Source Code
|
These source-code files are part of a reconstructed copy of Luminary 173, the
second (unflown) release of the Apollo 14 Lunar Module (LM) Apollo Guidance
Computer (AGC) software.
The reconstruction began with reconstructed source code for Luminary 178. Changes
between revision 173 and 178 were backed out, as described by Luminary memo 167
(revision 1). The reconstruction was verified by matching memory-bank checksums
to those listed in drawing 2021152N. Note that page numbers in the reconstructed
code match those for the baseline log section mentioned in each file's changelog;
the page numbers for a real Luminary 173 listing would be different.
Comments from the original source code are prefixed with a single '#' symbol,
whereas comments added later are prefixed by "##" or "###". Report any errors
noted by creating an
issue report at the Virtual AGC
project's GitHub repository.
|
000054,000002: ## Copyright: Public domain.
000055,000003: ## Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
000056,000004: ## Purpose: A section of Luminary revision 173.
000057,000005: ## It is part of the reconstructed source code for the second
000058,000006: ## (unflown) release of the flight software for the Lunar
000059,000007: ## Module's (LM) Apollo Guidance Computer (AGC) for Apollo 14.
000060,000008: ## The code has been recreated from a reconstructed copy of
000061,000009: ## Luminary 178, as well as Luminary memo 167 (revision 1).
000062,000010: ## It has been adapted such that the resulting bugger words
000063,000011: ## exactly match those specified for Luminary 173 in NASA
000064,000012: ## drawing 2021152N, which gives relatively high confidence
000065,000013: ## that the reconstruction is correct.
000066,000014: ## Reference: pp. 2-27
000067,000015: ## Assembler: yaYUL
000068,000016: ## Contact: Ron Burkey <info@sandroid.org>.
000069,000017: ## Website: www.ibiblio.org/apollo/index.html
000070,000018: ## Mod history: 2019-09-18 MAS Created from Luminary 178.
000071,000019: ## 2019-09-21 MAS Removed VELOCITY5 (ZZ) scaling and gave
000072,000020: ## FORVEL its original CC scaling.
000073,000021:
|
|
Page 2
|
000075,000023: # THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
000076,000024: # THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
000077,000025:
000078,000026:
000079,000027: # GUIDANCE SYSTEM OPERATIONS PLAN
000080,000028: # FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
000081,000029: # USING PROGRAM LUMINARY
000082,000030:
000083,000031:
000084,000032: # THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
000085,000033: # TECHNOLOGY 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS UNDER PROJECT55-238-70, SPONSORED BY THE MANNED
000086,000034: # SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065.
000087,000035:
000088,000036:
000089,000037: # THIS PROGRAM IS REFERRED TO AS LUMINARY 1D
000090,000038:
000091,000039: # TABLE OF LOG CARDS
000092,000040:
000093,000041: # ABSOLUTE ADDRESSES FOR UPDATE PROGRAM
000094,000042: # ASSEMBLY AND OPERATION INFORMATION
000095,000043: # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
000096,000044: # CONTROLLED CONSTANTS
000097,000045: # INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
000098,000046: # FLAGWORD ASSIGNMENTS
000099,000047: # SUBROUTINE CALLS
000100,000048:
000101,000049:
000102,000050: # TABLE OF SUBROUTINE LOG SECTIONS
000103,000051: # LUMERASE
000104,000052: # ERASABLE ASSIGNMENTS
000105,000053: # LEMONAID
000106,000054: # INTERRUPT LEAD INS
000107,000055: # T4RUPT PROGRAM
000108,000056: # RCS FAILURE MONITOR
000109,000057: # DOWNLINK LISTS
000110,000058: # AGS INITIALIZATION
000111,000059: # FRESH START AND RESTART
000112,000060: # RESTART TABLES
000113,000061: # AOTMARK
000114,000062: # EXTENDED VERBS
000115,000063: # PINBALL NOUN TABLES
000116,000064: # LEM GEOMETRY
000117,000065: # IMU COMPENSATION PACKAGE
000118,000066: # R63
000119,000067: # ATTITUDE MANEUVER ROUTINE
000120,000068: # GIMBAL LOCK AVOIDANCE
000121,000069: # KALCMANU STEERING
000122,000070: # SYSTEM TEST STANDARD LEAD INS
000123,000071: # IMU PERFORMANCE TESTS 2
000124,000072: # IMU PERFORMANCE TESTS 4
|
|
Page 3
|
000126,000074: # PINBALL GAMES BUTTONS AND LIGHTS
000127,000075: # R60,R62
000128,000076: # S-BAND ANTENNA FOR LM
000129,000077: # LEMP20S
000130,000078: # RADAR LEADIN ROUTINES
000131,000079: # P20-P25
000132,000080: # LEMP30S
000133,000081: # P30,P37
000134,000082: # P32-P35, P72-P75
000135,000083: # KISSING
000136,000084: # GROUND TRACKING DETERMINATION PROGRAM - P21
000137,000085: # P34-P35, P74-P75
000138,000086: # R31
000139,000087: # P76
000140,000088: # R30
000141,000089: # FLY
000142,000090: # BURN, BABY, BURN -- MASTER IGNITION ROUTINE
000143,000091: # P40-P47
000144,000092: # THE LUNAR LANDING
000145,000093: # THROTTLE CONTROL ROUTINES
000146,000094: # LUNAR LANDING GUIDANCE EQUATIONS
000147,000095: # P70-P71
000148,000096: # P12
000149,000097: # ASCENT GUIDANCE
000150,000098: # SERVICER
000151,000099: # LANDING ANALOG DISPLAYS
000152,000100: # FINDCDUW - GUIDAP INTERFACE
000153,000101: # LEMP50S
000154,000102: # P51-P53
000155,000103: # LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
000156,000104: # SKIPPER
000157,000105: # DOWN-TELEMETRY PROGRAM
000158,000106: # INTER-BANK COMMUNICATION
000159,000107: # INTERPRETER
000160,000108: # FIXED-FIXED CONSTANT POOL
000161,000109: # INTERPRETIVE CONSTANTS
000162,000110: # SINGLE PRECISION SUBROUTINES
000163,000111: # EXECUTIVE
000164,000112: # WAITLIST
000165,000113: # LATITUDE LONGITUDE SUBROUTINES
000166,000114: # PLANETARY INERTIAL ORIENTATION
000167,000115: # MEASUREMENT INCORPORATION
000168,000116: # CONIC SUBROUTINES
000169,000117: # INTEGRATION INITIALIZATION
000170,000118: # ORBITAL INTEGRATION
000171,000119: # INFLIGHT ALIGNMENT ROUTINES
000172,000120: # POWERED FLIGHT SUBROUTINES
000173,000121: # TIME OF FREE FALL
000174,000122: # AGC BLOCK TWO SELF-CHECK
000175,000123: # PHASE TABLE MAINTENANCE
|
|
Page 4
|
000177,000125: # RESTARTS ROUTINE
000178,000126: # IMU MODE SWITCHING ROUTINES
000179,000127: # KEYRUPT, UPRUPT
000180,000128: # DISPLAY INTERFACE ROUTINES
000181,000129: # SERVICE ROUTINES
000182,000130: # ALARM AND ABORT
000183,000131: # UPDATE PROGRAM
000184,000132: # RTB OP CODES
000185,000133: # LMDAP
000186,000134: # T6-RUPT PROGRAMS
000187,000135: # DAP INTERFACE SUBROUTINES
000188,000136: # DAPIDLER PROGRAM
000189,000137: # P-AXIS RCS AUTOPILOT
000190,000138: # Q,R-AXIS RCS AUTOPILOT
000191,000139: # TJET LAW
000192,000140: # KALMAN FILTER
000193,000141: # TRIM GIMBAL CONTROL SYSTEM
000194,000142: # AOSTASK AND AOSJOB
000195,000143: # SPS BACK-UP RCS CONTROL
000196,000144:
000197,000145:
000198,000146: # SYMBOL TABLE LISTING
000199,000147: # UNREFERENCED SYMBOL LISTING
000200,000148: # ERASABLE & EQUALS CROSS-REFERENCE TABLE
000201,000149: # SUMMARY OF SYMBOL TABLE LISTINGS
000202,000150: # MEMORY TYPE & AVAILABLITY DISPLAY
000203,000151: # COUNT TABLE
000204,000152: # PARAGRAPHS GENERATED FOR THIS ASSEMBLY
000205,000153: # OCTAL LISTING
000206,000154: # OCCUPIED LOCATIONS TABLE
000207,000155: # SUBROS CALLED & PROGRAM STATUS
000208,000156:
|
|
Page 5
|
000210,000158: # VERB LIST FOR LUMINARY
000211,000159:
000212,000160: # REGULAR VERBS
000213,000161:
000214,000162: # 00 NOT IN USE
000215,000163: # 01 DISPLAY OCTAL COMP 1 IN R1
000216,000164: # 02 DISPLAY OCTAL COMP 2 IN R1
000217,000165: # 03 DISPLAY OCTAL COMP 3 IN R1
000218,000166: # 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
000219,000167: # 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
000220,000168: # 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000221,000169: # 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
000222,000170: # 08
000223,000171: # 09
000224,000172: # 10
000225,000173: # 11 MONITOR OCTAL COMP 1 IN R1
000226,000174: # 12 MONITOR OCTAL COMP 2 IN R1
000227,000175: # 13 MONITOR OCTAL COMP 3 IN R1
000228,000176: # 14 MONITOR OCTAL COMP 1,2 IN R1,R2
000229,000177: # 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
000230,000178: # 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000231,000179: # 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
000232,000180: # 18
000233,000181: # 19
000234,000182: # 20
000235,000183: # 21 LOAD COMPONENT 1 INTO R1
000236,000184: # 22 LOAD COMPONENT 2 INTO R2
000237,000185: # 23 LOAD COMPONENT 3 INTO R3
000238,000186: # 24 LOAD COMPONENT 1,2 INTO R1,R2
000239,000187: # 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
000240,000188: # 26
000241,000189: # 27 DISPLAY FIXED MEMORY
000242,000190: # 28
000243,000191: # 29
000244,000192: # 30 REQUEST EXECUTIVE
000245,000193: # 31 REQUEST WAITLIST
000246,000194: # 32 RECYCLE PROGRAM
000247,000195: # 33 PROCEED WITHOUT DSKY INPUTS
000248,000196: # 34 TERMINATE FUNCTION
000249,000197: # 35 TEST LIGHTS
000250,000198: # 36 REQUEST FRESH START
000251,000199: # 37 CHANGE PROGRAM (MAJOR MODE)
000252,000200: # 38
000253,000201: # 39
000254,000202:
|
|
Page 6
|
000256,000204: # EXTENDED VERBS
000257,000205:
000258,000206: # 40 ZERO CDU-S
000259,000207: # 41 COARSE ALIGN CDU-S
000260,000208: # 42 FINE ALIGN IMU
000261,000209: # 43 LOAD IMU ATT ERROR METERS
000262,000210: # 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
000263,000211: # 45
000264,000212: # 46
000265,000213: # 47 INITIALIZE AGS (R47)
000266,000214: # 48 REQUEST DAP DATA LOAD ROUTINE (R03)
000267,000215: # 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
000268,000216: # 50 PLEASE PERFORM
000269,000217: # 51
000270,000218: # 52 MARK X-RETICLE
000271,000219: # 53 MARK Y-RETICLE
000272,000220: # 54 MARK X OR Y-RETICLE
000273,000221: # 55 INCREMENT AGC TIME (DECIMAL)
000274,000222: # 56 TERMINATE TRACKING (P20 + P25)
000275,000223: # 57 PERMIT LANDING RADAR UPDATES
000276,000224: # 58 INHIBIT LANDING RADAR UPDATES
000277,000225: # 59 COMMAND LR TO POSITION 2.
000278,000226: # 60 DISPLAY VEHICLE ATTITUDE RATES ON FDAI ERROR NEEDLES.
000279,000227: # 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
000280,000228: # 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
000281,000229: # 63 SAMPLE RADAR ONCE PER SECOND (R04).
000282,000230: # 64 REQUEST S-BAND ANTENNA ROUTINE (R05)
000283,000231: # 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
000284,000232: # 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
000285,000233: # 67 DISPLAY W MATRIX
000286,000234: # 68 DISABLE TERRAIN MODEL
000287,000235: # 69 CAUSE RESTART
000288,000236: # 70 UPDATE LIFTOFF TIME
000289,000237: # 71 UNIVERSAL UPDATE-BLOCK ADR
000290,000238: # 72 UNIVERSAL UPDATE-SINGLE ADR
000291,000239: # 73 UPDATE AGC TIME (OCTAL)
000292,000240: # 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
000293,000241: # 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
000294,000242: # 76 MINIMUM IMPULSE COMMAND MODE
000295,000243: # 77 RATE COMMAND AND ATTITUDE HOLD MODE
000296,000244: # 78 LR SPURIOUS RETURN TEST START (R77)
000297,000245: # 79 LR SPURIOUS RETURN TEST STOP
000298,000246: # 80 UPDATE LEM STATE VECTOR
000299,000247: # 81 UPDATE CSM STATE VECTOR
000300,000248: # 82 REQUEST ORBIT PARAM DISPLAY (R30)
000301,000249: # 83 REQUEST REND PARAM DISPLAY (R31)
000302,000250: # 84
000303,000251: # 85 DISPLAY RR LOS AZ AND ELEV
000304,000252: # 86
000305,000253: # 87
|
|
Page 7
|
000307,000255: # 88
000308,000256: # 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
000309,000257: # 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
000310,000258: # 91 DISPLAY BANK SUM
000311,000259: # 92 OPERATE IMU PERFORMANCE TEST (P07)
000312,000260: # 93 ENABLE W MATRIX INITIALIZATION
000313,000261: # 94
000314,000262: # 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
000315,000263: # 96 INTERRUPT INTEGRATION AND GO TO POO
000316,000264: # 97 PERFORM ENGINE FAIL PROCEDURE
000317,000265: # 98
000318,000266: # 99 PLEASE ENABLE ENGINE
000319,000267:
|
|
Page 8
|
000321,000269: # IN THE FOLLOWING NOUN LIST THE :NO LOAD: RESTRICTION MEANS THE NOUN
000322,000270: # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
000323,000271: # SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
000324,000272: # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22 OR 23
000325,000273: # MAY BE USED TO LOAD ANY OF THE NOUN:S COMPONENTS WHICH ARE NOT OF THE
000326,000274: # ABOVE SCALE TYPES.
000327,000275: # THE :DEC ONLY: RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
000328,000276: # EVERY COMPONENT IN THE NOUN. (NOTE THAT :NO LOAD: IMPLIES :DEC ONLY:.)
000329,000277:
000330,000278: # NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000331,000279:
000332,000280: # 00 NOT IN USE
000333,000281: # 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .XXXXX FOR EACH
000334,000282: # 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP XXXXX. FOR EACH
000335,000283: # 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP XXX.XX DEG FOR EACH
000336,000284: # 04 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000337,000285: # 05 ANGULAR ERROR/DIFFERENCE 1COMP XXX.XX DEG
000338,000286: # 06 OPTION CODE 3COMP OCTAL ONLY FOR EACH
000339,000287: # LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
000340,000288: # 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
000341,000289: # ONES FOR BITS TO BE MODIFIED
000342,000290: # 1 TO SET OR 0 TO RESET SELECTED BITS
000343,000291: # 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
000344,000292: # 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
000345,000293: # 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
000346,000294: # 11 TIG OF CSI 3COMP 00XXX. HRS DEC ONLY
000347,000295: # 000XX. MIN MUST LOAD 3 COMPS
000348,000296: # 0XX.XX SEC
000349,000297: # 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
000350,000298: # (USED BY EXTENDED VERBS ONLY)
000351,000299: # 13 TIG OF CDH 3COMP 00XXX. HRS DEC ONLY
000352,000300: # 000XX. MIN MUST LOAD 3 COMPS
000353,000301: # 0XX.XX SEC
000354,000302: # 14 CHECKLIST 3COMP XXXXX. FOR EACH
000355,000303: # (USED BY EXTENDED VERBS ONLY)
000356,000304: # (NOUN 25 IS PASTED AFTER DISPLAY)
000357,000305: # 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
000358,000306: # 16 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000359,000307: # (USED BY EXTENDED VERBS ONLY) 000XX. MIN MUST LOAD 3 COMPS
000360,000308: # 0XX.XX SEC
000361,000309: # 17 SPARE
000362,000310: # 18 AUTO MANEUVER BALL ANGLES 3COMP XXX.XX DEG FOR EACH
000363,000311: # 19 SPARE
000364,000312: # 20 ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000365,000313: # 21 PIPAS 3COMP XXXXX. PULSES FOR EACH
000366,000314: # 22 NEW ICDU ANGLES 3COMP XXX.XX DEG FOR EACH
000367,000315: # 23 SPARE
000368,000316: # 24 DELTA TIME FOR AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000369,000317: # 000XX. MIN MUST LOAD 3 COMPS
000370,000318: # 0XX.XX SEC
|
|
Page 9
|
000372,000320: # 25 CHECKLIST 3COMP XXXXX. FOR EACH
000373,000321: # (USED WITH PLEASE PERFORM ONLY)
000374,000322: # 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
000375,000323: # 27 SELF TEST ON/OFF SWITCH 1COMP XXXXX.
000376,000324: # 28 SPARE
000377,000325: # 29 SPARE
000378,000326: # 30 SPARE
000379,000327: # 31 SPARE
000380,000328: # 32 TIME FROM PERIGEE 3COMP 00XXX. HRS DEC ONLY
000381,000329: # 000XX. MIN MUST LOAD 3 COMPS
000382,000330: # 0XX.XX SEC
000383,000331: # 33 TIME OF IGNITION 3COMP 00XXX. HRS DEC ONLY
000384,000332: # 000XX. MIN MUST LOAD 3 COMPS
000385,000333: # 0XX.XX SEC
000386,000334: # 34 TIME OF EVENT 3COMP 00XXX. HRS DEC ONLY
000387,000335: # 000XX. MIN MUST LOAD 3 COMPS
000388,000336: # 0XX.XX SEC
000389,000337: # 35 TIME FROM EVENT 3COMP 00XXX. HRS DEC ONLY
000390,000338: # 000XX. MIN MUST LOAD 3 COMPS
000391,000339: # 0XX.XX SEC
000392,000340: # 36 TIME OF AGC CLOCK 3COMP 00XXX. HRS DEC ONLY
000393,000341: # 000XX. MIN MUST LOAD 3 COMPS
000394,000342: # 0XX.XX SEC
000395,000343: # 37 TIG OF TPI 3COMP 00XXX. HRS DEC ONLY
000396,000344: # 000XX. MIN MUST LOAD 3 COMPS
000397,000345: # 0XX.XX SEC
000398,000346: # 38 TIME OF STATE BEING INTEGRATED 3COMP 00XXX. HRS DEC ONLY
000399,000347: # 000XX. MIN MUST LOAD 3 COMPS
000400,000348: # 0XX.XX SEC
000401,000349: # 39 SPARE
000402,000350:
|
|
Page 10
|
000404,000352: # MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000405,000353:
000406,000354: # 40 TIME FROM IGNITION/CUTOFF 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000407,000355: # VG, XXXX.X FT/SEC
000408,000356: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000409,000357: # 41 TARGET AZIMUTH, 2COMP XXX.XX DEG (FOR SYSTEM TEST)
000410,000358: # ELEVATION XX.XXX DEG
000411,000359: # 42 APOGEE, 3COMP XXXX.X NAUT MI DEC ONLY
000412,000360: # PERIGEE, XXXX.X NAUT MI
000413,000361: # DELTA V (REQUIRED) XXXX.X FT/SEC
000414,000362: # 43 LATITUDE, 3COMP XXX.XX DEG DEC ONLY
000415,000363: # LONGITUDE, XXX.XX DEG
000416,000364: # ALTITUDE XXXX.X NAUT MI
000417,000365: # 44 APOGEE, 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000418,000366: # PERIGEE, XXXX.X NAUT MI
000419,000367: # TFF XXBXX MIN/SEC
000420,000368: # 45 MARKS, 3COMP XXXXX. NO LOAD, DEC ONLY
000421,000369: # TFI OF NEXT BURN XXBXX MIN/SEC
000422,000370: # MGA XXX.XX DEG
000423,000371: # 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
000424,000372: # 47 LEM WEIGHT, 2COMP XXXXX. LBS DEC ONLY
000425,000373: # CSM WEIGHT XXXXX. LBS
000426,000374: # 48 GIMBAL PITCH TRIM, 2COMP XXX.XX DEG DEC ONLY
000427,000375: # GIMBAL ROLL TRIM XXX.XX DEG
000428,000376: # 49 DELTA R, 3COMP XXXX.X NAUT MI DEC ONLY
000429,000377: # DELTA V, XXXX.X FT/SEC
000430,000378: # RADAR DATA SOURCE CODE XXXXX.
000431,000379: # 50 SPARE
000432,000380: # 51 S-BAND ANTENNA ANGLES PITCH 2COMP XXX.XX DEG DEC ONLY
000433,000381: # YAW XXX.XX DEG
000434,000382: # 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP XXX.XX DEG
000435,000383: # 53 SPARE
000436,000384: # 54 RANGE, 3COMP XXX.XX NAUT MI DEC ONLY
000437,000385: # RANGE RATE, XXXX.X FT/SEC
000438,000386: # THETA XXX.XX DEG
000439,000387: # 55 NO. OF APSIDAL CROSSINGS 3COMP XXXXX. DEC ONLY
000440,000388: # ELEVATION ANGLE XXX.XX DEG
000441,000389: # CENTRAL ANGLE OF PASSIVE VEHICLE XXX.XX DEG
000442,000390: # 56 RR LOS AZIMUTH 2COMP XXX.XX DEG
000443,000391: # ELEVATION XXX.XX DEG
000444,000392: # 57 SPARE
000445,000393: # 58 PERIGEE ALT (POST TPI) 3COMP XXXX.X NAUT MI DEC ONLY
000446,000394: # DELTA V TPI XXXX.X FT/SEC
000447,000395: # DELTA V TPF XXXX.X FT/SEC
000448,000396: # 59 DELTA VELOCITY LOS 3COMP XXXX.X FT/SEC FOR EA. DEC ONLY
000449,000397: # 60 FORWARD VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000450,000398: # ALTITUDE RATE XXXX.X FT/SEC
000451,000399: # COMPUTED ALTITUDE XXXXX. FEET
000452,000400: # 61 TIME TO GO IN BRAKING PHASE 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000453,000401: # TIME FROM IGNITION XXBXX MIN/SEC
|
|
Page 11
|
000455,000403: # CROSS RANGE DISTANCE XXXX.X NAUT MI
000456,000404: # 62 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC NO LOAD, DEC ONLY
000457,000405: # TIME FROM IGNITION XXBXX MIN/SEC
000458,000406: # DELTA V (ACCUMULATED) XXXX.X FT/SEC
000459,000407: # 63 ABSOLUTE VALUE OF VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000460,000408: # ALTITUDE RATE XXXX.X FT/SEC
000461,000409: # COMPUTED ALTITUDE XXXXX. FEET
000462,000410: # 64 TIME LEFT FOR REDESIGNATION- LPD ANGLE 3COMP XXBXX NO LOAD, DEC ONLY
000463,000411: # ALTITUDE RATE XXXX.X FT/SEC
000464,000412: # COMPUTED ALTITUDE XXXXX. FEET
000465,000413: # 65 SAMPLED AGC TIME 3COMP 00XXX. HRS DEC ONLY
000466,000414: # (FETCHED IN INTERRUPT) 000XX. MIN MUST LOAD 3 COMPS
000467,000415: # 0XX.XX SEC
000468,000416: # 66 LR RANGE 2COMP XXXXX. FEET NO LOAD, DEC ONLY
000469,000417: # POSITION +0000X
000470,000418: # 67 LRVX 3COMP XXXXX. FT/SEC
000471,000419: # LRVY XXXXX. FT/SEC
000472,000420: # LRVZ XXXXX. FT/SEC
000473,000421: # 68 SLANT RANGE TO LANDING SITE 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000474,000422: # TIME TO GO IN BRAKING PHASE XXBXX MIN/SEC
000475,000423: # LR ALTITUDE - COMPUTED ALTITUDE XXXXX. FEET
000476,000424: # 69 LANDING SITE CORRECTION, Z-COMPONENT 3COMP XXXXX. FEET DEC ONLY
000477,000425: # LANDING SITE CORRECTION, Y-COMPONENT XXXXX. FEET
000478,000426: # LANDING SITE CORRECTION, X-COMPONENT XXXXX. FEET
000479,000427: # 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000480,000428: # 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000481,000429: # 72 RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000482,000430: # SHAFT ANGLE XXX.XX DEG
000483,000431: # 73 NEW RR 360 - TRUNNION ANGLE 2COMP XXX.XX DEG
000484,000432: # SHAFT ANGLE XXX.XX DEG
000485,000433: # 74 TIME FROM IGNITION 3COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000486,000434: # YAW AFTER VEHICLE RISE XXX.XX DEG
000487,000435: # PITCH AFTER VEHICLE RISE XXX.XX DEG
000488,000436: # 75 DELTA ALTITUDE CDH 3COMP XXXX.X NAUT MI NO LOAD, DEC ONLY
000489,000437: # DELTA TIME (CDH-CSI OR TPI-CDH) XXBXX MIN/SEC
000490,000438: # DELTA TIME (TPI-CDH OR TPI-NOMTPI) XXBXX MIN/SEC
000491,000439: # 76 DESIRED HORIZONTAL VELOCITY 3COMP XXXX.X FT/SEC DEC ONLY
000492,000440: # DESIRED RADIAL VELOCITY XXXX.X FT/SEC
000493,000441: # CROSS-RANGE DISTANCE XXXX.X NAUT MI
000494,000442: # 77 TIME TO ENGINE CUTOFF 2COMP XXBXX MIN/SEC NO LOAD, DEC ONLY
000495,000443: # VELOCITY NORMAL TO CSM PLANE XXXX.X FT/SEC
000496,000444: # 78 RR RANGE 3COMP XXX.XX NAUT MI NO LOAD, DEC ONLY
000497,000445: # RANGE RATE XXXXX. FT/SEC
000498,000446: # TIME FROM IGNITION XXBXX MIN/SEC
000499,000447: # 79 CURSOR ANGLE 3COMP XXX.XX DEG DEC ONLY
000500,000448: # SPIRAL ANGLE XXX.XX DEG
000501,000449: # POSITION CODE XXXXX.
000502,000450: # 80 DATA INDICATOR, 2COMP XXXXX.
000503,000451: # OMEGA XXX.XX DEG
000504,000452: # 81 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
|
|
Page 12
|
000506,000454: # 82 DELTA V (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000507,000455: # 83 DELTA V (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000508,000456: # 84 DELTA V (OTHER VEHICLE) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000509,000457: # 85 VG (BODY) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000510,000458: # 86 VG (LV) 3COMP XXXX.X FT/SEC FOR EACH DEC ONLY
000511,000459: # 87 BACKUP OPTICS LOS AZIMUTH 2COMP XXX.XX DEG
000512,000460: # ELEVATION XXX.XX DEG
000513,000461: # 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .XXXXX FOR EACH DEC ONLY
000514,000462: # 89 LANDMARK LATITUDE 3COMP XX.XXX DEG DEC ONLY
000515,000463: # LONGITUDE/2 XX.XXX DEC
000516,000464: # ALTITUDE XXX.XX NAUT MI
000517,000465: # 90 Y 3COMP XXX.XX NM DEC ONLY
000518,000466: # Y DOT XXXX.X FPS
000519,000467: # PSI XXX.XX DEG
000520,000468: # 91 ALTITUDE 3COMP XXXXXB. NAUT MI
000521,000469: # VELOCITY XXXXX. FT/SEC
000522,000470: # FLIGHT PATH ANGLE XXX.XX DEG
000523,000471: # 92 PCT FTP(10,5KLB) AT PRESENT THRUST 3COMP XXXXX.
000524,000472: # ALTITUDE RATE XXXX.X FT/SEC
000525,000473: # COMPUTED ALTITUDE XXXXX.FEET
000526,000474: # 93 DELTA GYRO ANGLES 3COMP XX.XXX DEG FOR EACH
000527,000475: # 94 SPARE
000528,000476: # 95 SPARE
000529,000477: # 96 SPARE
000530,000478: # 97 SYSTEM TEST INPUTS 3COMP XXXXX. FOR EACH
000531,000479: # 98 SYSTEM TEST RESULTS AND INPUTS 3COMP XXXXX.
000532,000480: # .XXXXX
000533,000481: # XXXXX.
000534,000482: # 99 RMS IN POSITION 3COMP XXXXX.FT DEC ONLY
000535,000483: # RMS IN VELOCITY XXXX.X FT/SEC
000536,000484: # RMS IN BIAS XX.XXX RADIANS
000537,000485:
|
|
Page 13
|
000539,000487: # REGISTERS AND SCALING FOR NORMAL NOUNS
000540,000488:
000541,000489: # NOUN REGISTER SCALE TYPE
000542,000490:
000543,000491: # 00 NOT IN USE
000544,000492: # 01 SPECIFY ADDRESS B
000545,000493: # 02 SPECIFY ADDRESS C
000546,000494: # 03 SPECIFY ADDRESS D
000547,000495: # 04 DSPTEM1 H
000548,000496: # 05 DSPTEM1 H
000549,000497: # 06 OPTION1 A
000550,000498: # 07 XREG A
000551,000499: # 08 ALMCADR A
000552,000500: # 09 FAILREG A
000553,000501: # 10 SPECIFY CHANNEL A
000554,000502: # 11 TCSI K
000555,000503: # 12 OPTIONX A
000556,000504: # 13 TCDH K
000557,000505: # 14 DSPTEMX C
000558,000506: # 15 INCREMENT ADDRESS A
000559,000507: # 16 DSPTEMX K
000560,000508: # 17 SPARE
000561,000509: # 18 FDAIX D
000562,000510: # 19 SPARE
000563,000511: # 20 CDUX D
000564,000512: # 21 PIPAX C
000565,000513: # 22 THETAD D
000566,000514: # 23 SPARE
000567,000515: # 24 DSPTEM2 +1 K
000568,000516: # 25 DSPTEM1 C
000569,000517: # 26 DSPTEM1 A
000570,000518: # 27 SMODE C
000571,000519: # 28 SPARE
000572,000520: # 29 SPARE
000573,000521: # 30 SPARE
000574,000522: # 31 SPARE
000575,000523: # 32 -TPER K
000576,000524: # 33 TIG K
000577,000525: # 34 DSPTEM1 K
000578,000526: # 35 TTOGO K
000579,000527: # 36 TIME2 K
000580,000528: # 37 TTPI K
000581,000529: # 38 TET K
000582,000530: # 39 SPARE
000583,000531:
|
|
Page 14
|
000585,000533: # REGISTERS AND SCALING FOR MIXED NOUNS
000586,000534:
000587,000535: # NOUN COMP REGISTER SCALE TYPE
000588,000536:
000589,000537: # 40 1 TTOGO L
000590,000538: # 2 VGDISP S
000591,000539: # 3 DVTOTAL S
000592,000540: # 41 1 DSPTEM1 D
000593,000541: # 2 DSPTEM1 +1 E
000594,000542: # 42 1 HAPO Q
000595,000543: # 2 HPER Q
000596,000544: # 3 VGDISP S
000597,000545: # 43 1 LAT H
000598,000546: # 2 LONG H
000599,000547: # 3 ALT Q
000600,000548: # 44 1 HAPOX Q
000601,000549: # 2 HPERX Q
000602,000550: # 3 TFF L
000603,000551: # 45 1 TRKMKCNT C
000604,000552: # 2 TTOGO L
000605,000553: # 3 +MGA H
000606,000554: # 46 1 DAPDATR1 A
000607,000555: # 47 1 LEMMASS KK
000608,000556: # 2 CSMMASS KK
000609,000557: # 48 1 PITTIME NN
000610,000558: # 2 ROLLTIME NN
000611,000559: # 49 1 R22DISP Q
000612,000560: # 2 R22DISP +2 S
000613,000561: # 3 WHCHREAD C
000614,000562: # 50 SPARE
000615,000563: # 51 1 ALPHASB H
000616,000564: # 2 BETASB H
000617,000565: # 52 1 ACTCENT H
000618,000566: # 53 SPARE
000619,000567: # 54 1 RANGE JJ
000620,000568: # 2 RRATE S
000621,000569: # 3 RTHETA H
000622,000570: # 55 1 NN C
000623,000571: # 2 ELEV H
000624,000572: # 3 CENTANG H
000625,000573: # 56 1 RR-AZ H
000626,000574: # 2 RR-ELEV H
000627,000575: # 57 SPARE
000628,000576: # 58 1 POSTTPI Q
000629,000577: # 2 DELVTPI S
000630,000578: # 3 DELVTPF S
000631,000579: # 59 1 DVLOS S
000632,000580: # 2 DVLOS +2 S
000633,000581: # 3 DVLOS +4 S
000634,000582: # 60 1 FORVEL CC
|
|
Page 15
|
000636,000584: # 2 HDOTDISP S
000637,000585: # 3 HCALC1 RR
000638,000586: # 61 1 TTFDISP L
000639,000587: # 2 TTOGO L
000640,000588: # 3 OUTOFPLN QQ
000641,000589: # 62 1 ABVEL S
000642,000590: # 2 TTOGO L
000643,000591: # 3 DVTOTAL S
000644,000592: # 63 1 ABVEL S
000645,000593: # 2 HDOTDISP S
000646,000594: # 3 HCALC1 RR
000647,000595: # 64 1 FUNNYDSP PP
000648,000596: # 2 HDOTDISP S
000649,000597: # 3 HCALC RR
000650,000598: # 65 1 SAMPTIME K
000651,000599: # 2 SAMPTIME K
000652,000600: # 3 SAMPTIME K
000653,000601: # 66 1 RSTACK +6 W
000654,000602: # 2 CHANNEL 33 TT
000655,000603: # 67 1 RSTACK X
000656,000604: # 2 RSTACK +2 Y
000657,000605: # 3 RSTACK +4 Z
000658,000606: # 68 1 RANGEDSP QQ
000659,000607: # 2 TTFDISP L
000660,000608: # 3 DELTAH RR
000661,000609: # 69 1 DLANDZ RR
000662,000610: # 2 DLANDY RR
000663,000611: # 3 DLANDX RR
000664,000612: # 70 1 AOTCODE A
000665,000613: # 2 AOTCODE +1 A
000666,000614: # 3 AOTCODE +2 A
000667,000615: # 71 1 AOTCODE A
000668,000616: # 2 AOTCODE +1 A
000669,000617: # 3 AOTCODE +2 A
000670,000618: # 72 1 CDUT WW
000671,000619: # 2 CDUS D
000672,000620: # 73 1 TANG WW
000673,000621: # 2 TANG +1 D
000674,000622: # 74 1 TTOGO L
000675,000623: # 2 YAW H
000676,000624: # 3 PITCH H
000677,000625: # 75 1 DIFFALT Q
000678,000626: # 2 T1TOT2 L
000679,000627: # 3 T2TOT3 L
000680,000628: # 76 1 ZDOTD S
000681,000629: # 2 RDOTD S
000682,000630: # 3 XRANGE Q
000683,000631: # 77 1 TTOGO L
000684,000632: # 2 YDOT S
000685,000633: # 78 1 DNRRANGE U
|
|
Page 16
|
000687,000635: # 2 DNRRDOT V
000688,000636: # 3 TTOTIG L
000689,000637: # 79 1 CURSOR D
000690,000638: # 2 SPIRAL D
000691,000639: # 3 POSCODE C
000692,000640: # 80 1 DATAGOOD C
000693,000641: # 2 OMEGAD H
000694,000642: # 81 1 DELVLVC S
000695,000643: # 2 DELVLVC +2 S
000696,000644: # 3 DELVLVC +4 S
000697,000645: # 82 1 DELVLVC S
000698,000646: # 2 DELVLVC +2 S
000699,000647: # 3 DELVLVC +4 S
000700,000648: # 83 1 DELVIMU S
000701,000649: # 2 DELVIMU +2 S
000702,000650: # 3 DELVIMU +4 S
000703,000651: # 84 1 DELVOV S
000704,000652: # 2 DELVOV +2 S
000705,000653: # 3 DELVOV +4 S
000706,000654: # 85 1 VGBODY S
000707,000655: # 2 VGBODY +2 S
000708,000656: # 3 VGBODY +4 S
000709,000657: # 86 1 DELVLVC S
000710,000658: # 2 DELVLVC +2 S
000711,000659: # 3 DELVLVC +4 S
000712,000660: # 87 1 AZ D
000713,000661: # 2 EL D
000714,000662: # 88 1 STARAD B
000715,000663: # 2 STARAD +2 B
000716,000664: # 3 STARAD +4 B
000717,000665: # 89 1 LANDLAT G
000718,000666: # 2 LANDLONG G
000719,000667: # 3 LANDALT JJ
000720,000668: # 90 1 RANGE JJ
000721,000669: # 2 RRATE S
000722,000670: # 3 RTHETA H
000723,000671: # 91 1 P21ALT Q (MEMORY/100 TO DIPLAY TENS N.M.)
000724,000672: # 2 P21VEL P
000725,000673: # 3 P21GAM H
000726,000674: # 92 1 THRDISP C
000727,000675: # 2 HDOTDISP S
000728,000676: # 3 HCALC1 RR
000729,000677: # 93 1 OGC G
000730,000678: # 2 OGC +2 G
000731,000679: # 3 OGC +4 G
000732,000680: # 94 SPARE
000733,000681: # 95 SPARE
000734,000682: # 96 SPARE
000735,000683: # 97 1 DSPTEM1 C
000736,000684: # 2 DSPTEM1 +1 C
|
|
Page 17
|
000738,000686: # 3 DSPTEM1 +2 C
000739,000687: # 98 1 DSPTEM2 C
000740,000688: # 2 DSPTEM2 +1 B
000741,000689: # 3 DSPTEM2 +2 C
000742,000690: # 99 1 WWPOS XX
000743,000691: # 2 WWVEL YY
000744,000692: # 3 WWBIAS AAA
000745,000693:
|
|
Page 18
|
000747,000695: # NOUN SCALES AND FORMATS
000748,000696:
000749,000697: # -SCALE TYPE- PRECISION
000750,000698: # UNITS DECIMAL FORMAT -- AGC FORMAT
000751,000699: # ------------ -------------- -- ----------
000752,000700:
000753,000701: # -A-
000754,000702: # OCTAL XXXXX SP OCTAL
000755,000703:
000756,000704: # -B- -14
000757,000705: # FRACTIONAL .XXXXX SP BIT 1 = 2 UNITS
000758,000706: # (MAX .99996)
000759,000707:
000760,000708: # -C-
000761,000709: # WHOLE XXXXX. SP BIT 1 = 1 UNIT
000762,000710: # (MAX 16383.)
000763,000711:
000764,000712: # -D- 15
000765,000713: # CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360/2 DEGREES
000766,000714: # (MAX 359.99) (USES 15 BITS FOR MAGNI-
000767,000715: # TUDE AND 2-S COMP.)
000768,000716:
000769,000717: # -E- 14
000770,000718: # ELEVATION DEGREES XX.XXX DEGREES SP BIT 1 = 90/2 DEGREES
000771,000719: # (MAX 89.999)
000772,000720:
000773,000721: # -F- 14
000774,000722: # DEGREES (180) XXX.XX DEGREES SP BIT 1 = 180/2 DEGREES
000775,000723: # (MAX 179.99)
000776,000724:
000777,000725: # -G-
000778,000726: # DP DEGREES(90) XX.XXX DEGREES DP BIT 1 OF LOW REGISTER =
000779,000727: # 28
000780,000728: # 360/2 DEGREES
000781,000729:
000782,000730: # -H-
000783,000731: # DP DEGREES (360) XXX.XX DEGREES DP BIT 1 OF LOW REGISTER =
000784,000732: # 28
000785,000733: # (MAX 359.99) 360/2 DEGREES
000786,000734:
|
|
Page 19
|
000788,000736: # -K-
000789,000737: # TIME (HR, MIN, SEC) 00XXX. HR DP BIT 1 OF LOW REGISTER =
000790,000738: # 000XX. MIN -2
000791,000739: # 0XX.XX SEC 10 SEC
000792,000740: # (DECIMAL ONLY.
000793,000741: # MAX MIN COMP=59
000794,000742: # MAX SEC COMP=59.99
000795,000743: # MAX CAPACITY=745 HRS
000796,000744: # 39 MINS
000797,000745: # 14.55 SECS.
000798,000746: # WHEN LOADING, ALL 3
000799,000747: # COMPONENTS MUST BE
000800,000748: # SUPPLIED.)
000801,000749:
000802,000750: # -L-
000803,000751: # TIME (MIN/SEC) XXBXX MIN/SEC DP BIT 1 OF LOW REGISTER =
000804,000752: # (B IS A BLANK -2
000805,000753: # POSITION, DECIMAL 10 SEC
000806,000754: # ONLY, DISPLAY OR
000807,000755: # MONITOR ONLY. CANNOT
000808,000756: # BE LOADED.
000809,000757: # MAX MIN COMP=59
000810,000758: # MAX SEC COMP=59
000811,000759: # VALUES GREATER THAN
000812,000760: # 59 MIN 59 SEC
000813,000761: # ARE DISPLAYED AS
000814,000762: # 59 MIN 59 SEC.)
000815,000763:
000816,000764: # -M- -2
000817,000765: # TIME (SEC) XXX.XX SEC SP BIT 1 = 10 SEC
000818,000766: # (MAX 163.83)
000819,000767:
000820,000768: # -N-
000821,000769: # TIME(SEC) DP XXX.XX SEC DP BIT 1 OF LOW REGISTER =
000822,000770: # -2
000823,000771: # 10 SEC
000824,000772:
000825,000773: # -P-
000826,000774: # VELOCITY 2 XXXXX. FEET/SEC DP BIT 1 OF HIGH REGISTER =
000827,000775: # (MAX 41994.) -7
000828,000776: # 2 METERS/CENTI-SEC
000829,000777:
000830,000778: # -Q-
000831,000779: # POSITION 4 XXXX.X NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
000832,000780: # 2 METERS
000833,000781:
000834,000782: # -S-
000835,000783: # VELOCITY 3 XXXX.X FT/SEC DP BIT 1 OF HIGH REGISTER =
000836,000784: # -7
000837,000785: # 2 METERS/CENTI-SEC
000838,000786:
|
|
Page 20
|
000840,000788: # -T- -2
000841,000789: # G XXX.XX G SP BIT 1 = 10 G
000842,000790: # (MAX 163.83)
000843,000791:
000844,000792: # -U-
000845,000793: # RENDEZVOUS XXX.XX NAUT MI SP USES 15 BITS FOR UNSIGNED
000846,000794: # RADAR RANGE (DECIMAL ONLY. MAGNITUDE.
000847,000795: # DISPLAY OR MONITOR BIT 1 = 9.38 FEET
000848,000796: # ONLY. CANNOT BE
000849,000797: # LOADED.)
000850,000798:
000851,000799: # -V-
000852,000800: # RENDEZVOUS XXXXX. FEET/SEC SP USES 15 BITS FOR UNSIGNED
000853,000801: # RADAR RANGE RATE (DECIMAL ONLY. MAGNITUDE.
000854,000802: # DISPLAY OR MONITOR BIT 1 = -.6278 FEET/SEC
000855,000803: # ONLY. CANNOT BE
000856,000804: # LOADED.
000857,000805: # BIAS OF 17000 COUNTS
000858,000806: # SUBTRACTED BEFORE
000859,000807: # DISPLAY.)
000860,000808:
000861,000809: # -W-
000862,000810: # LANDING RADAR XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000863,000811: # ALTITUDE WORD = 1.079 FEET
000864,000812:
000865,000813: # -X-
000866,000814: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000867,000815: # VELX WORD = -.6440 FEET/SEC
000868,000816:
000869,000817: # -Y-
000870,000818: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000871,000819: # VELY WORD = 1.212 FEET/SEC
000872,000820:
000873,000821: # -Z-
000874,000822: # LANDING RADAR XXXXX. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000875,000823: # VELZ WORD = .8668 FEET/SEC
000876,000824:
000877,000825: # -AA-
000878,000826: # INITIAL/FINAL XXXXX. FEET DP LOW ORDER BIT OF LOW ORDER
000879,000827: # ALTITUDE WORD = 2.345 FEET
000880,000828:
000881,000829: # -BB-
000882,000830: # ALTITUDE RATE XXXXX. FEET/SEC SP LOW ORDER BIT = .5
000883,000831: # (MAX 08191.) FEET/SEC
000884,000832:
000885,000833: # -CC-
000886,000834: # FORWARD/LATERAL XXXX.X FEET/SEC SP LOW ORDER BIT = .5571
000887,000835: # VELOCITY (MAX 09126.) FEET/SEC
000888,000836:
000889,000837: # -DD-
|
|
Page 21
|
000891,000839: # ROTATIONAL HAND XXXXX. DEG/SEC SP FRACTIONAL PART OF PI RAD
000892,000840: # CONTROLLER ANGULAR (MAX 00044.) 4 SEC
000893,000841: # RATES
000894,000842:
000895,000843: # -EE-
000896,000844: # OPTICAL TRACKER XXX.XX DEG. DP LOW ORDER BIT OF LOW ORDER
000897,000845: # AZIMUTH ANGLE 15
000898,000846: # WORD = 360/2 DEGREES
000899,000847:
000900,000848: # -JJ-
000901,000849: # POSITION5 XXX.XX NAUT MI DP BIT 1 OF LOW REGISTER =
000902,000850: # 2 METERS
000903,000851:
000904,000852: # -KK- 16
000905,000853: # WEIGHT2 XXXXX. LBS SP FRACTIONAL PART OF 2 KG
000906,000854:
000907,000855: # -NN-
000908,000856: # TRIM DEGREES 2 XXX.XX DEG SP BIT 1=.01SEC(TIME)
000909,000857: # (MAX 032.76)
000910,000858:
000911,000859: # -PP-
000912,000860: # 2 INTEGERS +XXBYY DP BIT 1 OF HIGH REGISTER =
000913,000861: # (B IS A BLANK 1 UNIT OF XX
000914,000862: # POSITION. DECIMAL BIT 1 OF LOW REGISTER =
000915,000863: # ONLY, DISPLAY OR 1 UNIT OF YY
000916,000864: # MONITOR ONLY. CANNOT (EACH REGISTER MUST
000917,000865: # BE LOADED.) CONTAIN A POSITIVE INTEGER
000918,000866: # (MAX 99B99) LESS THAN 100)
000919,000867:
000920,000868: # -QQ-
000921,000869: # POSITION7 XXXX.X NAUT MI DP BIT 1 OF LOW REGISTER =
000922,000870: # (MAX 9058.9) -4
000923,000871: # 2 METERS
000924,000872:
000925,000873: # -RR-
000926,000874: # COMPUTED ALTITUDE XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000927,000875: # -4
000928,000876: # 2 METERS
000929,000877:
000930,000878: # -SS-
000931,000879: # DP DEGREES XXXX.X DEGREES DP BIT 1 OF HIGH REGISTER =
000932,000880: # 1 DEGREE
000933,000881:
000934,000882: # -TT-
000935,000883: # LANDING RADAR +0000X CHANNEL 33,BIT 6=NOT POSIT. 1
000936,000884: # POSITION (DECIMAL ONLY. CHANNEL 33,BIT 7=NOT POSIT. 2
000937,000885: # DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
000938,000886: # ONLY. CANNOT BE X = 2 FOR LR POSITION 2
000939,000887: # LOADED.)
000940,000888:
000941,000889: # -WW- 15
|
|
Page 22
|
000943,000891: # 360-CDU DEGREES XXX.XX DEGREES SP BIT 1 = 360 - (360/2 )
000944,000892: # (MAX 359.99) DEGREES
000945,000893: # (USES 15 BITS FOR MAGNI-
000946,000894: # TUDE AND 2-S COMP.)
000947,000895:
000948,000896: # -XX-
000949,000897: # POSITION 9 XXXXX. FEET DP BIT 1 OF LOW REGISTER =
000950,000898: # -9
000951,000899: # 2 METERS
000952,000900:
000953,000901: # -YY-
000954,000902: # VELOCITY 4 XXXX.X FEET/SEC DP FRACTIONAL PART OF
000955,000903: # (MAX 328.0) METERS/CENTI-SEC
000956,000904:
000957,000905: # -AAA-
000958,000906: # RADIANS XX.XXX RADIANS DP BIT 1 OF HIGH REGISTER =
000959,000907: # (MAX 31.999) -9
000960,000908: # 2 RADIANS
000961,000909:
000962,000910: # THAT-S ALL ON THE NOUNS.
000963,000911:
|
|
Page 23
|
000965,000913: # ALARM CODES FOR LUMINARY
000966,000914:
000967,000915: # *9 *18 *60 COLUMN
000968,000916:
000969,000917: # CODE * TYPE SET BY
000970,000918:
000971,000919: # 00107 MORE THAN 5 MARK PAIRS AOTMARK
000972,000920: # 00111 MARK MISSING AOTMARK
000973,000921: # 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
000974,000922: # 00113 NO INBITS AOTMARK
000975,000923: # 00114 MARK MADE BUT NOT DESIRED AOTMARK
000976,000924: # 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
000977,000925: # 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING
000978,000926: # 00206 + GIMBAL LOCK.
000979,000927: # 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
000980,000928: # 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, R02, P51, P57
000981,000929: # 00211 COARSE ALIGN ERROR IMU MODE SWITCH
000982,000930: # 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH,T4RPT
000983,000931: # 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
000984,000932: # 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
000985,000933: # 00217 BAD RETURN FROM IMUSTALL P51,P52,P57
000986,000934: # 00220 IMU NOT ALIGNED - NO REFSMMAT R02,R47
000987,000935: # 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
000988,000936: # FINDCDUW
000989,000937: # 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
000990,000938: # 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
000991,000939: # 00405 TWO STARS NOT AVAILABLE P52
000992,000940: # 00421 W-MATRIX OVERFLOW INTEGRV
000993,000941: # 00501 P RADAR ANTENNA OUT OF LIMITS R23
000994,000942: # 00502 BAD RADAR GIMBAL ANGLE INPUT V41N72
000995,000943: # 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V41N72
000996,000944: # 00510 RADAR AUTO DESCRETE NOT PRESENT R25
000997,000945: # 00511 LR ANTENNA MOVED AND NOT REPOSITIONED SERVICER
000998,000946: # 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
000999,000947: # 00515 RR CDU FAIL DISCRETE PRESENT R25
001000,000948: # 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
001001,000949: # 00522 LANDING RADAR POSITION CHANGE R04
001002,000950: # 00523 LR ANTENNA DIDN'T ACHIEVE POSITION 2 V59 IN V60)
001003,000951: # 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
001004,000952: # 00526 RANGE GREATER THAN 400 NAUTICAL MILES P20
001005,000953: # 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21,R24
001006,000954: # LUNAR SURFACE
001007,000955: # OR VEHICLE MANEUVER REQUIRED R24 (20)
001008,000956: # 00530 P LOS NOT IN MODE2 COVERAGE R21
001009,000957: # ON LUNAR SURFACE AFTER 600 SECS.
001010,000958: # 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
001011,000959: # 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32,P72,
001012,000960: # 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32,P72,
001013,000961: # 00603 CSI TO CDH TIME LT TMIN12 P32,P72,P33,P73
|
|
Page 24
|
001015,000963: # 00604 CDH TO TPI TIME LT TMIN23 P32,P72,
001016,000964: # OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
001017,000965: # 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
001018,000966: # 00606 DV EXCEEDS MAXIMUM P32,P72,
001019,000967: # 00611 NO TIG FOR GIVEN ELEV ANGLE P34,P74
001020,000968: # 00701 ILLEGAL OPTION CODE SELECTED P57
001021,000969: # 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
001022,000970: # 01102 AGC SELF TEST ERROR SELF CHECK
001023,000971: # 01105 DOWNLINK TOO FAST T4RUPT
001024,000972: # 01106 UPLINK TOO FAST T4RUPT
001025,000973: # 01107 PHASE TABLE FAILURE. ASSUME RESTART
001026,000974: # ERASABLE MEMORY IS SUSPECT. RESTART
001027,000975: # 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
001028,000976: # 01406 BAD RETURN FROM ROOTPSRS DESCENT GUIDANCE EQS.
001029,000977: # 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
001030,000978: # .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
001031,000979: # VECTOR.) S40.8
001032,000980: # 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
001033,000981: # 01412 DESCENT IGNALG NOT CONVERGING P63
001034,000982: # 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
001035,000983: # 01600 OVERFLOW IN DRIFT TEST IMU 4
001036,000984: # 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
001037,000985: # 01601 IMU 4 (LEM)
001038,000986: # 01703 IGNITION TIME SLIPPED MIDTOAVE
001039,000987: # 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
001040,000988: # CONFIGURATION P40, P42
001041,000989: # 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
001042,000990: # 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
001043,000991: # 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
001044,000992: # 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
001045,000993: # 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
001046,000994: # 04777 ICDU , PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001047,000995: # 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
001048,000996: # 10777 IMU , PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001049,000997: # 13777 IMU , ICDU FAILS CAUSED THE ISS WARNING T4RUPT
001050,000998: # 14777 IMU,ICDU,PIPA FAILS CAUSED ISS WARNING T4RUPT
001051,000999:
001052,001000: # THE FOLLOWING CODES INDICATE THE MORE SERIOUS POODOO ABORTS THAT RESULT
001053,001001: # IN THE PROGRAM GOING TO ROO.
001054,001002:
001055,001003: # 20105 AOTMARK SYSTEM IN USE AOTMARK
001056,001004: # 20430 ACCELERATION OVERFLOW IN INTEGRATION ORBITAL INTEGRATION
001057,001005: # 20607 NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET, TIMERAD
001058,001006: # 21103 UNUSED CCS BRANCH EXECUTED ABORT
001059,001007: # 21204 WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
001060,001008: # CALLED WITH ZERO OR NEGATIVE DELTA-TIME
001061,001009: # 21302 SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
001062,001010: # 21406 BAD RETURN FROM ROOTPSRS IGNITION ALGORITHMN
001063,001011: # 21501 KEYBOARD AND DISPLAY ALARM DURING PINBALL
001064,001012: # INTERNAL USE(NVSUB).ABORT
|
|
Page 25
|
001066,001014: # THE FOLLOWING CODES INDICATE A BAILOUT ABORT THAT RESULTS IN A SOFTWARE
001067,001015: # RESTART
001068,001016: # 31104 DELAY ROUTINE BUSY EXEC
001069,001017: # 31201 EXECUTIVE OVERFLOW-NO VAC AREAS EXEC
001070,001018: # 31202 EXECUTIVE OVERFLOW-NO CORE SETS EXEC
001071,001019: # 31203 WAITLIST OVERFLOW-TOO MANY TASKS WAITLIST
001072,001020: # 31206 SECOND JOB ATTEMPTS TO GO TO SLEEP VIA PINBALL
001073,001021: # KEYBOARD AND DISPLAY PROGRAM
001074,001022: # 31207 NO VAC AREAS FOR MARKS AOTMARK
001075,001023: # 31210 TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
001076,001024: # 31211 ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
001077,001025: # 31502 TWO PRIO DISPLAYS WAITING DSP INTRFCE
001078,001026: # 32000 DAP STILL IN PROGRESS AT NEXT TIME5 RUPT DAP
001079,001027:
|
|
Page 26
|
001081,001029: # CHECKLIST CODES FOR LUMINARY
001082,001030:
001083,001031: # *9 *17 *26 *9 COLUMN
001084,001032:
001085,001033: # R1CODE ACTION TO BE EFFECTED PROGRAM
001086,001034:
001087,001035: # 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
001088,001036: # 00014 PROCEED DO IMU FINE ALIGN ROUTINE P51,P63,P57
001089,001037: # 00014 ENTER DO LANDING SITE DETERMINATION(N89DISP) P57OPTION2
001090,001038: # 00015 PERFORM CELESTIAL BODY ACQUISITION R51,P51
001091,001039: # 00062 SWITCH AGC POWER DOWN P06
001092,001040: # 00201 SWITCH RR MODE TO AUTOMATIC P20,P22,R04
001093,001041: # 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12,P42,P71
001094,001042: # ALSO THR CONT TO AUTO P40,P63,P70
001095,001043: # 00205 PERFORM MANUAL ACQUISITION OF RR R23
001096,001044: # 00500 SWITCH LR ANTENNA TO POSITION 1 P63
001097,001045:
001098,001046: # SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
001099,001047: # PERFORM DENOTES START OR END OF A TASK
001100,001048: # KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
001101,001049:
|
|
Page 27
|
001103,001051: # OPTION CODES FOR LUMINARY
001104,001052:
001105,001053: # THE SPECIFIED OPTION CODES WILL BE FLASHED IN COMPONENT R1 IN
001106,001054: # CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
001107,001055: # ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
001108,001056:
001109,001057: # *9 *17 *52 *11 *25 COLUMN
001110,001058:
001111,001059: # OPTION
001112,001060: # CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
001113,001061:
001114,001062: # 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
001115,001063: # 4=LAND SITE
001116,001064: # 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
001117,001065: # 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
001118,001066: # 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
001119,001067: # 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
001120,001068: # 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
001121,001069: # 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
001122,001070: # 2=TWO BODIES 3=ONE BODY + G
001123,001071: # 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
001124,001072: # ORBIT TO PASS OVER LM
End of include-file ASSEMBLY_AND_OPERATION_INFORMATION.agc. Parent file is MAIN.agc