Source Code
000114,000001: # Copyright: Public domain.
000115,000002: # Filename: ASSEMBLY_AND_OPERATION_INFORMATION.agc
000116,000003: # Purpose: Part of the source code for Luminary 1A build 099.
000117,000004: # It is part of the source code for the Lunar Module's (LM)
000118,000005: # Apollo Guidance Computer (AGC), for Apollo 11.
000119,000006:
000120,000007: # Assembler: yaYUL
000121,000008: # Contact: Jim Lawton <jim.lawton@gmail.com>
000122,000009: # Website: www.ibiblio.org/apollo.
000123,000010: # Pages: 001-027
000124,000011: # Mod history: 2009-05-16 JVL Transcribed from page images.
000125,000012:
000126,000013: # This source code has been transcribed or otherwise adapted from digitized
000127,000014: # images of a hardcopy from the MIT Museum. The digitization was performed
000128,000015: # by Paul Fjeld, and arranged for by Deborah Douglas of the Museum. Many
000129,000016: # thanks to both. The images (with suitable reduction in storage size and
000130,000017: # consequent reduction in image quality as well) are available online at
000131,000018: # www.ibiblio.org/apollo. If for some reason you find that the images are
000132,000019: # illegible, contact me at info@sandroid.org about getting access to the
000133,000020: # (much) higher-quality images which Paul actually created.
000134,000021:
000135,000022: # Notations on the hardcopy document read, in part:
000136,000023:
000137,000024: # Assemble revision 001 of AGC program LMY99 by NASA 2021112-061
000138,000025: # 16:27 JULY 14, 1969
000139,000026:
000140,000027: # Page 1
000141,000028:
000142,000029: # THIS LGC PROGRAM IS INTENDED FOR USE IN THE LM DURING THE MANNED LUNAR LANDING MISSION OR ANY SUBSET THEREOF.
000143,000030: # THE DETAILS OF IMPLEMENTATION ARE SPECIFIED IN REPORT R-567, AS AMENDED.
000144,000031:
000145,000032: # GUIDANCE SYSTEM OPERATIONS PLAN
000146,000033: # FOR MANNED LM EARTH ORBITAL AND LUNAR MISSIONS
000147,000034: # USING PROGRAM LUMINARY
000148,000035:
000149,000036: # THIS PROGRAM AND R-567 HAVE BEEN PREPARED BY THE INSTRUMENTATION LABORATORY, MASSACHUSETTS INSTITUTE OF
000150,000037: # TECHNOLOGY, 75 CAMBRIDGE PARKWAY, CAMBRIDGE, MASSACHUSETTS, UNDER PROJECT 55-238-70, SPONSORED BY THE MANNED
000151,000038: # SPACECRAFT CENTER OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, CONTRACT NAS 9-4065.
000152,000039:
000153,000040: # THIS PROGRAM IS REFERRED TO AS LUMINARY 1A
000154,000041:
000155,000042: # Page 2
000156,000043:
000157,000044: # TABLE OF LOG CARDS
000158,000045: # ASSEMBLY AND OPERATION INFORMATION
000159,000046: # TAGS FOR RELATIVE SETLOC AND BLANK BANK CARDS
000160,000047: # CONTROLLED CONSTANTS
000161,000048: # INPUT/OUTPUT CHANNEL BIT DESCRIPTIONS
000162,000049: # FLAGWORD ASSIGNMENTS
000163,000050: # SUBROUTINE CALLS
000164,000051:
000165,000052: # TABLE OF SUBROUTINE LOG SECTIONS
000166,000053: # LUMERASE
000167,000054: # ERASABLE ASSIGNMENTS
000168,000055: # LNYAIDE
000169,000056: # INTERRUPT LEAD INS
000170,000057: # T4RUPT PROGRAM
000171,000058: # RCS FAILURE MONITOR
000172,000059: # DOWNLINK LISTS
000173,000060: # AGS INITIALIZATION
000174,000061: # FRESH START AND RESTART
000175,000062: # RESTART TABLES
000176,000063: # AOTMARK
000177,000064: # EXTENDED VERBS
000178,000065: # PINBALL NOUN TABLES
000179,000066: # LEM GEOMETRY
000180,000067: # IMU COMPENSATION PACKAGE
000181,000068: # R63
000182,000069: # ATTITUDE MANEUVER ROUTINE
000183,000070: # GIMBAL LOCK AVOIDANCE
000184,000071: # KALCMANU STEERING
000185,000072: # SYSTEM TEST STANDARD LEAD INS
000186,000073: # IMU PERFORMANCE TESTS 2
000187,000074: # IMU PERFORMANCE TESTS 4
000188,000075: # PINBALL GAMES BUTTONS AND LIGHTS
000189,000076: # R60,R62
000190,000077: # S-BAND ANTENNA FOR LM
000191,000078: # LEMP20S
000192,000079: # RADAR LEADIN ROUTINES
000193,000080: # P20-P25
000194,000081: # LEMP30S
000195,000082: # P30,P37
000196,000083: # P32-P35, P72-P75
000197,000084: # GENERAL LAMBERT AIMPOINT GUIDANCE
000198,000085: # KISSING
000199,000086: # GROUND TRACKING DETERMINATION PROGRAM - P21
000200,000087: # P34-P35, P74-P75
000201,000088: # R31
000202,000089: # P76
000203,000090: # R30
000204,000091: # STABLE ORBIT - P38-P39
000205,000092: # Page 3
000206,000093: # FLY
000207,000094: # BURN, BABY, BURN -- MASTER IGNITION ROUTINE
000208,000095: # P40-P47
000209,000096: # THE LUNAR LANDING
000210,000097: # THROTTLE CONTROL ROUTINES
000211,000098: # LUNAR LANDING GUIDANCE EQUATIONS
000212,000099: # P70-P71
000213,000100: # P12
000214,000101: # ASCENT GUIDANCE
000215,000102: # SERVICER
000216,000103: # LANDING ANALOG DISPLAYS
000217,000104: # FINDCDUW -- GUIDAP INTERFACE
000218,000105: # LEMP50S
000219,000106: # P51-P53
000220,000107: # LUNAR AND SOLAR EPHEMERIDES SUBROUTINES
000221,000108: # SKIPPER
000222,000109: # DOWN-TELEMETRY PROGRAM
000223,000110: # INTER-BANK COMMUNICATION
000224,000111: # INTEPRETER
000225,000112: # FIXED-FIXED CONSTANT POOL
000226,000113: # INTERPRETIVE CONSTANTS
000227,000114: # SINGLE PRECISION SUBROUTINES
000228,000115: # EXECUTIVE
000229,000116: # WAITLIST
000230,000117: # LATITUDE LONGITUDE SUBROUTINES
000231,000118: # PLANETARY INERTIAL ORIENTATION
000232,000119: # MEASUREMENT INCORPORATION
000233,000120: # CONIC SUBROUTINES
000234,000121: # INTEGRATION INITIALIZATION
000235,000122: # ORBITAL INTEGRATION
000236,000123: # INFLIGHT ALIGNMENT ROUTINES
000237,000124: # POWERED FLIGHT SUBROUTINES
000238,000125: # TIME OF FREE FALL
000239,000126: # AGC BLOCK TWO SELF-CHECK
000240,000127: # PHASE TABLE MAINTENANCE
000241,000128: # RESTARTS ROUTINE
000242,000129: # IMU MODE SWITCHING ROUTINES
000243,000130: # KEYRUPT, UPRUPT
000244,000131: # DISPLAY INTERFACE ROUTINES
000245,000132: # SERVICE ROUTINES
000246,000133: # ALARM AND ABORT
000247,000134: # UPDATE PROGRAM
000248,000135: # RTB OP CODES
000249,000136: # LMDAP
000250,000137: # T6-RUPT PROGRAMS
000251,000138: # DAP INTERFACE SUBROUTINES
000252,000139: # DAPIDLER PROGRAM
000253,000140: # P-AXIS RCS AUTOPILOT
000254,000141: # Q,R-AXIS RCS AUTOPILOT
000255,000142: # TJET LAW
000256,000143: # Page 4
000257,000144: # KALMAN FILTER
000258,000145: # TRIM GIMBAL CONTROL SYSTEM
000259,000146: # AOSTASK AND AOSJOB
000260,000147: # SPS BACK-UP RCS CONTROL
000261,000148:
000262,000149: # SYMBOL TABLE LISTING
000263,000150: # UNREFERENCED SYMBOL LISTING
000264,000151: # ERASABLE & EQUALS CROSS-REFERENCE TABLE
000265,000152: # SUMMARY OF SYMBOL TABLE LISTINGS
000266,000153: # MEMORY TYPE & AVAILABILITY DISPLAY
000267,000154: # COUNT TABLE
000268,000155: # PARAGRAPHS GENERATED FOR THIS ASSEMBLY
000269,000156: # OCTAL LISTING
000270,000157: # OCCUPIED LOCATIONS TABLE
000271,000158: # SUBROS CALLED & PROGRAM STATUS
000272,000159:
000273,000160: # Page 5
000274,000161: # VERB LIST FOR LUMINARY
000275,000162:
000276,000163: # REGULAR VERBS
000277,000164:
000278,000165: # 00 NOT IN USE
000279,000166: # 01 DISPLAY OCTAL COMP 1 IN R1
000280,000167: # 02 DISPLAY OCTAL COMP 2 IN R1
000281,000168: # 03 DISPLAY OCTAL COMP 3 IN R1
000282,000169: # 04 DISPLAY OCTAL COMP 1,2 IN R1,R2
000283,000170: # 05 DISPLAY OCTAL COMP 1,2,3 IN R1,R2,R3
000284,000171: # 06 DISPLAY DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000285,000172: # 07 DISPLAY DP DECIMAL IN R1,R2 (TEST ONLY)
000286,000173: # 08
000287,000174: # 09
000288,000175: # 10
000289,000176: # 11 MONITOR OCTAL COMP 1 IN R1
000290,000177: # 12 MONITOR OCTAL COMP 2 IN R1
000291,000178: # 13 MONITOR OCTAL COMP 3 IN R1
000292,000179: # 14 MONITOR OCTAL COMP 1,2 IN R1,R2
000293,000180: # 15 MONITOR OCTAL COMP 1,2,3 IN R1,R2,R3
000294,000181: # 16 MONITOR DECIMAL IN R1 OR R1,R2 OR R1,R2,R3
000295,000182: # 17 MONITOR DP DECIMAL IN R1,R2 (TEST ONLY)
000296,000183: # 18
000297,000184: # 19
000298,000185: # 20
000299,000186: # 21 LOAD COMPONENT 1 INTO R1
000300,000187: # 22 LOAD COMPONENT 2 INTO R2
000301,000188: # 23 LOAD COMPONENT 3 INTO R3
000302,000189: # 24 LOAD COMPONENT 1,2, INTO R1,R2
000303,000190: # 25 LOAD COMPONENT 1,2,3 INTO R1,R2,R3
000304,000191: # 26
000305,000192: # 27 DISPLAY FIXED MEMORY
000306,000193: # 28
000307,000194: # 29
000308,000195: # 30 REQUEST EXECUTIVE
000309,000196: # 31 REQUEST WAITLIST
000310,000197: # 32 RECYCLE PROGRAM
000311,000198: # 33 PROCEED WITHOUT DSKY INPUTS
000312,000199: # 34 TERMINATE FUNCTION
000313,000200: # 35 TEST LIGHTS
000314,000201: # 36 REQUEST FRESH START
000315,000202: # 37 CHANGE PROGRAM (MAJOR MODE)
000316,000203: # 38
000317,000204: # 39
000318,000205:
000319,000206: # Page 6
000320,000207: # EXTENDED VERBS
000321,000208:
000322,000209: # 40 XERO CDU-S
000323,000210: # 41 COARSE ALIGN CDU-S
000324,000211: # 42 FINE ALIGN IMU
000325,000212: # 43 LOAD IMU ATT ERROR METERS
000326,000213: # 44 TERMINATE RR CONTINUOUS DESIGNATE (V41N72 OPTION 2)
000327,000214: # 45
000328,000215: # 46
000329,000216: # 47 INITIALIZE AGS (R47)
000330,000217: # 48 REQUEST DAP DATA LOAD ROUTINE (R03)
000331,000218: # 49 REQUEST CREW DEFINED MANEUVER ROUTINE (R62)
000332,000219: # 50 PLEASE PERFORM
000333,000220: # 51
000334,000221: # 52 MARK X-RETICLE
000335,000222: # 53 MARK Y-RETICLE
000336,000223: # 54 MARK X OR Y-RETICLE
000337,000224: # 55 INCREMENT AGC TIME (DECIMAL)
000338,000225: # 56 TERMINATE TRACKING (P20 + P25)
000339,000226: # 57 PERMIT LANDING RADAR UPDATES
000340,000227: # 58 INHIBIT LANDING RADAR UPDATES
000341,000228: # 59
000342,000229: # 60 COMMAND LR TO POSITON 2.
000343,000230: # 61 DISPLAY DAP FOLLOWING ATTITUDE ERRORS.
000344,000231: # 62 DISPLAY TOTAL ATTITUDE ERRORS WITH RESPECT TO NOUN 22.
000345,000232: # 63 SAMPLE RADAR ONCE PER SECOND (R04).
000346,000233: # 64 REQUEST S-BAND ANTENNA ROUTINE (R05).
000347,000234: # 65 DISABLE U AND V JET FIRINGS DURING DPS BURNS.
000348,000235: # 66 VEHICLES ARE ATTACHED. MOVE THIS VEHICLE STATE TO OTHER VEHICLE.
000349,000236: # 67 DISPLAY W MATRIX
000350,000237: # 68
000351,000238: # 69 CAUSE RESTART
000352,000239: # 70 UPDATE LIFTOFF TIME
000353,000240: # 71 UNIVERSAL UPDATE-BLOCK ADR
000354,000241: # 72 UNIVERSAL UPDATE-SINGLE ADR
000355,000242: # 73 UPDATE AGC TIME (OCTAL)
000356,000243: # 74 INITIALIZE ERASABLE DUMP VIA DOWNLINK
000357,000244: # 75 ENABLE U AND V JET FIRINGS DURING DPS BURNS.
000358,000245: # 76 MINIMUM IMPUSE COMMAND MODE.
000359,000246: # 77 RATE COMMAND AND ATTITUDE HOLD MODE
000360,000247: # 78 LR SPURIOUS RETURN TEST START (R77)
000361,000248: # 79 LR SPURIOUS RETURN TEST STOP
000362,000249: # 80 UPDATE LEM STATE VECTOR
000363,000250: # 81 UPDATE CSM STATE FECTOR
000364,000251: # 82 REQUEST ORBIT PARAM DISPLAY (R30)
000365,000252: # 83 REQUEST REND PARAM DISPLAY (R31)
000366,000253: # 84
000367,000254: # 85 DISPLAY RR LOS AZ AND ELEV
000368,000255: # 86
000369,000256: # 87
000370,000257: # Page 7
000371,000258: # 88
000372,000259: # 89 REQUEST RENDEZVOUS FINAL ATTITUDE ROUTINE (R63)
000373,000260: # 90 REQUEST RENDEZVOUS OUT OF PLANE DISPLAY ROUTINE (R36)
000374,000261: # 91 DISPLAY BANK SUM
000375,000262: # 92 OPERATE IMU PERFORMANCE TEST (P07)
000376,000263: # 93 ENABLE W MATRIX INITALIZATION
000377,000264: # 94
000378,000265: # 95 NO UPDATE OF EITHER STATE VECTOR (P20 OR P22)
000379,000266: # 96 INTERRUPT INTEGRATION AND GO TO P00
000380,000267: # 97 PERFORM ENGINE FAIL PROCEDURE
000381,000268: # 98
000382,000269: # 99 PLEASE ENABLE ENGINE
000383,000270:
000384,000271: # Page 8
000385,000272: # IN THE FOLLOWING NOUN LIST THE 'NO LOAD' RESTRICTION MEANS THE NOUN
000386,000273: # CONTAINS AT LEAST ONE COMPONENT WHICH CANNOT BE LOADED, I.E. OF
000387,000274: # SCALE TYPE L (MIN/SEC), PP (2 INTEGERS) OR TT (LANDING RADAR POSITION).
000388,000275: # IN THIS CASE VERBS 24 AND 25 ARE NOT ALLOWED, BUT VERBS 21, 22, OR 23
000389,000276: # MAY BE USED TO LOAD ANY OF THE NOUN'S COMPONENTS WHICH ARE NOT OF THE
000390,000277: # ABOVE SCALE TYPES.
000391,000278:
000392,000279: # THE 'DEC ONLY' RESTRICTION MEANS ONLY DECIMAL OPERATION IS ALLOWED ON
000393,000280: # EVERY COMPONENT IN THE NOUN. (NOTE THAT 'NO LOAD' IMPLIES 'DEC ONLY'.)
000394,000281:
000395,000282: # NORMAL NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000396,000283: # 00 NOT IN USE
000397,000284: # 01 SPECIFY MACHINE ADDRESS (FRACTIONAL) 3COMP .xxxxx FOR EACH
000398,000285: # 02 SPECIFY MACHINE ADDRESS (WHOLE) 3COMP xxxxx. FOR EACH
000399,000286: # 03 SPECIFY MACHINE ADDRESS (DEGREES) 3COMP xxx.xx DEG FOR EACH
000400,000287: # 04 ANGULAR ERROR/DIFFERENCE 1COMP xxx.xx DEG
000401,000288: # 05 ANGULAR ERROR/DIFFERENCE 1COMP xxx.xx DEG
000402,000289: # 06 OPTION CODE 3COMP OCTAL ONLY FOR EACH
000403,000290: # LOADING NOUN 07 WILL SET OR RESET SELECTED BITS IN ANY ERASABLE REGISTER
000404,000291: # 07 ECADR OF WORD TO BE MODIFIED 3COMP OCTAL ONLY FOR EACH
000405,000292: # ONES FOR BITS TO BE MODIFIED
000406,000293: # 1 TO SET OR 0 TO RESET SELECTED BITS
000407,000294: # 08 ALARM DATA 3COMP OCTAL ONLY FOR EACH
000408,000295: # 09 ALARM CODES 3COMP OCTAL ONLY FOR EACH
000409,000296: # 10 CHANNEL TO BE SPECIFIED 1COMP OCTAL ONLY
000410,000297: # 11 TIG OF CSI 3COMP 00xxx. HRS DEC ONLY
000411,000298: # 000xx. MIN MUST LOAD 3 COMPS
000412,000299: # 0xx.xx SEC
000413,000300: # 12 OPTION CODE 2COMP OCTAL ONLY FOR EACH
000414,000301: # (USED BY EXTENDED VERBS ONLY)
000415,000302: # 13 TIG OF CDH 3COMP 00xxx. HRS DEC ONLY
000416,000303: # 000xx. MIN MUST LOAD 3 COMPS
000417,000304: # 0xx.xx SEC
000418,000305: # 14 CHECKLIST 3COMP xxxxx. FOR EACH
000419,000306: # (USED BY EXTENDED VERBS ONLY)
000420,000307: # (NOUN 25 IS PASTED AFTER DISPLAY)
000421,000308: # 15 INCREMENT MACHINE ADDRESS 1COMP OCTAL ONLY
000422,000309: # 16 TIME OF EVENT 3COMP 00xxx. HRS DEC ONLY
000423,000310: # (USED BY EXTENDED VERBS ONLY) 000xx. MIN MUST LOAD 3 COMPS
000424,000311: # 0xx.xx SEC
000425,000312: # 17 SPARE
000426,000313: # 18 AUTO MANEUVER BALL ANGLES 3COMP xxx.xx DEG FOR EACH
000427,000314: # 19 SPARE
000428,000315: # 20 ICDU ANGLES 3COMP xxx.xx DEG FOR EACH
000429,000316: # 21 PIPAS 3COMP xxxxx. PULSES FOR EACH
000430,000317: # 22 NEW ICDU ANGLES 3COMP xxx.xx DEG FOR EACH
000431,000318: # 23 SPARE
000432,000319: # 24 DELTA TIME FOR AGC CLOCK 3COMP 00xxx. HRS DEC ONLY
000433,000320: # 000xx. MIN MUST LOAD 3 COMPS
000434,000321: # 0xx.xx SEC
000435,000322: # Page 9
000436,000323: # 25 CHECKLIST 3COMP xxxxx. FOR EACH
000437,000324: # (USED WITH PLEASE PERFORM ONLY)
000438,000325: # 26 PRIORITY/DELAY, ADRES, BBCON 3COMP OCTAL ONLY FOR EACH
000439,000326: # 27 SELF TEST ON/OFF SWITCH 1COMP xxxxx.
000440,000327: # 28 SPARE
000441,000328: # 29 SPARE
000442,000329: # 30 SPARE
000443,000330: # 31 SPARE
000444,000331: # 32 TIME FROM PERIGEE 3COMP 00xxx. HRS DEC ONLY
000445,000332: # 000xx. MIN MUST LOAD 3 COMPS
000446,000333: # 0xx.xx SEC
000447,000334: # 33 TIME OF IGNITION 3COMP 00xxx. HRS DEC ONLY
000448,000335: # 000xx. MIN MUST LOAD 3 COMPS
000449,000336: # 0xx.xx SEC
000450,000337: # 34 TIME OF EVENT 3COMP 00xxx. HRS DEC ONLY
000451,000338: # 000xx. MIN MUST LOAD 3 COMPS
000452,000339: # 0xx.xx SEC
000453,000340: # 35 TIME FROM EVENT 3COMP 00xxx. HRS DEC ONLY
000454,000341: # 000xx. MIN MUST LOAD 3 COMPS
000455,000342: # 0xx.xx SEC
000456,000343: # 36 TIME OF AGC CLOCK 3COMP 00xxx. HRS DEC ONLY
000457,000344: # 000xx. MIN MUST LOAD 3 COMPS
000458,000345: # 0xx.xx SEC
000459,000346: # 37 TIG OF TPI 3COMP 00xxx. HRS DEC ONLY
000460,000347: # 000xx. MIN MUST LOAD 3 COMPS
000461,000348: # 0xx.xx SEC
000462,000349: # 38 TIME OF STATE BEING INTEGRATED 3COMP 00xxx. HRS DEC ONLY
000463,000350: # 000xx. MIN MUST LOAD 3 COMPS
000464,000351: # 0xx.xx SEC
000465,000352: # 39 SPARE
000466,000353:
000467,000354: # Page 10
000468,000355: # MIXED NOUNS COMPONENTS SCALE AND DECIMAL POINT RESTRICTIONS
000469,000356: # 40 TIME FROM IGNITION/CUTOFF 3COMP xxBxx MIN/SEC NO LOAD, DEC ONLY
000470,000357: # VG, xxxx.x FT/SEC
000471,000358: # DELTA V (ACCUMULATED) xxxx.x FT.SEC
000472,000359: # 41 TARGET AZIMUTH 2COMP xxx.xx DEG (FOR SYSTEM TEST)
000473,000360: # ELEVATION xx.xxx DEG
000474,000361: # 42 APOGEE, 3COMP xxxx.x NAUT MI DEC ONLY
000475,000362: # PERIGEE, xxxx.x NAUT MI
000476,000363: # DELTA V (REQUIRED) xxxx.x FT/SEC
000477,000364: # 43 LATITUDE, 3COMP xxx.xx DEG DEC ONLY
000478,000365: # LONGITUDE, xxx.xx DEG
000479,000366: # ALTITUDE xxxx.x NAUT MI
000480,000367: # 44 APOGEE, 3COMP xxxx.x NAUT MI NO LOAD, DEC ONLY
000481,000368: # PERIGEE, xxxx.x NAUT MI
000482,000369: # TFF xxBxx MIN/SEC
000483,000370: # 45 MARKS, 3COMP xxxxx. NO LOAD, DEC ONLY
000484,000371: # TFI OF NEXT BURN, xxBxx MIN/SEC
000485,000372: # MGA xxx.xx DEG
000486,000373: # 46 AUTOPILOT CONFIGURATION 1COMP OCTAL ONLY
000487,000374: # 47 LEM WEIGHT, 2COMP xxxxx. LBS DEC ONLY
000488,000375: # CSM WEIGHT xxxxx. LBS
000489,000376: # 48 GIMBAL PITCH TRIM, 2COMP xxx.xx DEG DEC ONLY
000490,000377: # GIMBAL ROLL TRIM xxx.xx DEG
000491,000378: # 49 DELTA R, 3COMP xxxx.x NAUT MI DEC ONLY
000492,000379: # DELTA V, xxxx.x FT/SEC
000493,000380: # RADAR DATA SOURCE CODE xxxxx.
000494,000381: # 50 SPARE
000495,000382: # 51 S-BAND ANTENNA ANGLES PITCH 2COMP xxx.xx DEG DEC ONLY
000496,000383: # YAW xxx.xx DEG
000497,000384: # 52 CENTRAL ANGLE OF ACTIVE VEHICLE 1COMP xxx.xx DEG
000498,000385: # 53 SPARE
000499,000386: # 54 RANGE, 3COMP xxx.xx NAUT MI DEC ONLY
000500,000387: # RANGE RATE, xxxx.x FT/SEC
000501,000388: # THETA xxx.xx DEG
000502,000389: # 55 NO. OF APSIDAL CROSSINGS 3COMP xxxxx. DEC ONLY
000503,000390: # ELEVATION ANGLE xxx.xx DEG
000504,000391: # CENTRAL ANGLE OF PASSIVE VEHICLE xxx.xx DEG
000505,000392: # 56 RR LOS AZIMUTH 2COMP xxx.xx DEG
000506,000393: # ELEVATION xxx.xx DEG
000507,000394: # 57 DELTA R 1COMP xxxx.x NAUT MI DEC ONLY
000508,000395: # 58 PERIGEE ALT (POST TPI) 3COMP xxxx.x NAUT MI DEC ONLY
000509,000396: # DELTA V TPI xxxx.x FT/SEC
000510,000397: # DELTA V TPF xxxx.x FT/SEC
000511,000398: # 59 DELTA VELOCITY LOS 3COMP xxxx.x FT/SEC FOR EA. DEC ONLY
000512,000399: # 60 HORIZONTAL VELOCITY 3COMP xxxx.x FT/SEC DEC ONLY
000513,000400: # ALTITUDE RATE xxxx.x FT/SEC
000514,000401: # COMPUTED ALTITUDE xxxxx. FEET
000515,000402: # 61 TIME TO GO IN BRAKING PHASE 3COMP xxBxx MIN/SEC NO LOAD, DEC ONLY
000516,000403: # TIME FROM IGNITION xxBxx MIN/SEC
000517,000404: # Page 11
000518,000405: # CROSS RANGE DISTANCE xxxx.x NAUT MI
000519,000406: # 62 ABSOLUTE VALUE OF VELOCITY 3COMP xxxx.x FT/SEC NO LOAD, DEC ONLY
000520,000407: # TIME FROM IGNITION xxBxx MIN/SEC
000521,000408: # DELTA V (ACCUMULATED) xxxx.x FT/SEC
000522,000409: # 63 ABSOLUTE VALUE OF VELOCITY 3COMP xxxx.x FT/SEC DEC ONLY
000523,000410: # ALTITUDE RATE xxxx.x FT/SEC
000524,000411: # COMPUTED ALTITUDE xxxxx. FEET
000525,000412: # 64 TIME LEFT FOR REDESIGNATION- LPD ANGLE 3COMP xxBxx NO LOAD, DEC ONLY
000526,000413: # ALTITUDE RATE xxxx.x FT/SEC
000527,000414: # COMPUTED ALTITUDE xxxxx. FEET
000528,000415: # 65 SAMPLED AGC TIME 3COMP 00xxx. HRS. DEC ONLY
000529,000416: # (FETCHED IN INTERRUPT) 000xx. MIN MUST LOAD 3 COMPS
000530,000417: # 0xx.xx SEC
000531,000418: # 66 LR RANGE 2COMP xxxxx. FEET NO LOAD, DEC ONLY
000532,000419: # POSITION +0000x
000533,000420: # 67 LRVX 3COMP xxxxx. FT/SEC
000534,000421: # LRVY xxxxx. FT/SEC
000535,000422: # LRVZ xxxxx. FT/SEC
000536,000423: # 68 SLANT RANGE TO LANDING SITE 3COMP xxxx.x NAUT MI NO LOAD, DEC ONLY
000537,000424: # TIME TO GO IN BRAKING PHASE xxBxx MIN/SEC
000538,000425: # LR ALTITUDE - COMPUTED ALTITUDE xxxxx. FEET
000539,000426: # 69 SPARE
000540,000427: # 70 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000541,000428: # 71 AOT DETENT CODE/STAR CODE 3COMP OCTAL ONLY FOR EACH
000542,000429: # 72 RR 360 - TRUNNION ANGLE 2COMP xxx.xx DEG
000543,000430: # SHAFT ANGLE xxx.xx DEG
000544,000431: # 73 NEW RR 360 - TRUNNION ANGLE 2COMP xxx.xx DEG
000545,000432: # SHAFT ANGLE xxx.xx DEG
000546,000433: # 74 TIME FROM IGNITION 3COMP xxBxx MIN/SEC NO LOAD, DEC ONLY
000547,000434: # YAW AFTER VEHICLE RISE xxx.xx DEG
000548,000435: # PITCH AFTER VEHICLE RISE xxx.xx DEG
000549,000436: # 75 DELTA ALTITUDE CDH 3COMP xxxx.x NAUT MI NO LOAD, DEC ONLY
000550,000437: # DELTA TIME (CDH-CSI OR TPI-CDH) xxBxx MIN/SEC
000551,000438: # DELTA TIME (TPI-CDH OR TPI-NOMTPI) xxBxx MIN/SEC
000552,000439: # 76 DESIRED HORIZONTAL VELOCITY 3COMP xxxx.x FT/SEC DEC ONLY
000553,000440: # DESIRED RADIAL VELOCITY xxxx.x FT/SEC
000554,000441: # CROSS-RANGE DISTANCE xxxx.x NAUT MI
000555,000442: # 77 TIME TO ENGINE CUTOFF 2COMP xxBxx MIN/SEC NO LOAD, DEC ONLY
000556,000443: # VELOCITY NORMAL TO CSM PLANE xxxx.x FT/SEC
000557,000444: # 78 RR RANGE 2COMP xxx.xx NAUT MI NO LOAD, DEC ONLY
000558,000445: # RANGE RATE xxxxx. FT/SEC
000559,000446: # 79 CURSOR ANGLE 3COMP xxx.xx DEG DEC ONLY
000560,000447: # SPIRAL ANGLE xxx.xx DEG
000561,000448: # POSITION CODE xxxxx.
000562,000449: # 80 DATA INDICATOR, 2COMP xxxxx.
000563,000450: # OMEGA xxx.xx DEG
000564,000451: # 81 DELTA V (LV) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
000565,000452: # Page 12
000566,000453: # 82 DELTA V (LV) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
000567,000454: # 83 DELTA V (BODY) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
000568,000455: # 84 DELTA V (OTHER VEHICLE) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
000569,000456: # 85 VG (BODY) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
000570,000457: # 86 VG (LV) 3COMP xxxx.x FT/SEC FOR EACH DEC ONLY
000571,000458: # 87 BACKUP OPTICS LOS AZIMUTH 2COMP xxx.xx DEG
000572,000459: # ELEVATION xxx.xx DEG
000573,000460: # 88 HALF UNIT SUN OR PLANET VECTOR 3COMP .xxxxx FOR EACH DEC ONLY
000574,000461: # 89 LANDMARK LATITUDE 3COMP xx.xxx DEG DEC ONLY
000575,000462: # LONGITUDE/2 xx.xxx DEC
000576,000463: # ALTITUDE xxx.xx NAUT MI
000577,000464: # 90 Y 3COMP xxx.xx NM DEC ONLY
000578,000465: # Y DOT xxxx.x FPS
000579,000466: # PSI xxx.xx DEG
000580,000467: # 91 ALTITUDE 3COMP xxxxxB. NAUT MI
000581,000468: # VELOCITY xxxxx. FT/SEC
000582,000469: # FLIGHT PATH ANGLE xxx.xx DEG
000583,000470: # 92 SPARE
000584,000471: # 93 DELTA GYRO ANGLES 3COMP xx.xxx DEG FOR EACH
000585,000472: # 94 SPARE
000586,000473: # 95 SPARE
000587,000474: # 96 SPARE
000588,000475: # 97 SYSTEM TEST INPUTS 3COMP xxxxx. FOR EACH
000589,000476: # 98 SYSTEM TEST RESULTS AND INPUTS 3COMP xxxxx.
000590,000477: # .xxxxx
000591,000478: # xxxxx.
000592,000479: # 99 RMS IN POSITION 3COMP xxxxx. FT DEC ONLY
000593,000480: # RMS IN VELOCITY xxxx.x FT/SEC
000594,000481: # RMS IN BIAS xx.xxx RADIANS
000595,000482:
000596,000483: # Page 13
000597,000484: # REGISTERS AND SCALING FOR NORMAL NOUNS
000598,000485:
000599,000486: # NOUN REGISTER SCALE TYPE
000600,000487: # 00 NOT IN USE
000601,000488: # 01 SPECIFY ADDRESS B
000602,000489: # 02 SPECIFY ADDRESS C
000603,000490: # 03 SPECIFY ADDRESS D
000604,000491: # 04 DSPTEM1 H
000605,000492: # 05 DSPTEM1 H
000606,000493: # 06 OPTION1 A
000607,000494: # 07 XREG A
000608,000495: # 08 ALMCADR A
000609,000496: # 09 FAILREG A
000610,000497: # 10 SPECIFY CHANNEL A
000611,000498: # 11 TCSI K
000612,000499: # 12 OPTIONX A
000613,000500: # 13 TCDH K
000614,000501: # 14 DSPTEMX C
000615,000502: # 15 INCREMENT ADDRESS A
000616,000503: # 16 DSPTEMX K
000617,000504: # 17 SPARE
000618,000505: # 18 FDAIX D
000619,000506: # 19 SPARE
000620,000507: # 20 CDUX D
000621,000508: # 21 PIPAX C
000622,000509: # 22 THETAD D
000623,000510: # 23 SPARE
000624,000511: # 24 DSPTEM2 +1 K
000625,000512: # 25 DSPTEM1 C
000626,000513: # 26 DSPTEM1 A
000627,000514: # 27 SMODE C
000628,000515: # 28 SPARE
000629,000516: # 29 SPARE
000630,000517: # 30 SPARE
000631,000518: # 31 SPARE
000632,000519: # 32 -TPER K
000633,000520: # 33 TIG K
000634,000521: # 34 DSPTEM1 K
000635,000522: # 35 TTOGO K
000636,000523: # 36 TIME2 K
000637,000524: # 37 TTPI K
000638,000525: # 38 TET K
000639,000526: # 39 SPARE
000640,000527:
000641,000528: # Page 14
000642,000529: # REGISTERS AND SCALING FOR MIXED NOUNS
000643,000530:
000644,000531: # NOUN COMP REGISTER SCALE TYPE
000645,000532: # 40 1 TTOGO L
000646,000533: # 2 VGDISP S
000647,000534: # 3 DVTOTAL S
000648,000535: # 41 1 DSPTEM1 D
000649,000536: # 2 DSPTEM1 +1 E
000650,000537: # 42 1 HAPO Q
000651,000538: # 2 HPER Q
000652,000539: # 3 VGDISP S
000653,000540: # 43 1 LAT H
000654,000541: # 2 LONG H
000655,000542: # 3 ALT Q
000656,000543: # 44 1 HAPOX Q
000657,000544: # 2 HPERX Q
000658,000545: # 3 TFF L
000659,000546: # 45 1 TRKMKCNT C
000660,000547: # 2 TTOGO L
000661,000548: # 3 +MGA H
000662,000549: # 46 1 DAPDATR1 A
000663,000550: # 47 1 LEMMASS KK
000664,000551: # 2 CSMMASS KK
000665,000552: # 48 1 PITTIME NN
000666,000553: # 2 ROLLTIME NN
000667,000554: # 49 1 R22DISP Q
000668,000555: # 2 R22DISP +2 S
000669,000556: # 3 WHCHREAD C
000670,000557: # 50 SPARE
000671,000558: # 51 1 ALPHASB H
000672,000559: # 2 BETASB H
000673,000560: # 52 1 ACTCENT H
000674,000561: # 53 SPARE
000675,000562: # 54 1 RANGE JJ
000676,000563: # 2 RRATE S
000677,000564: # 3 RTHETA H
000678,000565: # 55 1 NN C
000679,000566: # 2 ELEV H
000680,000567: # 3 CENTANG H
000681,000568: # 56 1 RR-AZ H
000682,000569: # 2 RR-ELEV H
000683,000570: # 57 1 DELTAR Q
000684,000571: # 58 1 POSTTPI Q
000685,000572: # 2 DELVTPI S
000686,000573: # 3 DELVTPF S
000687,000574: # 59 1 DVLOS S
000688,000575: # 2 DVLOS +2 S
000689,000576: # 3 DVLOS +4 S
000690,000577: # 60 1 VHORIZ S
000691,000578: # Page 15
000692,000579: # 2 HDOTDISP S
000693,000580: # 3 HCALC RR
000694,000581: # 61 1 TTFDISP L
000695,000582: # 2 TTOGO L
000696,000583: # 3 OUTOFPLN QQ
000697,000584: # 62 1 ABVEL S
000698,000585: # 2 TTOGO L
000699,000586: # 3 DVTOTAL S
000700,000587: # 63 1 ABVEL S
000701,000588: # 2 HDOTDISP S
000702,000589: # 3 HCALC1 RR
000703,000590: # 64 1 FUNNYDSP PP
000704,000591: # 2 HDOTDISP S
000705,000592: # 3 HCALC RR
000706,000593: # 65 1 SAMPTIME K
000707,000594: # 2 SAMPTIME K
000708,000595: # 3 SAMPTIME K
000709,000596: # 66 1 RSTACK +6 W
000710,000597: # 2 CHANNEL 33 TT
000711,000598: # 67 1 RSTACK X
000712,000599: # 2 RSTACK +2 Y
000713,000600: # 3 RSTACK +4 Z
000714,000601: # 68 1 RANGEDSP QQ
000715,000602: # 2 TTFDISP L
000716,000603: # 3 DELTAH RR
000717,000604: # 69 SPARE
000718,000605: # 70 1 AOTCODE A
000719,000606: # 2 AOTCODE +1 A
000720,000607: # 3 AOTCODE +2 A
000721,000608: # 71 1 AOTCODE A
000722,000609: # 2 AOTCODE +1 A
000723,000610: # 3 AOTCODE +2 A
000724,000611: # 72 1 CDUT WW
000725,000612: # 2 CDUS D
000726,000613: # 73 1 TANG WW
000727,000614: # 2 TANG +1 D
000728,000615: # 74 1 TTOGO L
000729,000616: # 2 YAW H
000730,000617: # 3 PITCH H
000731,000618: # 75 1 DIFFALT Q
000732,000619: # 2 T1TOT2 L
000733,000620: # 3 T2TOT3 L
000734,000621: # 76 1 ZDOTD S
000735,000622: # 2 RDOTD S
000736,000623: # 3 XRANGE Q
000737,000624: # 77 1 TTOGO L
000738,000625: # 2 YDOT S
000739,000626: # 78 1 RSTACK U
000740,000627: # 2 RSTACK +2 V
000741,000628: # 79 1 CURSOR D
000742,000629: # Page 16
000743,000630: # 2 SPIRAL D
000744,000631: # 3 POSCODE C
000745,000632: # 80 1 DATAGOOD C
000746,000633: # 2 OMEGAD H
000747,000634: # 81 1 DELVLVC S
000748,000635: # 2 DELVLVC +2 S
000749,000636: # 3 DELVLVC +4 S
000750,000637: # 82 1 DELVLVC S
000751,000638: # 2 DELVLVC +2 S
000752,000639: # 3 DELVLVC +4 S
000753,000640: # 83 1 DELVIMU S
000754,000641: # 2 DELVIMU +2 S
000755,000642: # 3 DELVIMU +4 S
000756,000643: # 84 1 DELVOV S
000757,000644: # 2 DELVOV +2 S
000758,000645: # 3 DELVOV +4 S
000759,000646: # 85 1 VGBODY S
000760,000647: # 2 VGBODY +2 S
000761,000648: # 3 VGBODY +4 S
000762,000649: # 86 1 DELVLVC S
000763,000650: # 2 DELVLVC +2 S
000764,000651: # 3 DELVLVC +4 S
000765,000652: # 87 1 AZ D
000766,000653: # 2 EL D
000767,000654: # 88 1 STARAD B
000768,000655: # 2 STARAD +2 B
000769,000656: # 3 STARAD +4 B
000770,000657: # 89 1 LANDLAT G
000771,000658: # 2 LANDLONG G
000772,000659: # 3 LANDALT JJ
000773,000660: # 90 1 RANGE JJ
000774,000661: # 2 RRATE S
000775,000662: # 3 RTHETA H
000776,000663: # 91 1 P21ALT Q (MEMORY/100 TO DISPLAY TENS N.M.)
000777,000664: # 2 P21VEL P
000778,000665: # 3 P21GAM H
000779,000666: # 92 SPARE
000780,000667: # 93 1 OGC G
000781,000668: # 2 OGC +2 G
000782,000669: # 3 OGC +4 G
000783,000670: # 94 SPARE
000784,000671: # 95 SPARE
000785,000672: # 96 SPARE
000786,000673: # 97 1 DSPTEM1 C
000787,000674: # 2 DSPTEM1 +1 C
000788,000675: # 3 DSPTEM1 +2 C
000789,000676: # 98 1 DSPTEM2 C
000790,000677: # 2 DSPTEM2 +1 B
000791,000678: # 3 DSPTEM2 +2 C
000792,000679: # 99 1 WWPOS XX
000793,000680: # Page 17
000794,000681: # 2 WWVEL YY
000795,000682: # 3 WWBIAS AAA
000796,000683: # Page 18
000797,000684: # NOUN SCALES AND FORMATS
000798,000685:
000799,000686: # -SCALE TYPE- PRECISION
000800,000687: # UNITS DECIMAL FORMAT -- AGC FORMAT
000801,000688: # ------------ -------------- -- ----------
000802,000689:
000803,000690: # -A-
000804,000691: # OCTAL xxxxx SP OCTAL
000805,000692:
000806,000693: # -B- -14
000807,000694: # FRACTIONAL .xxxxx SP BIT 1 = 2 UNITS
000808,000695: # (MAX .99996)
000809,000696:
000810,000697: # -C-
000811,000698: # WHOLE xxxxx. SP BIT 1 = 1 UNIT
000812,000699: # (MAX 16383.)
000813,000700:
000814,000701: # -D- 15
000815,000702: # CDU DEGREES xxx.xx DEGREES SP BIT 1 = 360/2 DEGREES
000816,000703: # (MAX 359.99) (USES 15 BITS FOR MAGNI-
000817,000704: # TUDE AND 2-S COMP.)
000818,000705:
000819,000706: # -E- 14
000820,000707: # ELEVATION DEGREES xx.xxx DEGREES SP BIT 1 = 90/2 DEGREES
000821,000708: # (MAX 89.999)
000822,000709:
000823,000710: # -F- 14
000824,000711: # DEGREES (180) xxx.xx DEGREES SP BIT 1 = 180/2 DEGREES
000825,000712: # (MAX 179.99)
000826,000713:
000827,000714: # -G-
000828,000715: # DP DEGREES (90) xx.xxx DEGREES DP BIT 1 OF LOW REGISTER =
000829,000716: # 28
000830,000717: # 360/2 DEGREES
000831,000718:
000832,000719: # -H-
000833,000720: # DP DEGREES (360) xxx.xx DEGREES DP BIT 1 OF LOW REGISTER =
000834,000721: # 28
000835,000722: # (MAX 359.99) 360/2 DEGREES
000836,000723:
000837,000724: # Page 19
000838,000725: # -K-
000839,000726: # TIME (HR, MIN, SEC) 00xxx. HR DP BIT 1 OF LOW REGISTER =
000840,000727: # 000xx. MIN -2
000841,000728: # 0xx.xx SEC 10 SEC
000842,000729: # (DECIMAL ONLY.
000843,000730: # MAX MIN COMP=59
000844,000731: # MAX SEC COMP=59.99
000845,000732: # MAX CAPACITY=745 HRS
000846,000733: # 39 MINS
000847,000734: # 14.55 SECS.
000848,000735: # WHEN LOADING, ALL 3
000849,000736: # COMPONENTS MUST BE
000850,000737: # SUPPLIED.)
000851,000738:
000852,000739: # -L-
000853,000740: # TIME (MIN/SEC) xxBxx MIN/SEC DP BIT 1 OF LOW REGISTER =
000854,000741: # (B IS A BLANK -2
000855,000742: # POSITION, DECIMAL 10 SEC
000856,000743: # ONLY, DISPLAY OR
000857,000744: # MONITOR ONLY. CANNOT
000858,000745: # BE LOADED.
000859,000746: # MAX MIN COMP=59
000860,000747: # MAX SEC COMP=59
000861,000748: # VALUES GREATER THAN
000862,000749: # 59 MIN 59 SEC
000863,000750: # ARE DISPLAYED AS
000864,000751: # 59 MIN 59 SEC.)
000865,000752:
000866,000753: # -M- -2
000867,000754: # TIME (SEC) xxx.xx SEC SP BIT 1 = 10 SEC
000868,000755: # (MAX 163.83)
000869,000756:
000870,000757: # -N-
000871,000758: # TIME(SEC) DP xxx.xx SEC DP BIT 1 OF LOW REGISTER =
000872,000759: # -2
000873,000760: # 10 SEC.
000874,000761:
000875,000762: # -P-
000876,000763: # VELOCITY 2 xxxxx. FEET/SEC DP BIT 1 OF HIGH REGISTER =
000877,000764: # (MAX 41994.) -7
000878,000765: # 2 METERS/CENTI-SEC
000879,000766:
000880,000767: # -Q-
000881,000768: # POSITION 4 xxxx.x NAUTICAL MILES DP BIT 1 OF LOW REGISTER =
000882,000769: # 2 METERS
000883,000770:
000884,000771: # -S-
000885,000772: # VELOCITY 3 xxxx.x FT/SEC DP BIT 1 OF HIGH REGISTER =
000886,000773: # -7
000887,000774: # 2 METERS/CENTI-SEC
000888,000775:
000889,000776: # Page 20
000890,000777: # -T- -2
000891,000778: # G xxx.xx G SP BIT 1 = 10 G
000892,000779: # (MAX 163.83)
000893,000780:
000894,000781: # -U-
000895,000782: # RENDEZVOUS xxx.xx NAUT MI DP LOW ORDER BIT OF LOW ORDER
000896,000783: # RADAR RANGE WORD = 9.38 FEET
000897,000784:
000898,000785: # -V-
000899,000786: # RENDEZVOUS xxxxx. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000900,000787: # RADAR RANGE RATE WORD = -.6278 FEET/SEC
000901,000788:
000902,000789: # -W-
000903,000790: # LANDING RADAR xxxxx. FEET DP LOW ORDER BIT OF LOW ORDER
000904,000791: # ALTITUDE WORD = 1.079 FEET
000905,000792:
000906,000793: # -X-
000907,000794: # LANDING RADAR xxxxx. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000908,000795: # VELX WORD = -.6440 FEET/SEC
000909,000796:
000910,000797: # -Y-
000911,000798: # LANDING RADAR xxxxx. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000912,000799: # VELY WORD = 1.212 FEET/SEC
000913,000800:
000914,000801: # -Z-
000915,000802: # LANDING RADAR xxxxx. FEET/SEC DP LOW ORDER BIT OF LOW ORDER
000916,000803: # VELZ WORD = .8668 FEET/SEC
000917,000804:
000918,000805: # -AA-
000919,000806: # INITIAL/FINAL xxxxx. FEET DP LOW ORDER BIT OF LOW ORDER
000920,000807: # ALTITUDE WORD = 2.345 FEET
000921,000808:
000922,000809: # -BB-
000923,000810: # ALTITUDE RATE xxxxx. FEET/SEC SP LOW ORDER BIT = .5
000924,000811: # (MAX 08191.) FEET/SEC
000925,000812:
000926,000813: # -CC-
000927,000814: # FORWARD/LATERAL xxxxx. FEET/SEC SP LOW ORDER BIT = .5571
000928,000815: # VELOCITY (MAX 09126.) FEET/SEC
000929,000816:
000930,000817: # -DD-
000931,000818: # ROTATIONAL HAND xxxxx. DEG/SEC SP FRACTIONAL PART OF PI RAD
000932,000819: # CONTROLLER ANGULAR (MAX 00044.) 4 SEC
000933,000820: # RATES
000934,000821:
000935,000822: # -EE-
000936,000823: # OPTICAL TRACKER xxx.xx DEG. DP LOW ORDER BIT OF LOW ORDER
000937,000824: # AZIMUTH ANGLE 15
000938,000825: # WORD = 360/2 DEGREES
000939,000826:
000940,000827: # Page 21
000941,000828:
000942,000829: # -JJ-
000943,000830: # POSITION5 xxx.xx NAUT MI DP BIT 1 OF LOW REGISTER =
000944,000831: # 2 METERS
000945,000832:
000946,000833: # -KK- 16
000947,000834: # WEIGHT2 xxxxx. LBS SP FRACTIONAL PART OF 2 KG
000948,000835:
000949,000836: # -NN-
000950,000837: # TRIM DEGREES 2 xxx.xx DEG SP BIT 1=.01 SEC(TIME)
000951,000838: # (MAX 032.76)
000952,000839:
000953,000840: # -PP-
000954,000841: # 2 INTEGERS +xxByy DP BIT 1 OF HIGH REGISTER =
000955,000842: # (B IS A BLANK 1 UNIT OF XX
000956,000843: # POSITION. DECIMAL BIT 1 OF LOW REGISTER =
000957,000844: # ONLY, DISPLAY OR 1 UNIT OF YY
000958,000845: # MONITOR ONLY. CANNOT (EACH REGISTER MUST
000959,000846: # BE LOADED.) CONTAIN A POSITIVE INTEGER
000960,000847: # (MAX 99B99) LESS THAN 100)
000961,000848:
000962,000849: # -QQ-
000963,000850: # POSITION7 xxxx.x NAUT MI DP BIT 1 OF LOW REGISTER =
000964,000851: # (MAX 9058.9) -4
000965,000852: # 2 METERS
000966,000853:
000967,000854: # -RR-
000968,000855: # COMPUTED ALTITUDE xxxxx. FEET DP BIT 1 OF LOW REGISTER =
000969,000856: # -4
000970,000857: # 2 METERS
000971,000858:
000972,000859: # -SS-
000973,000860: # DP DEGREES xxxx.x DEGREES DP BIT 1 OF HIGH REGISTER =
000974,000861: # 1 DEGREE
000975,000862:
000976,000863: # -TT-
000977,000864: # LANDING RADAR +0000x CHANNEL 33, BIT 6 = NOT POSIT. 1
000978,000865: # POSITION (DECIMAL ONLY. CHANNEL 33, BIT 7 = NOT POSIT. 2
000979,000866: # DISPLAY OR MONITOR X = 1 FOR LR POSITION 1
000980,000867: # ONLY. CANNOT BE X = 2 FOR LR POSITION 2
000981,000868: # LOADED.)
000982,000869:
000983,000870: # -WW- 15
000984,000871: # 360-CDU DEGREES xxx.xx DEGREES SP BIT 1 = 360 - (360/2 )
000985,000872: # (MAX 359.99) DEGREES
000986,000873: # (USES 15 BITS FOR MAGNI-
000987,000874: # TUDE AND 2-S COMP.)
000988,000875:
000989,000876: # -XX-
000990,000877: # POSITION 9 xxxxx. FEET DP BIT 1 OF LOW REGISTER =
000991,000878: # -9
000992,000879: # 2 METERS
000993,000880:
000994,000881: # Page 22
000995,000882:
000996,000883: # -YY-
000997,000884: # VELOCITY 4 xxxx.x FEET/SEC DP FRACTIONAL PART
000998,000885: # (MAX 328.0) METERS/CENTI-SEC
000999,000886:
001000,000887: # -AAA-
001001,000888: # RADIANS xx.xxx RADIANS DP BIT 1 OF HIGH REGISTER =
001002,000889: # (MAX 31.999) -9
001003,000890: # 2 RADIANS.
001004,000891:
001005,000892:
001006,000893: # THAT'S ALL ON THE NOUNS.
001007,000894:
001008,000895: # Page 23
001009,000896: # ALARM CODES FOR LUMINARY
001010,000897:
001011,000898: # *9 *18 *60 COLUMN
001012,000899:
001013,000900: # CODE * TYPE SET BY
001014,000901:
001015,000902: # 00105 ** AOTMARK SYSTEM IN USE
001016,000903: # 00107 MORE THAN 5 MARK PAIRS AOTMARK
001017,000904: # 00111 MARK MISSING AOTMARK
001018,000905: # 00112 MARK OR MARK REJECT NOT BEING ACCEPTED AOTMARK
001019,000906: # 00113 NO INBITS AOTMARK
001020,000907: # 00114 MARK MADE BUT NOT DESIRED AOTMARK
001021,000908: # 00115 NO MARKS IN LAST PAIR TO REJECT AOTMARK
001022,000909: # 00206 ZERO ENCODE NOT ALLOWED WITH COARSE ALIGN IMU MODE SWITCHING
001023,000910: # 00206 + GIMBAL LOC
001024,000911: # 00207 ISS TURNON REQUEST NOT PRESENT FOR 90 SEC T4RUPT
001025,000912: # 00210 IMU NOT OPERATING IMU MODE SWITCH, IMU-2, RD2, P51, P57
001026,000913: # 00211 COARSE ALIGN ERROR IMU MODE SWITCH
001027,000914: # 00212 PIPA FAIL BUT PIPA IS NOT BEING USED IMU MODE SWITCH, T4RPT
001028,000915: # 00213 IMU NOT OPERATING WITH TURN-ON REQUEST T4RUPT
001029,000916: # 00214 PROGRAM USING IMU WHEN TURNED OFF T4RUPT
001030,000917: # 00217 BAD RETURN FROM IMUSTALL P51, P52, P57
001031,000918: # 00220 IMU NOT ALIGNED - NO REFSMMAT R02, R47
001032,000919: # 00401 DESIRED GIMBAL ANGLE YIELDS GIMBAL LOCK INF ALIGN, IMU-2,
001033,000920: # FINDCDUW
001034,000921: # 00402 FINDCDUW NOT CONTROLLING ATTITUDE FINDCDUW
001035,000922: # 00404 TWO STARS NOT AVAILABLE IN ANY DETENT R59, LUNAR SURFACE
001036,000923: # 00405 TWO STARS NOT AVAILABLE P52
001037,000924: # 00421 W-MATRIX OVERFLOW INTEGRV
001038,000925: # 00430 ** ACCELERATION OVERFLOW IN INTEGRATION ORBITAL INTEGRATION
001039,000926: # 00501 P RADAR ANTENNA OUT OF LIMITS R23
001040,000927: # 00502 BAD RADAR GIMBAL ANGLE INPUT V41N72
001041,000928: # 00503 P RADAR ANTENNA DESIGNATE FAIL R21, NON-P IN V41N72
001042,000929: # 00510 RADAR AUTO DESCRETE NOT PRESENT R25
001043,000930: # 00511 LR NOT IN POSITION 2 OR REPOSITIONING SERVICER
001044,000931: # 00514 P RR GOES OUT OF AUTO MODE WHILE IN USE P20
001045,000932: # 00515 RR CDU FAIL DISCRETE PRESENT R25
001046,000933: # 00520 RADAR RUPT NOT EXPECTED AT THIS TIME RADAR READ
001047,000934: # 00521 COULD NOT READ RADAR P20
001048,000935: # 00522 LANDING RADAR POSITION CHANGE RADAR READ
001049,000936: # 00523 P LR ANTENNA DIDN'T ACHIEVE POSITION 2 SERVICER, V60 (NON-P IN V60)
001050,000937: # 00525 P DELTA THETA GREATER THAN 3 DEGREES R22
001051,000938: # 00526 P RANGE GREATER THAN 400 NAUT. MILES P20, P22
001052,000939: # 00527 P LOS NOT IN MODE II COVERAGE WHILE ON R21, R24
001053,000940: # LUNAR SURFACE
001054,000941: # OR VEHICLE MANEUVER REQUIRED R24 (20)
001055,000942: # 00530 P LOS NOT IN MODE2 COVERAGE R21
001056,000943: # ON LUNAR SURFACE AFTER 600 SECS.
001057,000944: # 00600 IMAGINARY ROOTS ON FIRST ITERATION P32, P72
001058,000945: # 00601 PERIGEE ALTITUDE CSI LT PMIN1 P32, P72.
001059,000946:
001060,000947: # Page 24
001061,000948:
001062,000949: # 00602 PERIGEE ALTITUDE CDH LT PMIN2 P32, P72.
001063,000950: # 00603 CSI TO CDH TIME LT TMIN12 P32, P72, P33, P73
001064,000951: # 00604 CDH TO TPI TIME LT TMIN23 P32, P72,
001065,000952: # OR COMPUTED CDH TIME GREATER THAN INPUT TP1 TIME
001066,000953: # 00605 NUMBER OF ITERATIONS EXCEEDS LOOP MAXIMUM P32, P72
001067,000954: # 00606 DV EXCEEDS MAXIMUM P32, P72
001068,000955: # 00607 ** NO SOLN FROM TIME-THETA OR TIME-RADIUS TIMETHET, TIMERAD
001069,000956: # 00611 NO TIG FOR GIVEN ELEV ANGLE P34, P74
001070,000957: # 00701 ILLEGAL OPTION CODE SELECTED P57
001071,000958: # 00777 PIPA FAIL CAUSED THE ISS WARNING T4RUPT
001072,000959: # 01102 AGC SELF TEST ERROR SELF CHECK
001073,000960: # 01103 ** UNUSED CCS BRANCH EXECUTED ABORT
001074,000961: # 01104 * DELAY ROUTINE BUSY EXEC
001075,000962: # 01105 DOWNLINK TOO FAST T4RUPT
001076,000963: # 01106 UPLINK TOO FAST T4RUPT
001077,000964: # 01107 PHASE TABLE FAILURE. ASSUME RESTART
001078,000965: # ERASABLE MEMORY IS SUSPECT. RESTART
001079,000966: # 01201 * EXECUTIVE OVERFLOW - NO VAC AREAS EXEC
001080,000967: # 01202 * EXECUTIVE OVERFLOW - NO CORE SETS EXEC
001081,000968: # 01203 * WAITLIST OVERFLOW - TOO MANY TASKS WAITLIST
001082,000969: # 01204 ** WAITLIST, VARDELAY, FIXDELAY, OR LONGCALL WAITLIST ROUTINES
001083,000970: # CALLED WITH ZERO OR NEGATIVE DELTA-TIME
001084,000971: # 01206 ** SECOND JOB ATTEMPTS TO GO TO SLEEP PINBALL
001085,000972: # 01206 VIA KYBD AND DISPLAY PROGRAM
001086,000973: # 01207 * NO VAC AREAS FOR MARKS AOTMARK
001087,000974: # 01210 * TWO PROGRAMS USING DEVICE AT SAME TIME MODE SWITCHING
001088,000975: # 01211 * ILLEGAL INTERRUPT OF EXTENDED VERB AOTMARK
001089,000976: # 01301 ARCSIN-ARCCOS ARGUMENT TOO LARGE INTERPRETER
001090,000977: # 01302 ** SQRT CALLED WITH NEGATIVE ARGUMENT INTERPRETER
001091,000978: # 01406 BAD RETURN FROM ROOTPSRS DESCENT GUIDANCE EQS.
001092,000979: # 01406 ** BAD RETURN FROM ROOTPSRS IGNITION ALGORITHM
001093,000980:
001094,000981: # NOTE: 1406 IS A POODOO DURING THE IGNITION ALGORITHM
001095,000982: # AND AN ALARM DURING THE ACTUAL GUIDANCE PHASE.
001096,000983:
001097,000984: # 01407 VG INCREASING (DELTA-V ACCUMULATED S40.8
001098,000985: # .GT. 90 DEGREES AWAY FROM DESIRED THRUST S40.8
001099,000986: # VECTOR.) S40.8
001100,000987: # 01410 UNINTENTIONAL OVERFLOW IN GUIDANCE DESCENT GUIDANCE EQS.
001101,000988: # 01412 DESCENT IGNALG NOT CONVERGING P63
001102,000989: # 01501 ** KEYBOARD AND DISPLAY ALARM DURING PINBALL
001103,000990: # 01501 INTERNAL USE (NVSUB). ABORT
001104,000991: # 01502 ** ILLEGAL FLASHING DISPLAY GOPLAY
001105,000992: # 01520 V37 REQUEST NOT PERMITTED AT THIS TIME V37
001106,000993: # 01600 OVERFLOW IN DRIFT TEST IMU 4
001107,000994: # 01601 BAD IMU TORQUE OPT PRE ALIGN CALIB
001108,000995: # 01601 IMU 4 (LEM)
001109,000996: # 01703 IGNITION TIME SLIPPED MIDTOAVE
001110,000997: # 01706 INCORRECT PROGRAM REQUESTED FOR VEHICLE
001111,000998: # CONFIGURATION P40, P42
001112,000999:
001113,001000: # Page 25
001114,001001:
001115,001002: # 02000 * DAP STILL IN PROGRESS AT NEXT TIMES RUPT DAP
001116,001003: # 02001 JET FAILURES HAVE DISABLED Y-Z TRANS. DAP
001117,001004: # 02002 JET FAILURES HAVE DISABLED X TRANSLATION DAP
001118,001005: # 02003 JET FAILURES HAVE DISABLED P-ROTATION DAP
001119,001006: # 02004 JET FAILURES HAVE DISABLED U-V ROTATION DAP
001120,001007: # 03777 ICDU FAIL CAUSED THE ISS WARNING T4RUPT
001121,001008: # 04777 ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001122,001009: # 07777 IMU FAIL CAUSED THE ISS WARNING T4RUPT
001123,001010: # 10777 IMU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001124,001011: # 13777 IMU, ICDU FAILS CAUSED THE ISS WARNING T4RUPT
001125,001012: # 14777 IMU, ICDU, PIPA FAILS CAUSED THE ISS WARNING T4RUPT
001126,001013:
001127,001014: # * INDICATES AN ABORT CODE THAT RESULTS IN A SOFTWARE RESTART.
001128,001015:
001129,001016: # ** INDICATES A MORE SERIOUS ABORT CODE THAT RESULTS IN THE
001130,001017: # PROGRAM GOING TO R00.
001131,001018:
001132,001019: # P INDICATES A PRIORITY ALARM.
001133,001020:
001134,001021: # ALL OTHERS ARE NON-ABORTIVE
001135,001022:
001136,001023: # Page 26
001137,001024:
001138,001025: # CHECKLIST CODES FOR LUMINARY
001139,001026:
001140,001027: # *9 *17 *26 *9 COLUMN
001141,001028:
001142,001029: # R1CODE ACTION TO BE EFFECTED PROGRAM
001143,001030:
001144,001031: # 00013 KEY IN NORMAL OR GYRO TORQUE COARSE ALIGN P52
001145,001032: # 00014 PROCEED DO IMU FINE ALIGN ROUTINE P51, P63, P57
001146,001033: # 00014 ENTER DO LANDING SITE DETERMINATION (N89DISP) P57OPTION2
001147,001034: # 00015 PERFORM CELESTIAL BODY ACQUISITION R51, P51
001148,001035: # 00062 SWITCH AGC POWER DOWN P06
001149,001036: # 00201 SWITCH RR MODE TO AUTOMATIC P20, P22, R04
001150,001037: # 00203 SWITCH GUID CONTROL TO GNC, MODE TO AUTO... P12, P42, P71
001151,001038: # ALSO THR CONT TO AUTO P40, P63, P70
001152,001039: # 00205 PERFORM MANUAL ACQUISITION OF RR R23
001153,001040: # 00500 SWITCH LR ANTENNA TO POSITION 1 P63
001154,001041:
001155,001042: # SWITCH DENOTES CHANGE POSITION OF A CONSOLE SWITCH
001156,001043: # PERFORM DENOTES START OR END OF A TASK
001157,001044: # KEY IN DENOTES KEY IN OF DATA THRU THE DSKY
001158,001045:
001159,001046: # Page 27
001160,001047: # OPTION CODES FOR LUMINARY
001161,001048:
001162,001049: # THE SPECIFIED OPTION CODES WIL BE FLASHED IN COMPONENT R1 IN
001163,001050: # CONJUNCTION WITH V04N06 OR V04N12 (FOR EXTENDED VERBS) TO REQUEST THE
001164,001051: # ASTRONAUT TO LOAD INTO COMPONENT R2 THE OPTION HE DESIRES.
001165,001052:
001166,001053: # *9 *17 *52 *11 *25 COLUMN
001167,001054:
001168,001055: # OPTION
001169,001056: # CODE PURPOSE INPUT FOR COMPONENT 2 PROGRAM(S) APPLICABILITY
001170,001057:
001171,001058: # 00001 SPECIFY IMU ORIENTATION 1=PREF 2=NOM 3=REFSMMAT P52 ALL
001172,001059: # 4=LAND SITE
001173,001060: # 00002 SPECIFY VEHICLE 1=THIS 2=OTHER P21,R30 ALL
001174,001061: # 00003 SPECIFY TRACKING ATTITUDE 1=PREFERRED 2=OTHER R63 ALL
001175,001062: # 00004 SPECIFY RADAR 1=RR 2=LR R04 SUNDANCE + LUMINARY
001176,001063: # 00005 SPECIFY SOR PHASE 1=FIRST 2=SECOND P38 COLOSSUS + LUMINARY
001177,001064: # 00006 SPECIFY RR COARSE ALIGN OPTION 1=LOCKON 2=CONTINUOUS DESIG. V41N72 SUNDANCE + LUMINARY
001178,001065: # 00010 SPECIFY ALIGNMENT MODE 0=ANY TIME 1=REFSMMAT +G P57 LUMINARY
001179,001066: # 2=TWO BODIES 3=ONE BODY + G
001180,001067: # 00012 SPECIFY CSM ORBIT OPTION 1=NO ORBIT CHANGE 2=CHANGE P22 LUMINARY
001181,001068: # ORBIT TO PASS OVER LM.
001182,001069:
End of include-file ASSEMBLY_AND_OPERATION_INFORMATION.agc. Parent file is MAIN.agc