 = 90/2 DEGREES
000716,000699: # (MAX 89.999)
000717,000700:
000718,000701: # -F- 14
000719,000702: # DEGREES (180) XXX.XX DEGREES SP BIT 1 = 180/2 DEGREES
000720,000703: # (MAX 179.99)
000721,000704:
000722,000705: # -G-
000723,000706: # DP DEGREES (90) XX.XXX DEGREES DP BIT 1 OF LOW REGISTER =
000724,000707: # 28
000725,000708: # 360/2 DEGREES
000726,000709:
000727,000710: # -H-
000728,000711: # DP DEGREES (360) XXX.XX DEGREES DP BIT 1 OF LOW REGISTER =
000729,000712: # 28
000730,000713: # (MAX 359.99) 360/2 DEGREES
000731,000714:
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Page 19
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000733,000716: # -K-
000734,000717: # TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER =
000735,000718: # 000XX. MIN -2
000736,000719: # 0XX.XX SEC 10 SEC
000737,000720: # (DECIMAL ONLY.
000738,000721: # MAX MIN COMP=59
000739,000722: # MAX SEC COMP=59.99
000740,000723: # MAX CAPACITY=745 HRS
000741,000724: # 39 MINS
000742,000725: # 14.55 SECS.
000743,000726: # WHEN LOADING, ALL 3
000744,000727: # COMPONENTS MUST BE
000745,000728: # SUPPLIED.)
000746,000729:
000747,000730: # -L-
000748,000731: # TIME (MIN/SEC) XXBXX MIN/SEC DP BIT 1 OF LOW REGISTER =
000749,000732: # (B IS A BLANK -2
000750,000733: # POSITION, DECIMAL 10 SEC
000751,000734: # ONLY, DISPLAY OR
000752,000735: # MONITOR ONLY. CANNOT
000753,000736: # BE LOADED.
000754,000737: # MAX MIN COMP=59
000755,000738: # MAX SEC COMP=59
000756,000739: # VALUES GREATER THAN
000757,000740: # 59 MIN 59 SEC
000758,000741: # ARE DISPLAYED AS
000759,000742: # 59 MIN 59 SEC.)
000760,000743:
000761,000744: # -M- -2
000762,000745: # TIME (SEC) XXX.XX SEC SP BIT 1 = 10 SEC
000763,000746: # (MAX 163.83)
000764,000747:
000765,000748: # -N-
000766,000749: # TIME(SEC) DP XXX.XX SEC DP BIT 1 OF LOW REGISTER =
000767,000750: # -2
000768,000751: # 10 SEC
000769,000752:
000770,000753: # -P-
000771,000754: # VELOCITY 2 XXXXX. FEET/SEC DP BIT 1 OF HIGH REGISTER =
000772,000755: # (MAX 41994.) -7
000773,000756: # 2 METERS/CENTI-SEC
000774,000757:
000775,000758: # -Q-
000776,000759: # POSITION 4 XXXX.X NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
000777,000760: # 2 METERS
000778,000761:
000779,000762: # -S-
000780,000763: # VELOCITY 3 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
000781,000764: # -7
000782,000765: # 2 METERS/CENTI-SEC
000783,000766:
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Page 20
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000785,000768: # -T- -2
000786,000769: # G XXX.XX G SP BIT 1 = 10 G
000787,000770: # (MAX 163.83)
000788,000771:
000789,000772: # -U-
000790,000773: # RENDEZVOUS XXX.XX NAUT MI DP LOW ORDER BIT OF LOW ORDER
000791,000774: # RADAR RANGE WORD = 9.38 FEET
000792,000775:
000793,000776: # -V-
000794,000777: # RENDEZVOUS XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000795,000778: # RADAR RANGE RATE WORD = -.6278 FEET/SEC
000796,000779:
000797,000780: # -W-
000798,000781: # LANDING RADAR XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000799,000782: # ALTITUDE WORD = 1.079 FEET
000800,000783:
000801,000784: # -X-
000802,000785: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000803,000786: # VELX WORD = -.6440 FEET/SEC
000804,000787:
000805,000788: # -Y-
000806,000789: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000807,000790: # VELY WORD = 1.212 FEET/SEC
000808,000791:
000809,000792: # -Z-
000810,000793: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000811,000794: # VELZ WORD = .8668 FEET/SEC
000812,000795:
000813,000796: # -AA-
000814,000797: # INITIAL/FINAL XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000815,000798: # ALTITUDE WORD = 2.345 FEET
000816,000799:
000817,000800: # -BB-
000818,000801: # ALTITUDE RATE XXXXX. FEET/SEC SP LOW ORDER BIT = .5
000819,000802: # (MAX 08191.) FEET/SEC
000820,000803:
000821,000804: # -CC-
000822,000805: # FORWARD/LATERAL XXXXX. FEET/SEC SP LOW ORDER BIT = .5571
000823,000806: # VELOCITY (MAX 09126.) FEET/SEC
000824,000807:
000825,000808: # -DD-
000826,000809: # ROTATIONAL HAND XXXXX. DEG/SEC SP FRACTIONAL PART OF PI RAD
000827,000810: # CONTROLLER ANGULAR (MAX 00044.) 4 SEC
000828,000811: # RATES
000829,000812:
000830,000813: # -EE-
000831,000814: # OPTICAL TRACKER XXX.XX DEG. DP LOW ORDER BIT OF LOW ORDER
000832,000815: # AZIMUTH ANGLE 15
000833,000816: # WORD = 360/2 DEGREES
000834,000817:
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Page 21
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000836,000819:
000837,000820: # -JJ-
000838,000821: # POSITION5 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
000839,000822: # 2 METERS
000840,000823:
000841,000824: # -KK- 16
000842,000825: # WEIGHT2 XXXXX. LBS SP FRACTIONAL PART OF 2 KG
000843,000826:
000844,000827: # -NN-
000845,000828: # TRIM DEGREES 2 XXX.XX DEG SP BIT 1=.01 SEC(TIME)
000846,000829: # (MAX 032.76)
000847,000830:
000848,000831: # -PP-
000849,000832: # 2 INTEGERS +XXBYY DP BIT 1 OF HIGH REGISTER =
000850,000833: # (B IS A BLANK 1 UNIT OF XX
000851,000834: # POSITION. DECIMAL BIT 1 OF LOW REGISTER =
000852,000835: # ONLY, DISPLAY OR 1 UNIT OF YY
000853,000836: # MONITOR ONLY. CANNOT (EACH REGISTER MUST
000854,000837: # BE LOADED.) CONTAIN A POSITIVE INTEGER
000855,000838: # (MAX 99B99) LESS THAN 100)
000856,000839:
000857,000840: # -QQ-
000858,000841: # POSITION7 XXXX.X NAUT MI DP BIT 1 OF LOW REGISTER =
000859,000842: # (MAX 9058.9) -4
000860,000843: # 2 METERS
000861,000844:
000862,000845: # -RR-
000863,000846: # COMPUTED ALTITUDE XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000864,000847: # -4
000865,000848: # 2 METERS
000866,000849:
000867,000850: # -SS-
000868,000851: # DP DEGREES XXXX.X DEGREES DP BIT 1 OF HIGH REGISTER =
000869,000852: # 1 DEGREE
000870,000853:
000871,000854: # -TT-
000872,000855: # LANDING RADAR +0000X CHANNEL 33, BIT 6 = NOT POSIT. 1
000873,000856: # POSITION (DECIMAL ONLY. CHANNEL 33, BIT 7 = NOT POSIT. 2
000874,000857: # DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
000875,000858: # ONLY. CANNOT BE X = 2 FOR LR POSITION 2
000876,000859: # LOADED.)
000877,000860:
000878,000861: # -WW- 15
000879,000862: # 360-CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360 - (360/2 )
000880,000863: # (MAX 359.99) DEGREES
000881,000864: # (USES 15 BITS FOR MAGNI-
000882,000865: # TUDE AND 2-S COMP.)
000883,000866:
000884,000867: # -XX-
000885,000868: # POSITION 9 XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000886,000869: # -9
000887,000870: # 2 METERS
000888,000871:
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|
Page 22
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000890,000873:
000891,000874: # -YY-
000892,000875: # VELOCITY 4 XXXX.X FEET/SEC DP FRACTIONAL PART OF
000893,000876: # (MAX 328.0) METERS/CENTI-SEC
000894,000877:
000895,000878: # -AAA-
000896,000879: # RADIANS XX.XXX RADIANS DP BIT 1 OF HIGH REGISTER =
000897,000880: # (MAX 31.999) -9
000898,000881: # 2 RADIANS
000899,000882:
000900,000883:
000901,000884: # THAT-S ALL ON THE NOUNS.
000902,000885:
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Page 23
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000904,000887: # ALARM CODES FOR LUMINARY
000905,000888:
000906,000889: # *9 *18 *60 COLUMN
000907,000890:
000908,000891: # CODE * TYPE SET BY
000909,000892:
000910,000893: # 00105 ** AOTMARK SYSTEM IN USE
000911,000894: # 00107 MORE THAN 5 MARK PAIRS AOTMARK
000912,000895: # 00111 MARK MISSING AOTMARK
000913,000896: # 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
000914,000897: # 00113 NO INBITS AOTMARK
000915,000898: # 00114 MARK MADE BUT NOT DESIRED AOTMARK
000916,000899: # 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
000917,000900: # 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING
000918,000901: # 00206 + GIMBAL LOCK.
000919,000902: # 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
000920,000903: # 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51, P57
000921,000904: # 00211 COARSE ALIGN ERROR IMU MODE SWITCH
000922,000905: # 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH, T4RPT
000923,000906: # 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
000924,000907: # 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
000925,000908: # 00217 BAD RETURN FROM IMUSTALL P51, P52, P57
000926,000909: # 00220 IMU NOT ALIGNED - NO REFSMMAT R02, R47
000927,000910: # 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
000928,000911: # FINDCDUW
000929,000912: # 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
000930,000913: # 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
000931,000914: # 00405 TWO STARS NOT AVAILABLE P52
000932,000915: # 00421 W-MATRIX OVERFLOW INTEGRV
000933,000916: # 00430 ** ACCELERATION OVERFLOW IN INTEGRATION ORBITAL INTEGRATION
000934,000917: # 00501 P RADAR ANTENNA OUT OF LIMITS R23
000935,000918: # 00502 BAD RADAR GIMBAL ANGLE INPUT V41N72
000936,000919: # 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V41N72
000937,000920: # 00510 RADAR AUTO DESCRETE NOT PRESENT R25
000938,000921: # 00511 LR NOT IN POSITION 2 OR REPOSITIONING SERVICER
000939,000922: # 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
000940,000923: # 00515 RR CDU FAIL DISCRETE PRESENT R25
000941,000924: # 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
000942,000925: # 00521 COULD NOT READ RADAR P20
000943,000926: # 00522 LANDING RADAR POSITION CHANGE RADAR READ
000944,000927: # 00523 P LR ANTENNA DIDN'T ACHIEVE POSITION 2 SERVICER, V60 (NON-P IN V60)
000945,000928: # 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
000946,000929: # 00526 P RANGE GREATER THAN 400 NAUT. MILES P20, P22
000947,000930: # 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21, R24
000948,000931: # LUNAR SURFACE
000949,000932: # OR VEHICLE MANEUVER REQUIRED R24 (20)
000950,000933: # 00530 P LOS NOT IN MODE2 COVERAGE R21
000951,000934: # ON LUNAR SURFACE AFTER 600 SECS.
000952,000935: # 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
000953,000936: # 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32, P72,
000954,000937:
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000956,000939:
000957,000940: # 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32, P72,
000958,000941: # 00603 CSI TO CDH TIME LT TMIN12 P32, P72, P33, P73
000959,000942: # 00604 CDH TO TPI TIME LT TMIN23 P32, P72,
000960,000943: # OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
000961,000944: # 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
000962,000945: # 00606 DV EXCEEDS MAXIMUM P32,P72,
000963,000946: # 00607 ** NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET, TIMERAD
000964,000947: # 00611 NO TIG FOR GIVEN ELEV ANGLE P34, P74
000965,000948: # 00701 ILLEGAL OPTION CODE SELECTED P57
000966,000949: # 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
000967,000950: # 01102 AGC SELF TEST ERROR SELF CHECK
000968,000951: # 01103 ** UNUSED CCS BRANCH EXECUTED ABORT
000969,000952: # 01104 * DELAY ROUTINE BUSY EXEC
000970,000953: # 01105 DOWNLINK TOO FAST T4RUPT
000971,000954: # 01106 UPLINK TOO FAST T4RUPT
000972,000955: # 01107 PHASE TABLE FAILURE. ASSUME RESTART
000973,000956: # ERASABLE MEMORY IS SUSPECT. RESTART
000974,000957: # 01201 * EXECUTIVE OVERFLOW - NO VAC AREAS EXEC
000975,000958: # 01202 * EXECUTIVE OVERFLOW - NO CORE SETS EXEC
000976,000959: # 01203 * WAITLIST OVERFLOW - TOO MANY TASKS WAITLIST
000977,000960: # 01204 ** WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
000978,000961: # CALLED WITH ZERO OR NEGATIVE DELTA-TIME
000979,000962: # 01206 ** SECOND JOB ATTEMPTS TO GO TO SLEEP PINBALL
000980,000963: # 01206 VIA KYBD AND DISPLAY PROGRAM
000981,000964: # 01207 * NO VAC AREAS FOR MARKS AOTMARK
000982,000965: # 01210 * TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
000983,000966: # 01211 * ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
000984,000967: # 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
000985,000968: # 01302 ** SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
000986,000969: # 01406 BAD RETURN FROM ROOTPSRS DESCENT GUIDANCE EQS.
000987,000970: # 01406 ** BAD RETURN FROM ROOTPSRS IGNITION ALGORITHM
000988,000971:
000989,000972: # NOTE: 1406 IS A POODOO DURING THE IGNITION ALGORITHM
000990,000973: # AND AN ALARM DURING THE ACTUAL GUIDANCE PHASE.
000991,000974:
000992,000975: # 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
000993,000976: # .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
000994,000977: # VECTOR.) S40.8
000995,000978: # 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
000996,000979: # 01412 DESCENT IGNALG NOT CONVERGING P63
000997,000980: # 01501 ** KEYBOARD AND DISPLAY ALARM DURING PINBALL
000998,000981: # 01501 INTERNAL USE (NVSUB). ABORT
000999,000982: # 01502 ** ILLEGAL FLASHING DISPLAY GOPLAY
001000,000983: # 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
001001,000984: # 01600 OVERFLOW IN DRIFT TEST IMU 4
001002,000985: # 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
001003,000986: # 01601 IMU 4 (LEM)
001004,000987: # 01703 IGNITION TIME SLIPPED MIDTOAVE
001005,000988: # 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
001006,000989: # CONFIGURATION P40, P42
001007,000990:
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001009,000992:
001010,000993: # 02000 * DAP STILL IN PROGRESS AT NEXT TIME5 RUPT DAP
001011,000994: # 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
001012,000995: # 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
001013,000996: # 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
001014,000997: # 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
001015,000998: # 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
001016,000999: # 04777 ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001017,001000: # 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
001018,001001: # 10777 IMU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001019,001002: # 13777 IMU, ICDU FAILS CAUSED THE ISS WARNING T4RUPT
001020,001003: # 14777 IMU, ICDU, PIPA FAILS CAUSED THE ISSWNING T4RUPT
001021,001004:
001022,001005: # * INDICATES AN ABORT CODE THAT RESULTS IN A SOFTWARE RESTART.
001023,001006:
001024,001007: # ** INDICATES A MORE SERIOUS ABORT CODE THAT RESULTS IN THE
001025,001008: # PROGRAM GOING TO R00.
001026,001009:
001027,001010: # P INDICATES A PRIORITY ALARM.
001028,001011:
001029,001012: # ALL OTHERS ARE NON-ABORTIVE
001030,001013:
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001032,001015:
001033,001016: # CHECKLIST CODES FOR LUMINARY
001034,001017:
001035,001018: # *9 *17 *26 *9 COLUMN
001036,001019:
001037,001020: # R1CODE ACTION TO BE EFFECTED PROGRAM
001038,001021:
001039,001022: # 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
001040,001023: # 00014 PROCEED DO IMU FINE ALIGN ROUTINE P51, P63, P57
001041,001024: # 00014 ENTER DO LANDING SITE DETERMINATION (N89DISP) P57OPTION2
001042,001025: # 00015 PERFORM CELESTIAL BODY ACQUISITION R51, P51
001043,001026: # 00062 SWITCH AGC POWER DOWN P06
001044,001027: # 00201 SWITCH RR MODE TO AUTOMATIC P20, P22, R04
001045,001028: # 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12, P42, P71
001046,001029: # ALSO THR CONT TO AUTO P40, P63, P70
001047,001030: # 00205 PERFORM MANUAL ACQUISITION OF RR R23
001048,001031: # 00500 SWITCH LR ANTENNA TO POSITION 1 P63
001049,001032:
001050,001033: # SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
001051,001034: # PERFORM DENOTES START OR END OF A TASK
001052,001035: # KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
001053,001036:
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001055,001038: # OPTION CODES FOR LUMINARY
001056,001039:
001057,001040: # THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
001058,001041: # CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
001059,001042: # ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
001060,001043:
001061,001044: # *9 *17 *52 *11 *25 COLUMN
001062,001045:
001063,001046: # OPTION
001064,001047: # CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
001065,001048:
001066,001049: # 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
001067,001050: # 4=LAND SITE
001068,001051: # 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
001069,001052: # 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
001070,001053: # 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
001071,001054: # 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
001072,001055: # 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
001073,001056: # 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
001074,001057: # 2=TWO BODIES 3=ONE BODY + G
001075,001058: # 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
001076,001059: # ORBIT TO PASS OVER LM
001077,001060:
End of include-file ASSEMBLY_AND_OPERATION_INFORMATION.agc. Parent file is MAIN.agc